Haerens FF.6

Acquisition from Spain of five 150hp Hispano-Suiza eight-cylinder Vee-type engines prompted the Norwegian Army Flying-Service (Haerens Flyvevaesen) to order the design of a single-seat fighter around this power plant.

Design was begun by Ing Hellesen at the Kjeller Flyfabrikk in the autumn of 1919, by which time the requirement had changed to that of a two-seat fighter-reconnaissance aircraft. Of wooden construction with a plywood monocoque fuselage and designated FF 6 by the factory and T.2 by the Army, the prototype was flown in 1921.

It immediately displayed unacceptable characteristics which were exacerbated by the fact that the Hispano-Suiza engine was found to develop only 103hp. A max speed of only 100km/h was attained compared with an anticipated maximum of 132km/h. Further development was therefore abandoned after the first test flight.

Engine: 150 hp Hispano-Suiza 8
Wingspan: 11.75 m / 39 ft 7 in
Length: 7.25 m / 24 ft 9 in
Height: 3.57 m / 12 ft 9 in

Gwinn Aircar

The first Aircar was completed in 1937 when it also received its Approved Type Certificate.
The test pilot for the Air Car was Richard K. Benson. During one flight he inadvertently got the Air Car into a spin and at about 10,000 feet and was able to recover at about 1000 feet. Saving the airframe got him a $10,000 reward from Gwinn.

Engine: 2 x Pobjoy Niagara II.
Seats: 2.
Top speed: 118 mph.
Cruise: 103 mph.
Landing speed: 41 mph.

Guyot et Verdier 1911 biplane

In 1911, in Juvisy in Essonne, construction of a 4th biplane started but with monocoque metal fuselage on wheels with shock absorbers, the hull joining the front cell to the aft stabilizer adjustable, a rear stabilizer in two parts to allow the development of the rudder with a crutch for ground braking. Combination of ailerons with controls on joystick, 60 hp E.N.V motor, Regy tractor propeller, foot rudder control, upper plane span of 8 meters, and lower plane 7 meters.

Louis Verdier carried out the development and flight tests in presence of an officer from the military aeronautical laboratory of Chalais-Meudon in view of the use of this two-seater by the army.

In view of the results obtained, including the solidity of the aircraft, well built, good flight behavior, possibility of landing on very short terrain due to the solidity of its landing gear, a very soft suspension and good braking at
ground, the Guyot-Verdier airplane registered before January 1, 1911 in the 1st major military aviation competition in Reims in la Marne, which began on October 1, 1911.

42 manufacturers take part in this competition, registering around 70 machines. Unfortunately, the Guyot-Verdier aircraft does not meet the qualifications, the required conditions are too stringent.

On Sunday, October 29, 1911, Louis made a demonstration flight of in front of 4000 to 6000 spectators, in the field Berthonnerie Air Force (2 km from La Souterraine), flying for 35 minutes, completing a 35 km circuit where it reaches an altitude of 500 meters. He is carried in triumph in the streets of the city and a wine of honor is offered.

Then follow other flights and aerial celebrations, in November 1911, January 12, 1912, April 28, 1912 in Azérables in Creuse.

In 1912, Louis received his pilot’s license n° 526, from the aeronautical sports commission.

In 1913, Louis Verdier wrote:
“Despite all these facts and qualities as well as many steps taken by our gentlemen, Deputies and Senators of Creuse and Haute-Vienne, the La Souterraine aviation factory has never obtained any order of a military service from the French State, nor any financial aid, all this aviation equipment has been studied, built and developed to no avail, for it was not the few parties and exhibitions that were able to cover all these study and construction costs for these aircraft prototypes. I give up building and flying these planes, I leave the provinces and return to the Paris region”

Louis entered the Sanchez-Beza Establishments as a pilot, then as a test pilot and engine developer at the Salmson aviation factories in Billancourt and, with mechanics, replaces engines on seaplanes in Saint-Raphaël (Var), Bizerte (Tunisia), Marseille (Bouches-du-Rhône), Toulon (Var).

Guyot et Verdier 1910 biplane

Henri Guyot and Louis Verdier undertake, still at La Souterraine, the construction of a third biplane, two-seater, at Chauvière, 80 horsepower engine and pusher propeller, unequal span wings.

The front cell and the rear fixed plane are joined by V-shaped ash spars and to reduce resistance in flight, the masts and metal parts are profiled. The span of the upper plane is 17.50 meters and the span of the lower plane 15 meters, bearing surfaces with beak entry into the air profiled to avoid resistance to the advancement of the aircraft, the engine mounted on a fuselage which is fixed on the lower plane of the aircraft which constitutes the cockpit. The cell is mounted on skid with 4 shock absorbers metal fixed on two wheels on each runner. The wheels are mounted on balloon tires with bead rims, brakes on wheels and brake stand on the ground.

The first official flight, piloted by Louis, took place on April 24, 1910 at Le Dorat on the flat racecourse. It was completely fenced which facilitated the control of entries because the event was paying. It’s a rectangle of 50 meters by 60 meters, the aircraft can take off in all directions.

Louis passed his A.C.F. (Aéro-Club de France) on July 1, 1911 on this Guyot-Verdier aircraft. His pilot’s license civil bears the n° 538. The license n°1 was obtained in 1909 by Louis Blériot.

Guillon and Clouzy 1907 biplane

Standing on three bicycle wheels and with wings twenty feet across, Mr. Guillon’s “airship” had a 20 hp engine drive the propeller, which was five feet long and made of aluminium. The total weight of the machine was 300 lb., and with Mr. Guillon on board, reclining in a sloping position of 45 degrees at the back, the weight was 420 lb. When tested at Epsom Downs, Surrey, UK, on 11 April 1907, the aeroplane started away at a good twenty miles an hour, but Mr. Guillon could not get the engine to work satisfactorily, and the machine failed to rise from the ground. Furthermore, the rudder did not seem to act properly, darting this way and that. The aeroplane kept the crowd of some fifty persons constantly running to keep out of danger. Six unsuccessful trials were made, then the axle was found to be bent, and the experiment came to an end.