Tophe said:In the Trait d'Union #208 (Mar-Apr 2003): "in 1934, someone named Goudant designed a flying boat with variable area wing. Two half wings (of 6.25m x 2m) disappear inside the the thick wing. 4 engines, speed near 300km/h, not built."
avion ancien said:... Maybe if Flight had featured it, the translation would have been Three Comrades!
Jemiba said:The answer is completely in the article, you posted:
Maurice Paltz was an aviation engineer, who worked for Guerchais-Roche and Holste and
proposed those 2, or better one-and-a half designs, intended for amateur construction and
designed for easy building. And both designs differed in wing only, the fuselage was the same.
avion ancien said:Curiously the TU index for issues 1 to 266 contains no mention of Durandeaux and the D.510 or DS.10 and Pierre Gaillard's book is succinct in the extreme in describing it as an amateur built light aeroplane dating from about 1945 (with no illustration). I wonder whether it was realised?
hesham said:From Ailes 10/1945,
here is a DS.10, a low-wing light monoplane Project as I suggest,created by J. Durandeaux,
in the book; Les Avions Francais 1944-1964,he designed a light aircraft called D.510,or
maybe it was a misprint and they meant DS.10 and they saw the letter "S" as the number
"5" ?!.
hesham said:It was actually built,from Ailes 12/1945.
hesham said:here is the Jean Simon unknown helicopter project,there's no sign for this design
on Internet.
http://gallica.bnf.fr/ark:/12148/bpt6k65560687/f2.image
In 1932 Jean Simon patented a
boundary layer control device
called "turbo-rotor." This device consisted in adapting a turbo-rotor to
paddle or vane, mechanically driven, positioned at the center of
running over the entire span of the wing.
The air circulating on the extrados was sucked in and
repressed on the underside. Several provisions
of the idea were patented and a demonstrator was tested at the wind tunnel of
STAé in Issy-les-Moulineaux in May 1933
under the direction of the Chief Engineer
Lapresle. Built at Zodiac, on the
plans of Simon, this wing of experience
was constituted by a rectangular plane
thick profile: box construction
wood, duralumin rotor, mounting on ball rollings and steel bearings. The
motive power was given by two compressed air turbines placed at each end of the rotor. The dimensions were:
length of 1,430 m; profile depth
297 mm; 53 mm thick; total thickness with the rotor of 90 mm (the rotor exceeded under the intrados).
The tunnel tests demonstrated
especially that the rotor had to turn to a
extremely high speed. In the
it could not exceed 3,000 tr/mn,
which proved very insufficient, the aspiration
at the extrados then being almost zero. he
should have reached a speed of at
minus 8 500/9 000 tr/mn, which was not
possible with compressed air turbines.
Wonder if there is some joke in that piece: "Le Trouffion" is French military slang for "the low-rank soldier"...
Thank you my dear Jemiba,
The W. Margoulis was designed in 1922 tilt-propeller triplane,and powered
by two 320 hp ABC Dragonfly engines,mounted between the top two wings
and remained a project.
here is the Maurice Brion fighter,it was a single seat fighter biplane,and put the
upper wing behind the cockpit to make a good vision for the pilot,the aircraft
mention in Les Ailes journal and in Trait d'Union magazine also,may be intended
for 1930 C.1 contest,we know about 31 to 32 entries competed in this competition,
many of them remained a drawing board only.
http://gallica.bnf.fr/ark:/12148/bpt6k65537145/f6.image