Turkish engines, power packs and propulsion projects

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With the increased effort of Turkey to develop various domestic vehicles and missiles. Turkey has also decided to exert effort into developing engines, power packs and propulsion systems to power and propel them.

There are currently Five prominent engine manufacturers in Turkey;

  • BMC POWER
  • TUMOSAN
  • FORD-OTOSAN
  • TEI
  • KALE AERO

BMC POWER

TTZA
is an Inline 4 cylinder turbo diesel engine with expected power output of 350hp
TTZA.jpg

AZRA is an inline 6 cylinder turbo diesel engine with expected power output of 550hp
AZRA.jpg

UTKU is an V configured turbo diesel engine with 8 cylinder with expected power output of 950hp
UTKU.jpg

BATU is an V configured turbo diesel engine with 12 cylinder with an expected power output of 1450hp
BATU.jpg


TUMOSAN

S8000-4 is an inline 4 cylinder turbo diesel engine with output of 115hp
upload_2020-1-24_18-25-7.jpeg

S8000-6 is an inline 6 cylinder turbo diesel engine with output of 175hp
upload_2020-1-24_18-26-15.jpeg

TMSN 5.5 is a inline 4 cylinder turbo diesel engine with output of 360hp
upload_2020-1-24_19-7-35.jpeg

TMSN 7.5 inline 6 cylinder turbo diesel engine with output of 530hp
upload_2020-1-24_19-52-21.jpeg

TMSN V8 is V configured turbo diesel engine with 8 cylinder with output of 750hp
upload_2020-1-24_19-43-7.png

FORD-OTOSAN

Ecotorq inline 6 cylinder turbo engine with outputs of 325-470hp
motor.jpg

Duratorq inline 4 cylinder turbo diesel engine with output of 155hp
urettigimizmotorlar7.jpg

TEI

TEI-PD222 is a inline 4 cylinder turbo diesel aviation engine with output of 220hp
1580729417_tei-pd170.png

TEI-PD170 is a inline 4 cylinder turbo diesel aviation engine with output of 172hp
1581686781_pd170web.png


TEI-PG30/40/50 is a 2 cylinder gasoline boxer type engine with 30, 40 and 50hp
1581687368_pg50web.png
 
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TEI

TEI-TS1400 is a turbo shaft engine with output of 1400shp
EV18N4hXYAAISyH.jpg

TEI-TJ300 is a turbojet engine with a thrust of 1.3Kn / 290lb
Untitled-1.jpg

KALE AERO

KTJ-3200 is a turbojet engine with a thrust of 3.2Kn / 720lb
DnhrPnVWsAA-5Bc.jpg
 
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TRMOTOR

Supposedly in development within a consortium of three companies (BMC Power - TAI - SSTEK). This turbofan engine is envisaged to power TFX.

Thrust requirement of max thrust 120 kN (27,000 lb) to power TFX
ee7d077f3b476a3.jpg
 
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TÜLOMSAŞ

TLM6 is an V configured 6 cylinder turbo diesel engine with output of 1000hp
tulomsas-1000-hp-gucundeki-milli-dizel-motoru-uretti_std.original.jpg



TLM 16V 185 is an V configured 16 cylinder turbo diesel engine with output of 2400hp
unnamed.png
 
Domestically produced Super-alloys turbine blades
Foundry < to > Final product
Untitled-1.jpg
To further add - blades are reported to be 3rd generation single crystal nickel super-alloy and will be used for TEI-TS1400 engines being developed to power Gokbey T-625.
 
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Air Independent Propulsion proposed for 'MILDEN' - Turkey's domestic submarine project

This article gives an overview related to stealth submarine propulsion system, in particular recently being developed by IdeaLab, closed loop Supercritical Carbon Dioxide (sCO2) Brayton power cycle based Air Independent Propulsion (AIP).

