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Author Topic: Aotian-1, a Chinese hypersonic reentry demonstrator flown tested on 20/09/2013?  (Read 86869 times)

Offline sferrin

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And regarding the 'can-do attitude' you claim has died in the west please make sure you qualify that you are speaking for yourself.

Yeah?  Where's Fasthawk? RATTLRS? HyFly? X-51 developments? LRASM-B? AARGM? ATKs MSST? What happened to follow on HTV-2 flights? US Army AHW? There are isolated exceptions to the rule (SpaceX and Blue Origin for example) but in the DoD? Please.  The only X-51 flight that was marginally successful (the last one) they ALMOST DIDN'T DO BECAUSE THEY THOUGHT, "WHAT IF WE FAIL?".   That's straight from the horse's mouth.  And what did they do with that glimmer of success?  Quit immediately.  "Whoa, that was scary.  Better not do that again, we might not get as lucky." 
"DARPA Hard"  It ain't what it use to be.

Offline VH

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I worked third shift on Apollo at what was then North American. I was right out of high school and attending Harbor JC to later transfer to UCSD. The dedication of our work team was phenomenal. The sheer determination to beat the Russians to the moon was beyond belief. While things may have slipped a bit since that time that same heart still beats among other Americans today.

Yeah I said it: Americans. Like you I also want more and would like to see those projects you mentioned come to fruition. But I am not bitter due to our lack of progress in certain areas. There are too many examples of America raising up and raising hell. And the damn damn is about to be rained down on those who doubt our ability to lead the way.

Please stay tuned!

Offline antigravite

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I worked third shift on Apollo at what was then North American. I was right out of high school and attending Harbor JC to later transfer to UCSD. The dedication of our work team was phenomenal. The sheer determination to beat the Russians to the moon was beyond belief. While things may have slipped a bit since that time that same heart still beats among other Americans today.

Yeah I said it: Americans. Like you I also want more and would like to see those projects you mentioned come to fruition. But I am not bitter due to our lack of progress in certain areas. There are too many examples of America raising up and raising hell. And the damn damn is about to be rained down on those who doubt our ability to lead the way.

Please stay tuned!

Okay guys. If you want to discuss US technological supremacy and 3rd shift Apollo, there is the bar.

The context has changed. Tools changed. The global situation has changed and we all have to understand this. You cant think of today's situation framed in the past. We should get back to China's hypersonic aerospace / reentry topic.

I'm not like you. In those matters I stick to the facts and I am agnostic to understand what the hell is going out here. Wether you like it or not, China is making huge progress in various areas of hypersonics.

Back to the point. Thank you.

A.
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Offline antigravite

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Thermal protection device of attitude control system for hypersonic-speed and large-attack-angle reentry vehicle
Patent No.CN106394938 (A)
Inventor(s):   SHAN HUAWEI; LU DI; LIU LIHONG; WANG HUI; HU CHENGLAN; LIN XUEFENG; TU ZHENGGUANG; QIN JIANFEI; SHU MENGJIONG +
Applicant(s):   THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD +
Application number:   CN20161863521 20160929 
Priority number(s):   CN20161863521 20160929
Abstract: The invention discloses a thermal protection device of an attitude control system for a hypersonic-speed and large-attack-angle reentry vehicle. The thermal protection device is used for thermal protection of an attitude control power unit, and comprises a rear bottom cover plate, a rear bottom cover plate heat-proof layer, an attitude control heat-proof force-bearing plate, an attitude control heat-proof layer, an attitude control engine jet pipe heat-proof sleeve and a pluggable plug heat-proof sleeve, wherein the rear bottom cover plate is mounted on a cabin and serves as a force-bearing piece, the attitude control power unit is arranged on the rear bottom cover plate, and the rear bottom cover plate is covered with the rear bottom cover plate heat-proof layer; attitude control power unit is wrapped and sleeved with the attitude control heat-proof force-bearing plate, and the attitude control heat-proof force-bearing plate is covered with the attitude control heat-proof layer; the attitude control power unit comprises an attitude control engine, an attitude control engine jet pipe is arranged at an outlet of the attitude control engine, and an end opening of the attitude control engine jet pipe is wrapped and sleeved with the attitude control engine jet pipe heat-proof sleeve; and a pluggable plug is wrapped and sleeved with the pluggable plug heat-proof sleeve. By adoption of the thermal protection device of the attitude control system for the hypersonic-speed and large-attack-angle reentry vehicle, thermal protection of the attitude control system for the hypersonic-speed and large-attack-angle reentry vehicle can be effectively achieved, and the design reliability of the attitude control system can be improved.

