GB191323471A - Improvements in Aerial Vehicles. - Google Patents

Improvements in Aerial Vehicles.

Info

Publication number
GB191323471A
GB191323471A GB191323471DA GB191323471A GB 191323471 A GB191323471 A GB 191323471A GB 191323471D A GB191323471D A GB 191323471DA GB 191323471 A GB191323471 A GB 191323471A
Authority
GB
United Kingdom
Prior art keywords
plane
shock
car
machine
air
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
Inventor
Alexis Beurrier
Edouard Jean Bigourdan
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Application granted granted Critical
Publication of GB191323471A publication Critical patent/GB191323471A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/06—Aircraft not otherwise provided for having disc- or ring-shaped wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
    • B64C29/0025—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being fixed relative to the fuselage

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)

Abstract

23,471. Beurrier, A., and Bigourdan, E. J. Oct. 16, 1912, [Convention date]. Aerial machines without aerostats; planes, construction and arrangement of ; cars ; parachutes ; wind-deflecting screens.- An aerial machine is provided with an oval annular plane a of truncated conical form at the back and sides and flat at the front part. Lifting-propellers a<2> are arranged in the opening in the plane, and driving- propellers d are placed at the rear. An elevator g and a trapezoidal-shaped spring-controlled plane c are mounted on the plane a. The car i is tapered at the front and fitted above with a wind-screen i<1>. Shock-absorbing means are fitted below the car, through the sides of which surfaces k, shaped as sectors of a cone, are protruded when the engine fails, and the machine descends as a parachute. Steering and propelling.-A trapezoidal plane c is connected by springs to arms secured to the plane a so as to oscillate and stabilize the machine. Conical sector surfaces k with the concave surface underneath are pivoted at the point k<1>, Fig. 5, to the floor of the car and inclined rearwardly at about 45 degrees. They are protruded by jointlyoperated pinions m and racks l<1> to cause the machine to descend obliquely. An elevator g and rudder h are provided. A lifting - propeller system a<2> is mounted in the opening in the plane a, and a driving-system d is mounted at the rear and is carried by arms f sliding on rods e so that the point of application of the propeller thrust may be raised or lowered. Shock of landing, deadening.-The landing-frame n is provided with wheels o supported by links hinged at p to the car, and the axle of the wheels is connected by arcuate rods o<2> to a buffer p<1> composed of plates interleaved with leather, india-rubber, cork, &c., a spring o<3> also serving to deaden the shock. The air in telescopic tubes t and in a chamber q is compressed after the shock has been taken by the springs o<3>. The chamber q and piston u are made of blocks of resilient material with air spaces between. Air vents s are made in the tubes t and the air chambers.
GB191323471D 1912-10-16 1913-10-16 Improvements in Aerial Vehicles. Expired GB191323471A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR191323471X 1912-10-16

Publications (1)

Publication Number Publication Date
GB191323471A true GB191323471A (en) 1914-08-07

Family

ID=32339937

Family Applications (1)

Application Number Title Priority Date Filing Date
GB191323471D Expired GB191323471A (en) 1912-10-16 1913-10-16 Improvements in Aerial Vehicles.

Country Status (1)

Country Link
GB (1) GB191323471A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2474079A (en) * 1944-09-08 1949-06-21 Harry Waldman Rotating wing for aircraft

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2474079A (en) * 1944-09-08 1949-06-21 Harry Waldman Rotating wing for aircraft

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