AIP allows a submarine to run its electric motor and other electrical systems without using the batteries. It reduces the frequency with which the submarine has to put its mast above the surface to suck in air for the diesel engines to recharge the batteries. The submarine still has to snort for brief periods on most days in order to ventilate, but is much less exposed than conventional diesel-electric submarines. During operations, if the tactical situation prohibits ventilation then the submarine can delay snorting for much longer than normal. And it can revert to lighting oxygen candles (or equivalent) in dire situations. Therefore the submarine can remain submerged for much longer, giving the submarine commander much greater flexibility. There are currently over 50 AIP submarines in service around the world, with the number likely to double in the coming decade.

Let’s discuss and compare IdeaLab’s new sCO2 Brayton power cycle AIP with existing technologies. We will describe sCO2 Brayton power cycle based AIP system in detail and provide brief discussion on existing technologies.

What is Supercritical CO2?
Supercritical CO2 is a fluid state of carbon dioxide where it is held above its critical point (i.e., critical pressure and temperature). The density at that point is similar to that of a liquid and allows for the pumping power needed in a compressor to be significantly reduced, thus significantly increasing the thermal-to-electric energy conversion efficiency.

The IdeaLab Solution
Basically, IdeaLab is developing a thermal-to-electric power conversion technology in a configuration called the recompression closed Brayton cycle (RCBC) that uses supercritical carbon dioxide as the working fluid, rather than steam, thereby dramatically increasing conversion efficiency compared to the steam Rankine cycle.

The primary reason for improved power conversion efficiency is simply that the use of sCO2 as the working fluid in a Brayton cycle requires less work to convert a given thermal input to electricity. In general, increased efficiency represents increased output for the same thermal input, regardless of the thermal source (natural gas, nuclear, solar or coal). Where fuel costs are a significant portion of overall costs (coal and natural gas fired plants), the benefit is reduced fuel costs. Where capital investments are high (nuclear and concentrating solar power), the benefit is increased output for the initial investment.


img_4128.png



IdeaLab sCO2 Power Cycle Benefits as AIP
IdeaLab sCO2 AIP power conversion technology offers a number of benefits over competing AIP Technologies. Most important of all is having 25% higher volume power density (Figure 1) makes IdeaLab AIP power system a strong candidate while the weight stays half of the competing AIP technologies such Fuel Cell and Stirling (Figure 2).

Other benefit is increased efficiency (resulting in increased electricity/power production for same thermal input) due to using sCO2 that provides extra 7 points compared to close challenger fuel cells (Figure 3).

IdeaLab sCO2 AIP system consists of high pressure piping loop that allows depths of 1200 m without any other CO2 disposal pump system on board. Excess CO2 can be stored in vessel if desired.

IdeaLab sCO2 AIP power module is capable of providing up to 4MW electric power. Traction system could be configured so that 4MW burst of energy can be directed to drive system. This is serious advantage over other existing AIP technologies that has limited low speeds due to maximum power drainage problems.

Due to innovative hybrid catalytic combustion chamber; diesel, JP-8 or liquefied natural gas can be used as fuel. Based on conceptual mission analysis, with 100 tons of diesel fuel, sCO2 AIP system could potentially stay submerged 90 days and provide 20,000 km mission range between refuels. This unsurpassed capability compared to existing AIP technologies gives a conventional submarine nuclear-submarine like potency and stealth. Also having high speed turbomachinery as an inherent design future mutes all the noise concerns that a diesel or stirling engine has.

Challenges
All these benefits brings up new challenges as well. Before the benefits of sCO2 AIP power cycle can be realized, it must be shown to be ready and reliable. In concert with the Undersecretaries for Defence Industries (SSM), IdeaLab has been conducting research and development to deliver a technology that is ready for field implementation. In fact, IdeaLab has adopted the following mission statement “By the end of FY 2018, IdeaLab shall develop a fully operational up to 1 MWe R&D Demonstration sCO2 Brayton Power Conversion System that will allow the systematic identification and retirement of technical risks and testing of components for the marine application of this technology.” Ongoing activities in support of that mission include:

  • Confirm viability of existing components (bearings and gas seals) and suitability of materials,
  • Accommodate a wide range of operating parameters and applications,
  • Integrate and scale up existing technologies into a new application, and
  • Develop robust operating procedures for operating at critical point.
Future Applications
sCO2 power cycles are potentially applicable to a wide variety of power-generation applications. Nuclear power, concentrated solar thermal, fossil fuel boilers, geothermal, and floating shipboard propulsion systems have all been identified as favourable applications for sCO2 cycles and would replace traditional steam Rankine cycles.