Thermal protection device for hypersonic gliding aircraft 
Patent No. CN106547965 (A)
Inventor(s):   SHAN HUAWEI; WANG HUI; HU CHENGLAN; LU DI; LIU LIHONG; LIN XUEFENG; TU ZHENGGUANG; QIN JIANFEI; SHU MENGJIONG +
Applicant(s):   THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD +
Application number:   CN20161929527 20161031
Priority number(s):   CN20161929527 20161031
Abstract(A) The invention discloses a thermal protection device for a hypersonic gliding aircraft. The thermal protection device comprises a thermal protection layer, a heat-insulation layer and a carrying layer, wherein the carrying layer is covered with the heat-insulation layer; the heat-insulation layer is covered with the thermal protection layer; the thermal protection layer and the carrying layer are separated from each other without physical connection or contact in order to ensure free deformation of the thermal protection layer and the carrying layer in a pneumatic heating environment; a plurality of pieces of thermal protection layers are spliced with one another to form the whole thermal protection layer; the plurality of pieces of thermal protection layers are spliced with one another at the corners of cabin segments, angle parts of the cabin segments, and joints between horizontal fins and a cabin body; a plurality of thermal protection strips are locally arranged between the thermal protection layer at the joints of the cabin segments and the carrying layer; the plurality of thermal protection strips are arranged at intervals; the thermal protection strips can slide freely relative to the thermal protection layer in order to adapt to stress deformation; and the thermal protection strips and the thermal protection layer are made of the same material. In the thermal protection device, the plurality of pieces of thermal protection layers are provided, and the thermal protection layer and the carrying layer are designed separately, so that the problems of thermal matching and thermal stress can be solved effectively, and the reliability of the thermal protection device is enhanced.


Device for determining performance of control surface transmission mechanism in thermal-mechanical environments 
PatentNo.CN106352925 (A)
Inventor(s):   LIU YEBAO; RONG HUA; CHEN LIANG; YUAN YUAN; SHI MIQING; ZHAO JIANBO; SHA AN'AN; DU PENGFEI; ZHENG SIXING; HUANG SHIYONG; ZHANG JING; CAI QIAOYAN; HAI ERHAN; ZHAO DAHAI; SHAO QIUHU +
Applicant(s):   CHINA ACADEMY LAUNCH VEHICLE TECHNOLOGY +
Application number:   CN20161839685 20160921
Priority number(s):   CN20161839685 20160921
Abstract
The invention discloses a device for determining performance of a control surface transmission mechanism in thermal-mechanical environments and relates to the field of thermal protection of hypersonic flight vehicles in aerospace. The device comprises an oscillating guide bar-torsion shaft type air rudder mechanism, a heating device, a bearing reaction simulation device, a torque sensor, a transition supporting seat, a torque applying device, a connecting platform, a heat insulation device and a steering engine supporting seat support. The device has the advantages that the device is capable of carrying out not only mechanism function test in a mechanical environment at a normal temperature but also motion reliability test and determination of thermal sealing and thermal transfer characteristics of the mechanism in a thermal environment, so that utilization rate of the device is improved; simultaneous thermal-mechanical loading during motion of the oscillating guide bar-torsion shaft type air rudder mechanism can be achieved; six-component force and rotation inertia of a control surface are simulated sufficiently, so that testing result reliability is improved, and the device is widely applicable to testing of different models of air rudder systems.

A.
« Last Edit: July 10, 2017, 09:45:43 am by antigravite »
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Offline Airplane

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And regarding the 'can-do attitude' you claim has died in the west please make sure you qualify that you are speaking for yourself.

Yeah?  Where's Fasthawk? RATTLRS? HyFly? X-51 developments? LRASM-B? AARGM? ATKs MSST? What happened to follow on HTV-2 flights? US Army AHW? There are isolated exceptions to the rule (SpaceX and Blue Origin for example) but in the DoD? Please.  The only X-51 flight that was marginally successful (the last one) they ALMOST DIDN'T DO BECAUSE THEY THOUGHT, "WHAT IF WE FAIL?".   That's straight from the horse's mouth.  And what did they do with that glimmer of success?  Quit immediately.  "Whoa, that was scary.  Better not do that again, we might not get as lucky."

The advent of stealth, followed about 10 years later by the fall of the Soviet Union killed the need for speed. Many big ticket items were scrapped immediately after the demise of the USSR including the Virginia, the B-2, the Midgetman and others... That was the 90s. Then came 2001 and we know where defense spending went for the next 16 years. There has been no need for hypersonic weapons, and only now are we seeing things starting to get warm again with potential foes.

There were other more important weapons systems to modernize the military that were canceled to even be concerned about hypersonic weapons that were not needed.
"The test of success is not what you do when your on top. Success is how high you bounce when you hit bottom.
General George S. Patton

Offline sferrin

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There were other more important weapons systems to modernize the military that were canceled to even be concerned about hypersonic weapons that were not needed.

Really?  So why all the failed programs then if they weren't needed?
"DARPA Hard"  It ain't what it use to be.

Offline Airplane

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There were other more important weapons systems to modernize the military that were canceled to even be concerned about hypersonic weapons that were not needed.

Really?  So why all the failed programs then if they weren't needed?

I work in engineering on unspecified "vehicles", and I've been both a mechanical and electrical engineer. If you do not keep the talent pool "warm" with projects for the sake of maintaining first hand knowledge, then a given capability is truly 100% lost forever until it is reinvented. What you may call a failed project is actually a 'win' for maintaining experience and know-how. These failed projects are giving many engineers first hand experience and also making gains in knowledge over what was done in the past. Be thankful the US is keeping the talent warm until such time these weapons may be needed. We learn as much from 'fails' as we learn with the 'wins'.


Oops! In the above post I meant "seawolf" instead of "virgina"
« Last Edit: July 10, 2017, 09:38:38 am by Airplane »
"The test of success is not what you do when your on top. Success is how high you bounce when you hit bottom.
General George S. Patton

Offline sferrin

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There were other more important weapons systems to modernize the military that were canceled to even be concerned about hypersonic weapons that were not needed.

Really?  So why all the failed programs then if they weren't needed?

I work in engineering on unspecified "vehicles", and I've been both a mechanical and electrical engineer. If you do not keep the talent pool "warm" with projects for the sake of maintaining first hand knowledge, then a given capability is truly 100% lost forever until it is reinvented. What you may call a failed project is actually a 'win' for maintaining experience and know-how. These failed projects are giving many engineers first hand experience and also making gains in knowledge over what was done in the past. Be thankful the US is keeping the talent warm until such time these weapons may be needed. We learn as much from 'fails' as we learn with the 'wins'.

The purpose was not to keep the pool "warm".  If they were interested in charity programs for that purpose they'd have been worried about not losing what we already had. (Nuclear weapon expertise, large solid motors, and ramjets for example.)  With these other programs, quitting at the first sign of difficulty only teaches how to produce failures.  They never get the chance to find out what actually works.  They just know what they did didn't work.  Doesn't sound incredibly effective to me. 
"DARPA Hard"  It ain't what it use to be.

Offline antigravite

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Hi, here's another might-be related interesting patent. Enjoy.

A.

Thermal protection device for hypersonic gliding aircraft 
Patent Number: CN106547965 (A)
Inventor(s):   SHAN HUAWEI; WANG HUI; HU CHENGLAN; LU DI; LIU LIHONG; LIN XUEFENG; TU ZHENGGUANG; QIN JIANFEI; SHU MENGJIONG +
Applicant(s):   THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD +
Application number:   CN20161929527 20161031
Priority number(s):   CN20161929527 20161031
Abstract: The invention discloses a thermal protection device for a hypersonic gliding aircraft. The thermal protection device comprises a thermal protection layer, a heat-insulation layer and a carrying layer, wherein the carrying layer is covered with the heat-insulation layer; the heat-insulation layer is covered with the thermal protection layer; the thermal protection layer and the carrying layer are separated from each other without physical connection or contact in order to ensure free deformation of the thermal protection layer and the carrying layer in a pneumatic heating environment; a plurality of pieces of thermal protection layers are spliced with one another to form the whole thermal protection layer; the plurality of pieces of thermal protection layers are spliced with one another at the corners of cabin segments, angle parts of the cabin segments, and joints between horizontal fins and a cabin body; a plurality of thermal protection strips are locally arranged between the thermal protection layer at the joints of the cabin segments and the carrying layer; the plurality of thermal protection strips are arranged at intervals; the thermal protection strips can slide freely relative to the thermal protection layer in order to adapt to stress deformation; and the thermal protection strips and the thermal protection layer are made of the same material. In the thermal protection device, the plurality of pieces of thermal protection layers are provided, and the thermal protection layer and the carrying layer are designed separately, so that the problems of thermal matching and thermal stress can be solved effectively, and the reliability of the thermal protection device is enhanced.
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Offline antigravite

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Below is a database-ready csv list of known patents (64 as of today's posting) filed by and issued to the "THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACADEMY". Some of them are useful and bear special relevance in the context of hypersonics, reentry, and VTHL & HTHL RLVs. (Table head followed by structured data.)

Title,"Publication number","Publication date","Inventor(s)","Applicant(s)","International classification","Cooperative Patent Classification","Application number","Date of application","Priority number(s)","Patents cited in the search report","Literature cited in the search report","Patents cited during examination","Literature cited during examination","Other patent citations","Other literature citations","Patents used in opposition","Literature used in opposition","Patents cited by the applicant","Literature cited by the applicant","International search citation","International search NPL citation","Supplementary international search citation","Supplementary international search NPL citation"

                                                                           
Thermal protection device of attitude control system for hypersonic-speed and large-attack-angle reentry vehicle,"CN106394938 (A)","2017-02-15","SHAN HUAWEI     LU DI     LIU LIHONG     WANG HUI     HU CHENGLAN     LIN XUEFENG     TU ZHENGGUANG     QIN JIANFEI     SHU MENGJIONG","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","B64G1/58","","CN20161863521","20160929","CN20161863521 20160929","","","","","","","","","","","","","",""                                                   

Missile-rotating satellite searching method for hypersonic velocity missile,"CN106568355 (A)","2017-04-19","MAO JING     ZENG QINGWEI     SUN LIHUA     MAO JINDI     LI SHUMIN     DENG CHAN     SHU MENGJIONG     CUI YUEJUN     GUI YONGFENG     GUO JIANGTAO     LIN XUEFENG     TU ZHENGGUANG     YANG XIN     ZHOU ZHENG     LI GUANGLEI     MENG BIN     LIU LIHONG     CHEN KEWEN","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","F42B15/01","","CN20161939916","20161101","CN20161939916 20161101","","","","","","","","","","","","","",""                        
Aircraft rudder system three-dimensional load performance testing device and test method thereof,"CN106564616 (A)","2017-04-19","GUO HUIRONG     ZHANG ZHENGYI     DENG ZHIJUN     CHU CHENGBIAO     HU SHANGANG     DUAN XIANGJUN     FAN KAICHUN","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","B64F5/60","","CN20161947869","20161026","CN20161947869 20161026","","","","","","","","","","","","","",""                                                         