We will end this article by discussing briefly competing existing technologies.

Stirling Engines
The original Stirling Engine was patented in 1816 by British engineer Robert Stirling as a rival to the steam engine. Although successful, it was largely replaced by the electric motor in the early 1900s and almost forgotten, until the Swedes looked for clever ways to propel a submarine. The engine’s heat is produced in a combustion chamber but it is separated from the actual engine. The heat is transferred to the engine’s working gas (e.g. oxygen), operating in a completely closed system. The working gas forces the pistons in the engine to move, thus producing mechanical energy. Although Stirling engines are well tested and simple, they are relatively bulky, comparatively noisy due to moving parts. Limits the submarine’s operating depth to about 200 m when in use.

Fuel Cells
Fuel cells mix oxygen with a hydrogen-rich chemical to produce an electric current. Fuel cells use an electrochemical reaction in which oxygen and a hydrogen-rich fuel combine to form water, and electricity. Unlike internal combustion engines, the fuel is not combusted. Instead the energy is released electrocatalytically. Fuel Cell AIP was developed in the 1980s for the German Navy. The main system in use today is the German designed Seimens PEM (Polymer Electrolyte Module), but Indian and American firms also supply them for AIP submarines. Fuel cells have a high power density and generally provide the longest endurance of current AIP systems. They are very quiet and the technology is seen as offering further potential. Major downside is Fuel cells are being expensive and complex.

MESMA
MESMA is a French system which runs a steam turbine off the chemical reaction between ethanol and oxygen. In many respects the system is based on the nuclear propulsion but with an alternative heat source. Only Pakistan fields this type of AIP currently. MESMA has a high power output potentially allowing greatest underwater speed but it is relatively thirsty, noisy and has complex plumbing.

Power to Volume;
Most important of all is having 25% higher volume power density (Figure 1)
Q7PWaA.jpg



Power to weight;
Weight half of the competing AIP technologies such Fuel Cell and Stirling (Figure 2).
XXbJ0o.jpg


Power production efficiency;
Other benefit is increased efficiency (resulting in increased electricity/power production for same thermal input) due to using sCO2 that provides extra 7 points compared to close challenger fuel cells (Figure 3).
bGvYrY.jpg



Size comparison
AAOZLFOTO_11816716_040520171144250000_D_GEN_20170504000000_aa-picture-20170504-11816716.jpg



Model

aL6yP4.jpg
 
KALE KTJ-3200 | Turbojet engine for SOM cruise Missile and Atmaca AShM - Qualifications tests to end this year in December and production to begin next year. Will replace French Microturbo TR-40.
3.2kn of thrust / 900hp
1ad58a03-d02a-4b01-b5f8-8372180c4ae5_2.jpg
1ad58a03-d02a-4b01-b5f8-8372180c4ae5_12.jpg
 
Last edited:
Two TS1400 engines delivered to TAI to power domestic multirole helicopter
Project started in 2017, 2020 delivered engines for integration.
Capture3.PNG
 
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Air Independent Propulsion proposed for 'MILDEN' - Turkey's domestic submarine project

This article gives an overview related to stealth submarine propulsion system, in particular recently being developed by IdeaLab, closed loop Supercritical Carbon Dioxide (sCO2) Brayton power cycle based Air Independent Propulsion (AIP).

AIP allows a submarine to run its electric motor and other electrical systems without using the batteries. It reduces the frequency with which the submarine has to put its mast above the surface to suck in air for the diesel engines to recharge the batteries. The submarine still has to snort for brief periods on most days in order to ventilate, but is much less exposed than conventional diesel-electric submarines. During operations, if the tactical situation prohibits ventilation then the submarine can delay snorting for much longer than normal. And it can revert to lighting oxygen candles (or equivalent) in dire situations. Therefore the submarine can remain submerged for much longer, giving the submarine commander much greater flexibility. There are currently over 50 AIP submarines in service around the world, with the number likely to double in the coming decade.