Mounting structure for aircraft built-in type engine and shifting assembly method for mounting structure,"CN106564605 (A)","2017-04-19","ZHANG ZHENGYI     LIU QING     HU SHANGANG     WANG HUI     FAN KAICHUN","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","B64D27/26    B64F5/10","","CN20161951439","20161026","CN20161951439 20161026","","","","","","","","","","","","","",""                                                            

Azimuth measurement method based on distance measurement principle,"CN106569222 (A)","2017-04-19","XU WEIGUO     MA XINPU     QIN CHUN     SONG CHANGZHE     CHEN XINGFU     HAN MINGJING     ZHANG HONG","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","G01S17/42","","CN20161935503","20161101","CN20161935503 20161101","","","","","","","","","","","","","",""                                                         

Integral proportional guidance nonlinear correction method,"CN106556287 (A)","2017-04-05","YAN QINTAO     YUE XINGZUO     WU LEI     JIANG JINLONG     YANG DENGFENG     CHEN XINGFU     CUI YUEJUN     XIA FEI     TIAN QUNFANG     ZHU WEI     ZHU ZHENGHUI","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","F41G3/00","","CN20161944823","20161102","CN20161944823 20161102","","","","","","","","","","","","","",""                                             

Thermal protection device for hypersonic gliding aircraft,"CN106547965 (A)","2017-03-29","SHAN HUAWEI     WANG HUI     HU CHENGLAN     LU DI     LIU LIHONG     LIN XUEFENG     TU ZHENGGUANG     QIN JIANFEI     SHU MENGJIONG","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","G06F17/50","","CN20161929527","20161031","CN20161929527 20161031","","","","","","","","","","","","","",""                                                   

Low-altitude hood casting device for high-speed unmanned aerial vehicle,"CN106516077 (A)","2017-03-22","ZHANG ZHENGYI     WANG WENLONG     XU GUOWEI     QIN YOUHUA     BAO YONGDING     ZHAI HAITAO","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","B64C1/14","","CN20161897912","20161014","CN20161897912 20161014","","","","","","","","","","","","","",""                                                            

Single-soldier rapid rocket battle field testing method and system based on network communication,"CN106524838 (A)","2017-03-22","LIU QIHANG     LI XIAODAN     GAN LIN     HUA QING     YU GUISHENG     XIAO YIN     WANG DENG","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","F42B35/02","","CN20161901770","20161014","CN20161901770 20161014","","","","","","","","","","","","","",""                                                         

Demodulation method for incoherent spread spectrum communication system,"CN106506037 (A)","2017-03-15","LI RAN     PENG KEXUE     WANG DONG     FU TAO     LI ZHI     ZHANG JING     WANG JIE","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","H04B1/707    H04B1/708    H04L27/233","","CN20161939433","20161025","CN20161939433 20161025","","","","","","","","","","","","","",""                                                   

Locking device for large-tonnage carrier,"CN106494642 (A)","2017-03-15","ZHU SHUFENG     LI MINGBING     LI XIUZHEN     ZHANG KUN     LI FANG","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","B64G1/16","","CN20161905952","20161018","CN20161905952 20161018","","","","","","","","","","","","","",""                                                               

Four-core flight control computer based on dual-SoC architecture SiP modules,"CN106527261 (A)","2017-03-22","CHEN MINGXIN     ZHENG YU     LI BING     HUANG XIAOMING     CHEN JIALIN     DING BO     SONG CHANGZHE     WU XIANG     HAN MINGJING     WANG HUAN","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","G05B19/042","","CN20161947821","20161026","CN20161947821 20161026","","","","","","","","","","","","","",""                                                

Separation, connection and locking device for launching vehicle and launching pad,"CN106468522 (A)","2017-03-01","ZHU SHUFENG     LI MINGBING     LI XIUZHEN     ZHANG ALING","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","F41F1/00    B60R11/00","","CN20161834292","20160913","CN20161834292 20160913","","","","","","","","","","","","","",""                                                               

Vehicle heat preservation layer and manufacturing method thereof,"CN106428644 (A)","2017-02-22","WANG YANGJIAN     XU GUOWEI     FENG KAI     GUO HUIRONG     CHEN WEI","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","B64G1/58","","CN20161887243","20160928","CN20161887243 20160928","","","","","","","","","","","","","",""                                                               

Shear-stress-resisting flange butt joint device,"CN106438602 (A)","2017-02-22","ZHANG XIAOBO     LI XIUZHEN     LI MINGBING     FAN ZHIYONG     ZHOU XINHONG     XU CHENGLONG","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","F16B1/02","","CN20161887315","20160928","CN20161887315 20160928","","","","","","","","","","","","","",""                                                            

Compound attitude control method of grid rudder and lateral jet,"CN106444807 (A)","2017-02-22","GUO YIJIANG     YAO SHAOJUN     LI YAN     JIANG JINLONG     WANG ZHIJUN     TIAN QUNFANG     BAO XIAOQIANG     ZHU WEI     YANG DENGFENG     CHEN XINGFU     SU MAO","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","G05D1/08","","CN20161864293","20160929","CN20161864293 20160929","","","","","","","","","","","","","",""                                             

Gas detecting device,"CN106442354 (A)","2017-02-22","WANG YULEI     WANG HUIHUA     XU WEICAI     HU HAILI     YAN LISONG     YANG XIAOWEI     LAN SHUO     LI MENGQING","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","G01N21/31    G01N21/03","","CN20161863505","20160929","CN20161863505 20160929","","","","","","","","","","","","","",""                                                   

High-temperature-resisting flexible quartz fiber sealing ring,"CN106439019 (A)","2017-02-22","WANG HUI     ZHANG ZHENGYI     HU SHANGANG     FAN KAICHUN","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","F16J15/10","","CN20161850923","20160926","CN20161850923 20160926","","","","","","","","","","","","","",""                                                                  

Satellite and rocket separation system,"CN106428645 (A)","2017-02-22","LIANG JIQIU     XIANG BIN     HU CHANGWEI     PENG WEI     HU SHI     HUANG LEI     XIAO RENQIN     WEN XIAONI     HAN TONG     WU JIHUA","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","B64G1/64","","CN20161754292","20160829","CN20161754292 20160829","","","","","","","","","","","","","",""                                                

Self-locked folding grid rudder integrating positioning and bearing,"CN106197172 (A)","2016-12-07","WU JINGFENG     WANG BOZHE     FAN KAICHUN     LIANG JIQIU     CHU CHENGBIAO     BAO YONGDING     XIN AO","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","F42B15/00","","CN20161817188","20160908","CN20161817188 20160908","","","","","","","","","","","","","",""                                                         

Aircraft head heat container with repeatable disassembly and assembly,"CN106394937 (A)","2017-02-15","GAO HAO     LI MINGBING     LI XIUZHEN     ZHU SHUFENG","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","B64G1/52","","CN20161834566","20160920","CN20161834566 20160920","","","","","","","","","","","","","",""                                                                  

High-Mach number long-endurance aircraft surface sensor mounting device,"CN106379547 (A)","2017-02-08","WANG HUI     WANG WENLONG     FAN KAICHUN     SHAN HUAWEI     LU DI     DAI ZHAOPENG     ZHU XUAN     XIAO HANSHAN","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","B64D47/00","","CN20161863465","20160929","CN20161863465 20160929","","","","","","","","","","","","","",""                                                      

Sectional semitrailer,"CN106379431 (A)","2017-02-08","ZHANG XIAOBO     LI XIUZHEN     LI MINGBING     CHEN PING     ZHOU XINHONG     ZHU SHUFENG","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","B62D53/06    B60B35/00    B60B35/12    B60G17/00    B60S9/04    B60S9/10    B62D53/08","","CN20161887103","20160928","CN20161887103 20160928","","","","","","","","","","","","","",""                                          

Aircraft nonlinear attitude control system stability analysis method,"CN106383523 (A)","2017-02-08","BAO XIAOQIANG     ZHU WEI     CHEN XINGFU     CHEN HONGYAN     YANG DENGFENG     TIAN QUNFANG     JIANG JINLONG     GUO YIJIANG     LI YAN     CUI YUEJUN     YE CHANG","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","G05D1/08","","CN20161874908","20160930","CN20161874908 20160930","","","","","","","","","","","","","",""                                             

Transition navigation method applicable to airborne launching of missile,"CN106379559 (A)","2017-02-08","LIU JIANXIONG     XIA FEI     XU FANGJIA     WANG ZHIJUN     YAO SHAOJUN     JIANG JINLONG     SONG CHANGZHE     LI HAN     HUANG XINXIN     CHEN XINGFU     XU GUOWEI","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","B64G1/24    F42B15/01","","CN20161864500","20160929","CN20161864500 20160929","","","","","","","","","","","","","",""                                          

Isolation type electric push rod control method and device with in-place feedback function,"CN106354040 (A)","2017-01-25","ZHENG ZHIWEI     CAI CHUNMEI     SUN BINGGANG     CHEN YAO     HE DONG     CHEN ZHE     HE QINNAN     LEI YONGJIE     ZHANG YANPING","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","G05B19/04","","CN20161905882","20161018","CN20161905882 20161018","","","","","","","","","","","","","",""                                                   

Folding fin automatic and synchronous unlocking driving device,"CN106352746 (A)","2017-01-25","XU CHENGLONG     CHEN PING     DING WEI     YANG HUI     LI XIUZHEN     ZHANG XIAOBO","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","F42B10/02","","CN20161906020","20161018","CN20161906020 20161018","","","","","","","","","","","","","",""                                                            

Heat protection and diversion integrated device of attitude control nozzle in high-Mach environment,"CN106347637 (A)","2017-01-25","LU DI     WANG HUI     SHAN HUAWEI     DAI ZHAOPENG     WANG WENLONG     FAN KAICHUN","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","B64C15/02    B64D33/04","","CN20161864195","20160929","CN20161864195 20160929","","","","","","","","","","","","","",""                                                         