Let’s discuss and compare IdeaLab’s new sCO2 Brayton power cycle AIP with existing technologies. We will describe sCO2 Brayton power cycle based AIP system in detail and provide brief discussion on existing technologies.

What is Supercritical CO2?
Supercritical CO2 is a fluid state of carbon dioxide where it is held above its critical point (i.e., critical pressure and temperature). The density at that point is similar to that of a liquid and allows for the pumping power needed in a compressor to be significantly reduced, thus significantly increasing the thermal-to-electric energy conversion efficiency.

The IdeaLab Solution
Basically, IdeaLab is developing a thermal-to-electric power conversion technology in a configuration called the recompression closed Brayton cycle (RCBC) that uses supercritical carbon dioxide as the working fluid, rather than steam, thereby dramatically increasing conversion efficiency compared to the steam Rankine cycle.

The primary reason for improved power conversion efficiency is simply that the use of sCO2 as the working fluid in a Brayton cycle requires less work to convert a given thermal input to electricity. In general, increased efficiency represents increased output for the same thermal input, regardless of the thermal source (natural gas, nuclear, solar or coal). Where fuel costs are a significant portion of overall costs (coal and natural gas fired plants), the benefit is reduced fuel costs. Where capital investments are high (nuclear and concentrating solar power), the benefit is increased output for the initial investment.


img_4128.png



IdeaLab sCO2 Power Cycle Benefits as AIP
IdeaLab sCO2 AIP power conversion technology offers a number of benefits over competing AIP Technologies. Most important of all is having 25% higher volume power density (Figure 1) makes IdeaLab AIP power system a strong candidate while the weight stays half of the competing AIP technologies such Fuel Cell and Stirling (Figure 2).

Other benefit is increased efficiency (resulting in increased electricity/power production for same thermal input) due to using sCO2 that provides extra 7 points compared to close challenger fuel cells (Figure 3).

IdeaLab sCO2 AIP system consists of high pressure piping loop that allows depths of 1200 m without any other CO2 disposal pump system on board. Excess CO2 can be stored in vessel if desired.

IdeaLab sCO2 AIP power module is capable of providing up to 4MW electric power. Traction system could be configured so that 4MW burst of energy can be directed to drive system. This is serious advantage over other existing AIP technologies that has limited low speeds due to maximum power drainage problems.

Due to innovative hybrid catalytic combustion chamber; diesel, JP-8 or liquefied natural gas can be used as fuel. Based on conceptual mission analysis, with 100 tons of diesel fuel, sCO2 AIP system could potentially stay submerged 90 days and provide 20,000 km mission range between refuels. This unsurpassed capability compared to existing AIP technologies gives a conventional submarine nuclear-submarine like potency and stealth. Also having high speed turbomachinery as an inherent design future mutes all the noise concerns that a diesel or stirling engine has.

Challenges
All these benefits brings up new challenges as well. Before the benefits of sCO2 AIP power cycle can be realized, it must be shown to be ready and reliable. In concert with the Undersecretaries for Defence Industries (SSM), IdeaLab has been conducting research and development to deliver a technology that is ready for field implementation. In fact, IdeaLab has adopted the following mission statement “By the end of FY 2018, IdeaLab shall develop a fully operational up to 1 MWe R&D Demonstration sCO2 Brayton Power Conversion System that will allow the systematic identification and retirement of technical risks and testing of components for the marine application of this technology.” Ongoing activities in support of that mission include:

  • Confirm viability of existing components (bearings and gas seals) and suitability of materials,
  • Accommodate a wide range of operating parameters and applications,
  • Integrate and scale up existing technologies into a new application, and
  • Develop robust operating procedures for operating at critical point.
Future Applications
sCO2 power cycles are potentially applicable to a wide variety of power-generation applications. Nuclear power, concentrated solar thermal, fossil fuel boilers, geothermal, and floating shipboard propulsion systems have all been identified as favourable applications for sCO2 cycles and would replace traditional steam Rankine cycles.

We will end this article by discussing briefly competing existing technologies.