Starting monitoring device and method for torque extraction generator,"CN106357179 (A)","2017-01-25","LI GANG     CHEN ZHE     WANG WENJUN     HUANG JUYING","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","H02P9/08    H02P101/45","","CN20161817218","20160908","CN20161817218 20160908","","","","","","","","","","","","","",""                                                               

Space-based Internet-of-Things system structure and networking method thereof,"CN106357321 (A)","2017-01-25","YAN HAIPING     XIANG BIN     LIANG JIQIU     WANG XINGYOU     CHI XIANBIN     SUN SHUPENG     WU XIAOMENG     DUAN XIAO     YAN YEHUI","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","H04B7/185    H04L29/08    H04W4/00","","CN20161817127","20160908","CN20161817127 20160908","","","","","","","","","","","","","",""                                             

Fiber laser asymmetric compensation spectral synthesizing device,"CN106338836 (A)","2017-01-18","LIU HOUKANG     DING SHULIN     ZHAO PENGFEI     LYU LIANG     WU CHUNFENG     JIANG YONGLIANG     LI QIANG","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","G02B27/10","","CN20161933072","20161025","CN20161933072 20161025","","","","","","","","","","","","","",""                                                         

Angle deviation calibration method between two interferometer emergence plane wave light beams,"CN106338261 (A)","2017-01-18","YAN LISONG     WANG HUIHUA     LI QIANG     CHEN XIAOCHEN     SHI YAOTAO     JIANG YONGLIANG     XU WEICAI     WANG YULEI     HU HAILI","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","G01B11/26","","CN20161820673","20160913","CN20161820673 20160913","","","","","","","","","","","","","",""                                                   

Object tracking control system,"CN106338808 (A)","2017-01-18","XU YANGANG     TUO WENBO     LEI YANG     SONG LEI     WU YILING     ZHANG GUIQING","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","G02B7/182    G05D1/12","","CN20161902481","20161017","CN20161902481 20161017","","","","","","","","","","","","","",""                                                         

End cap heat resistance connecting device,"CN106314758 (A)","2017-01-11","DAI ZHAOPENG     WANG HUI     WANG WENLONG     FAN KAICHUN     ZHU XUAN     LIU QING     OU CHAO","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","B64C1/40","","CN20161863502","20160929","CN20161863502 20160929","","","","","","","","","","","","","",""                                                         

Universal controller of spaceflight carrier rocket,"CN106325292 (A)","2017-01-11","DAN CHUNHUA     DING BO     SONG CHANGZHE     TAO JIN     DU PENG     XIE YANG     ZHANG HONGQIAN     CHEN MINGXIN     WU XIANG     ZHENG YU","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","G05D1/08    G05D1/10","","CN20161899957","20161017","CN20161899957 20161017","","","","","","","","","","","","","",""                                             

Method and system for determining airborne load of missile distribution,"CN106326664 (A)","2017-01-11","SUN MEIFENG     ZHANG YIGUANG     JIA XIANGTING     RAN HONG     CHAO KAIXIU     CHEN KEWEN","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","G06F19/00","","CN20161769626","20160830","CN20161769626 20160830","","","","","","","","","","","","","",""                                                            

Underwater unmanned platform aircraft autonomous test launch and control system,"CN106292644 (A)","2017-01-04","LONG YAOSONG     XI MAOJUN     WANG ZHONGLING     WANG ZHUO     YAO SHAOJUN     JIANG JINLONG     SONG CHANGZHE     DING BO     LI BING     ZHANG KUI     LU HONGHAI","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","G05B23/02","","CN20161866277","20160929","CN20161866277 20160929","","","","","","","","","","","","","",""                                             

Rapid analysis and optimization method for vibration response characteristic of carrier rocket cabin,"CN106295074 (A)","2017-01-04","CAO PENG     FU MIGUO     LIANG JIQIU     LIU XIAOLEI     SHU MENGJIONG     ZHAO TAO     FENG NANPENG     ZHAO QUAN     ZHOU LYU     CHEN ZHIGUO","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","G06F17/50","","CN20161764335","20160830","CN20161764335 20160830","","","","","","","","","","","","","",""                                                

Flight test data recording device and method for recording and reading test data,"CN106296872 (A)","2017-01-04","FU TAO     QI SHIBING     WANG XIAOLIN     WANG YUFEI     WANG DENG     WANG DONG","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","G07C5/08    G06F3/06","","CN20161638321","20160805","CN20161638321 20160805","","","","","","","","","","","","","",""                                                         

Object type and position state recognition method,"CN106289335 (A)","2017-01-04","LI GANG     CHEN YAO     HE QINNAN     ZHENG WEI","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","G01D5/249","","CN20161569649","20160719","CN20161569649 20160719","","","","","","","","","","","","","",""                                                                  

Border area coolant flow adjusting device for injector,"CN106246412 (A)","2016-12-21","HUANG FENG     WANG TAOFENG     LIANG JIQIU     WANG XIAOYU     ZHANG FANG     LIU ZHANGLONG     ZHOU LEI     LIU YANG     CHEN ZE     CHEN WEI     YANG YI     YU QUAN     CHEN WENJIE","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","F02K9/64","","CN20161866526","20160929","CN20161866526 20160929","US4739613 (A)    US6324832 (B1)    CN105736181 (A)    CN105888883 (A)","","","","","","","","","","","","",""                              