Stirling Engines
The original Stirling Engine was patented in 1816 by British engineer Robert Stirling as a rival to the steam engine. Although successful, it was largely replaced by the electric motor in the early 1900s and almost forgotten, until the Swedes looked for clever ways to propel a submarine. The engine’s heat is produced in a combustion chamber but it is separated from the actual engine. The heat is transferred to the engine’s working gas (e.g. oxygen), operating in a completely closed system. The working gas forces the pistons in the engine to move, thus producing mechanical energy. Although Stirling engines are well tested and simple, they are relatively bulky, comparatively noisy due to moving parts. Limits the submarine’s operating depth to about 200 m when in use.

Fuel Cells
Fuel cells mix oxygen with a hydrogen-rich chemical to produce an electric current. Fuel cells use an electrochemical reaction in which oxygen and a hydrogen-rich fuel combine to form water, and electricity. Unlike internal combustion engines, the fuel is not combusted. Instead the energy is released electrocatalytically. Fuel Cell AIP was developed in the 1980s for the German Navy. The main system in use today is the German designed Seimens PEM (Polymer Electrolyte Module), but Indian and American firms also supply them for AIP submarines. Fuel cells have a high power density and generally provide the longest endurance of current AIP systems. They are very quiet and the technology is seen as offering further potential. Major downside is Fuel cells are being expensive and complex.

MESMA
MESMA is a French system which runs a steam turbine off the chemical reaction between ethanol and oxygen. In many respects the system is based on the nuclear propulsion but with an alternative heat source. Only Pakistan fields this type of AIP currently. MESMA has a high power output potentially allowing greatest underwater speed but it is relatively thirsty, noisy and has complex plumbing.

Power to Volume;
Most important of all is having 25% higher volume power density (Figure 1)
Q7PWaA.jpg



Power to weight;
Weight half of the competing AIP technologies such Fuel Cell and Stirling (Figure 2).
XXbJ0o.jpg


Power production efficiency;
Other benefit is increased efficiency (resulting in increased electricity/power production for same thermal input) due to using sCO2 that provides extra 7 points compared to close challenger fuel cells (Figure 3).
bGvYrY.jpg



Size comparison
AAOZLFOTO_11816716_040520171144250000_D_GEN_20170504000000_aa-picture-20170504-11816716.jpg



Model

aL6yP4.jpg

Most of the times when i read something about supercritical co2 turbines it was as a power conversion system for molten salt reactors. What is the heat source in this application ? Burning diesel without oxygin ?
 
TEI General Manager Prof. Dr. Mahmut F. Akşit said, “Production of the second engine of TEI-TS1400 has been completed. In the coming weeks, the testing process of the second engine will begin. Our third engine assembly will be completed in 1.5 months. We will produce at least five TS1400 engines in the next six months. ”

Serial production of TS1400 Gas Turbine engine expected in 2024 - TEI CEO

View: https://twitter.com/C4Defence/status/1347520527959781379?s=20
 
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Second TS1400 engine has passed factory tests and will be transferred over to TAI to integrate it on-board T-625 Gokbey helicopter
View: https://www.youtube.com/watch?v=7abKCuPkQFU&feature=emb_title

5ffd56bf65ce7.jpg
This is Turkey's first Gas Turbine engine, yet it features single crystal nickel super alloy, cooling ducts within and ceramic coating on turbine blades also TEI is making use of various additive manufacturing techniques for one piece complex components.



TEI has been tasked to develop an engine for 10 ton helicopter project which will require +3000shp.
 
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BATU is an V configured turbo diesel engine with 12 cylinder with an expected power output of 1450hp
View attachment 637507
Slightly more detailed image of the 1450-1500hp BATU engine being developed for Altay MBT
1610415368730.jpeg

UTKU is an V configured turbo diesel engine with 8 cylinder with expected power output of 950hp
View attachment 637509
UTKU development of a 950-1000hp engine for Infantry fighting vehicles and self-propelled howitzers
3.jpg
 
Is the BATU engine based on the South Korean dv27k engine & S&T transmission. On other forums South Korean members reject the arrangement that it is license produced. They are adamant that the technology is only available off the shelf to the safeguard the technology. Can any Turkish brother confirm the arrangement, given that it is due to be tested this year- 2021?
 