Horizontal wing inner wall temperature sensor installation device and method,"CN106248234 (A)","2016-12-21","LU DI     WANG HUI     DAI ZHAOPENG     SHAN HUAWEI     WANG WENLONG     FAN KAICHUN","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","G01K1/14","","CN20161863504","20160929","CN20161863504 20160929","","","","","","","","","","","","","",""                                                            

Launching stand with lifting deflector,"CN106247855 (A)","2016-12-21","XU CHENGLONG     YANG HUI     LI MINGBING     LI FANG","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","F41F3/04    F16C35/00","","CN20161834232","20160913","CN20161834232 20160913","","","","","","","","","","","","","",""                                                               

Large-aperture plane mirror splicing detection alignment method,"CN106248352 (A)","2016-12-21","YAN LISONG     LI QIANG     WANG HUIHUA     CHEN XIAOCHEN     SHI YAOTAO     JIANG YONGLIANG     XU WEICAI     WANG YULEI     YANG ZIWEI","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","G01M11/02","","CN20161820991","20160913","CN20161820991 20160913","","","","","","","","","","","","","",""                                                   

Method for controlling rolling time domain of flight orbit of spacecraft,"CN106114910 (A)","2016-11-16","CHI XIANBIN     LIANG JIQIU     HU ZHANGWEI     SUN SHUPENG     YAN YEHUI     YE CHANG     ZHANG JIANPENG     DUAN XIAO     WU XIAOMENG     WANG KUN","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","B64G1/24","","CN20161442832","20160615","CN20161442832 20160615","","","","","","","","","","","","","",""                                                

Inertial navigation standard prism misalignment angle self adaptive measuring method based on linear array type CCD (charge coupled device),"CN106153075 (A)","2016-11-23","LI CHUNQUAN     ZHOU HAI     WANG YONG     ZHANG LI","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","G01C25/00","","CN20161673251","20160811","CN20161673251 20160811","","","","","","","","","","","","","",""                                                                  

Supplement type two-cylinder synchronous hydraulic control method and system thereof,"CN106122140 (A)","2016-11-16","WANG WENJUN     LI XIUZHEN     LEI JIANHONG     CHEN YIHONG     CHEN PING","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","F15B11/22    F15B21/02","","CN20161820672","20160913","CN20161820672 20160913","","","","","","","","","","","","","",""                                                            

Combined throat liner spraying pipe of solid rocket engine and manufacturing method,"CN106050477 (A)","2016-10-26","XU YURONG     ZHONG ZHIWEN     ZHOU SHENGPAN     XU JIERONG     YU QUAN     CHEN WENJIE     SI XUELONG","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","F02K9/97","","CN20161623732","20160728","CN20161623732 20160728","","","","","","","","","","","","","",""                                                         

High-speed vehicle insulating layer and installation method thereof,"CN106005485 (A)","2016-10-12","XU GUOWEI     FAN KAICHUN     LIU QING     HU SHANGANG","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","B64G1/58","","CN20161492898","20160628","CN20161492898 20160628","","","","","","","","","","","","","",""                                                                  

Integrated airborne optical pod test system,"CN106017862 (A)","2016-10-12","YU XIANG     YANG KAIXIN     ZHONG HUA     WU FENGYANG     CHEN LIFENG     ZHOU SHIPING","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","G01M11/00","","CN20161303282","20160510","CN20161303282 20160510","","","","","","","","","","","","","",""                                                            

Flexible connection device for high-temperature resistant radome,"CN105914463 (A)","2016-08-31","XU GUOWEI     WANG YANGJIAN     CHEN WEI     SANG XIJUN     QIN YOUHUA","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","H01Q1/42    H01Q1/12    H01Q1/28","","CN20161488553","20160628","CN20161488553 20160628","","","","","","","","","","","","","",""                                                         

Sun-pointing control system for satellite and control method of sun-pointing control system,"CN105905317 (A)","2016-08-31","YAN YEHUI     LIANG JIQIU     HU CHANGWEI     SUN SHUPENG     CHI XIANBIN     GUO YIJIANG     WU XIAOMENG     DUAN XIAO     ZHANG JIANPENG     WANG KUN","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","B64G1/24","","CN20161414531","20160607","CN20161414531 20160607","","","","","","","","","","","","","",""                                                

Calibration method of inertial unit optical aiming prism installation error,"CN105910624 (A)","2016-08-31","SHEN XIAOLONG     LIU MING     WANG ANDI     HU HUAFENG     YANG DAOAN","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","G01C25/00    G01C1/06","","CN20161302867","20160504","CN20161302867 20160504","","","","","","","","","","","","","",""                                                            

Serial inertial navigation system having self-calibrating, self-aligning and self-diagnosing functions,"CN105865486 (A)","2016-08-17","LIU YUANYUAN     YU QIANG     HU QIBO     LIU JUNQING     REN YONGFANG     GAO BO     YANG XIN     ZHENG YONGQIANG     LYU JIANGTAO     LIU MING     LUO WEI     HU HUAFENG     DAI SHILONG","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","G01C25/00","","CN20161181486","20160328","CN20161181486 20160328","","","","","","","","","","","","","",""                                       

General advanced upper stage of solid launch vehicle,"CN105841556 (B)    CN105841556 (A)","2016-08-10","LIANG JIQIU     HU CHANGWEI     SUN SHUPENG     XIE YANG     XIAO RENQIN     GAN LIN     WU XIAOMENG     YAN YEHUI     CHI XIANBIN     WANG KUN     DUAN XIAO     DING BO     WANG YUFEI     SONG CHANGZHE     WANG BOZHE     YAN HAIPING","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","F42B15/00    F42B15/01    G05D1/08","","CN20161102622","20160225","CN20161102622 20160225","US4798141 (A)    US7687025 (B2)    CN102530267 (A)    US2012227374 (A1)    CN102717900 (A)    CN104675562 (A)    CN105099504 (A)    CN105370440 (A)","","","","","","","","","","","","",""

Near space satellite launching platform and method,"CN105819002 (A)","2016-08-03","CAO HONGWEI     FAN KAICHUN     DUAN XIANGJUN     RAO TIANLIANG     FANG WANGLIN     HAO LINGYUN     ZHANG MEINING","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","B64G1/00","","CN20161226663","20160408","CN20161226663 20160408","","","","","","","","","","","","","",""                                                         

Image correction method and system of navigation height errors,"CN105825517 (A)","2016-08-03","WANG CHUNLIAN     JIN MIN     CHEN SHUTAO     XIE XIAOMIN     SHEN ZHI","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","G06T7/00    G01C25/00    G06K9/46    G06K9/62","","CN20161195049","20160331","CN20161195049 20160331","","","","","","","","","","","","","",""                                                      

Single-power-source single-point-locking three-stage synchronous unfolding device,"CN105644811 (A)","2016-06-08","LI YUNFENG     FAN KAICHUN     MA WEI     WU YONG     CHENG CHANG     ZHANG ZHOUZHOU     CHEN QINGWEI","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","B64G1/64","","CN20161185733","20160329","CN20161185733 20160329","JPH02160494 (A)    US5040748 (A)    JPH0763245 (A)    CN102102701 (A)    CN103625656 (A)","","","","","","","","","","","","",""                                             

Multifunctional platform device used for parking, overturning and transferring of aircraft cabin,"CN105644806 (A)","2016-06-08","DAI ZHAOPENG     WANG BOZHE     BAO YONGDING     XIN AO     FAN KAICHUN     YANG PAN","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","B64F5/00","","CN2016104582","20160106","CN2016104582 20160106","US2008011932 (A1)    EP2221151 (A2)    US2012228839 (A1)    CN203365162U (U)    CN104097789 (A)","","","","","","","","","","","","",""                                                

Heterogeneous optical scene matching target template based performance assessment system and method,"CN105740913 (A)","2016-07-06","ZHONG HUA     CUI JUN     WANG PINXI     LI JIAO     CHEN SHUTAO     JIN MIN     GUO CHENYU     YANG KAIXIN     CHEN JIE     WU FENGYANG","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","G06K9/62","","CN20161101879","20160225","CN20161101879 20160225","","","","","","","","","","","","","",""                                                

Missile warhead,"CN105509576 (A)","2016-04-20","CAO HONGWEI     RAO TIANLIANG     FANG WANGLIN","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","F42B15/00    F42B15/01","","CN20151821161","20151119","CN20151821161 20151119","DE202004010194U (U1)    GB2430994 (A)    JP4462735B (B2)    US8084724 (B1)    EP1714105 (B1)","","","","","","","","","","","","",""                                                      

Method for measuring installation errors of star sensor and strapdown inertial measurement unit of aircraft,"CN105424060 (A)","2016-03-23","WANG YAJUN     ZHOU HAI     LI CHUNQUAN     WANG YONG     LU ZHUANGZHI","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","G01C25/00","","CN20151794566","20151118","CN20151794566 20151118","","","","","","","","","","","","","",""                                                               

Optical fiber inertia measurement combined device,"CN105424039 (A)","2016-03-23","GAO BO     HU ZHENLIN     LU JUNQING     LIU YUANYUAN     LYU JIANGTAO     YUAN HUIZHENG     YANG YUANXIA     WANG ANDI     DAI SHILONG","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","G01C21/16    G01C25/00","","CN2016105780","20160106","CN2016105780 20160106","","","","","","","","","","","","","",""                                                

Multi-degree-of-freedom stage-separation test device and test method,"CN105416617 (B)    CN105416617 (A)","2016-03-23","LIANG JIQIU     CHEN BO     LIU XIAOLEI     XIANG BIN     HU CHANGWEI     HUANG LEI     WANG BOZHE     PENG WEI     WU JIHUA     HU SHI     CHEN XU","THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD","B64G7/00","","CN20151777730","20151114","CN20151777730 20151114","JPH0664598 (A)    RU2385445 (C1)    CN102050230 (A)","","","","","","","","","","","","",""                                    
« Last Edit: August 25, 2017, 03:30:44 pm by antigravite »
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Offline antigravite

  • CLEARANCE: Top Secret
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... I miss Aotian project related news.

Hmmm...

A.
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