BATU - Powerpack development for Altay MBT
yanma (1).png

It is a power group development project consisting of a 1500 HP engine, transmission and cooling package, developed from scratch by BMC POWER.
The V12 engine, which is the first 12-cylinder engine designed and developed by Turkish engineers, was successfully fired for the first time in 2021. Testing and qualification studies continue at the BMC POWER test centre.
In line with the 1500 HP engine, transmission with steering and braking capability and high torque transmission, high-efficiency chiller and multi-functional control unit development projects are carried out simultaneously within BMC POWER.

Property Table:
12 Cylinder - V Type Engine
27.3 L Combustion Volume
1500 HP Power
6+2 Cross Drive Transmission

First Ignition Footage
View: https://www.youtube.com/watch?v=CQCKOKfB0L4
 
BATU - Powerpack development for Altay MBT
View attachment 664660

It is a power group development project consisting of a 1500 HP engine, transmission and cooling package, developed from scratch by BMC POWER.
The V12 engine, which is the first 12-cylinder engine designed and developed by Turkish engineers, was successfully fired for the first time in 2021. Testing and qualification studies continue at the BMC POWER test centre.
In line with the 1500 HP engine, transmission with steering and braking capability and high torque transmission, high-efficiency chiller and multi-functional control unit development projects are carried out simultaneously within BMC POWER.

Property Table:
12 Cylinder - V Type Engine
27.3 L Combustion Volume
1500 HP Power
6+2 Cross Drive Transmission

First Ignition Footage
View: https://www.youtube.com/watch?v=CQCKOKfB0L4

BATU 1500hp first prototype engine. Many prototypes engines will be produced and will undergo testing and certifications process for 2-3 years before being ready for serial production and integration onto Altay MBT.
20210923_112357.jpg
 

KALE ARGE - KTJ-3200
1634730588739.png

KTJ-3200 has the ability to provide "Overthrust" thrust when the platform requires more thrust, churning up to 38-40,000 rpm.

KTJ-3200 Low-rate initial production deliveries are continuing in 2021, full-rate serial production is to begin at the start of 2022.

Based on current production plans, Kale ARGE will be able to produce 150 KTJ-3200 engines per year with the capability to expand production capacity.

---

KTJ-3200 will replace French TRI40 jet engine power Turkey's SOM Cruise Missiles and
SOM.jpg

ATMACA AShM and LACM
Atmaca-03-692x360.jpg
 

KALE ARGE - KTJ-3200
View attachment 666658

KTJ-3200 has the ability to provide "Overthrust" thrust when the platform requires more thrust, churning up to 38-40,000 rpm.

KTJ-3200 Low-rate initial production deliveries are continuing in 2021, full-rate serial production is to begin at the start of 2022.

Based on current production plans, Kale ARGE will be able to produce 150 KTJ-3200 engines per year with the capability to expand production capacity.

---

KTJ-3200 will replace French TRI40 jet engine power Turkey's SOM Cruise Missiles and
View attachment 666660

ATMACA AShM and LACM
View attachment 666659

Turkey is improving KTJ-3200 micro jet engine, increasing thrust and flight altitude. First test run of the prototype KTJ-3700 will happen in second quarter of 2022.

EngineThrustWeightFlight AltitudeSpeed
KTJ32003200N / 719lbf50kg16000 ft0.95 mach
KTJ37003700N / 831lbf50kg32000 ft0.95 mach

1650482215981.png

KTJ-1750 to power Cakir Mini Cruise Missile family, engine is stated to be completed by the third quarter of 2022.
EngineThrustWeightFlight AltitudeSpeed
KTJ17501750N / 393lbf17kg32000 ft0.95 mach

1650489727811.png
Cakir Mini Cruise Missile
1650489837201.png
 
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KTJ 3200 - powering ATMACA AShM and SOM Cruise Missile
KTJ-1750 - powering Cakir Mini Cruise Missile
1666820794463.png
 

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