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
GB3716664A
Inventor
Rolf Riccius
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.)
Vereinigte Flugtechnische Werke Fokker GmbH
Original Assignee
Vereinigte Flugtechnische Werke Fokker GmbH
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Filing date
Publication date
Application filed by Vereinigte Flugtechnische Werke Fokker GmbHfiledCriticalVereinigte Flugtechnische Werke Fokker GmbH
Priority to GB3716664ApriorityCriticalpatent/GB1074660A/en
Publication of GB1074660ApublicationCriticalpatent/GB1074660A/en
B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
B64C29/0091—Accessories not provided for elsewhere
Landscapes
Engineering & Computer Science
(AREA)
Aviation & Aerospace Engineering
(AREA)
Transmission Devices
(AREA)
Abstract
1,074,660. VTOL Aircraft. VEREINIGTE FLUGTECHMISCHE FRUEHER "WESER" FLUGZEUGBAU FOCKE-WULF HEINKELFLUGZEUGBAU G.m.b.H. Sept. 10, 1964, No. 37166/64. Heading B7G. A VTOL aircraft has one or more pairs of jet lift engines, the engines of each pair being arranged on opposite sides of the centre of gravity and the fuel pump of each is driven by the other so that if one engine fails the other does also and asymmetric lift is avoided., The engines may be in the fuselage or in wing- mounted nacelles.
GB3716664A1964-09-101964-09-10Cut-out arrangement for lifting power units of vtol aircraft
ExpiredGB1074660A
(en)
The c-142 role in coin air mobile operations(C-142 high-wing aircraft with four turboshaft engines and tilt-wing deflected slipstream to attain V/STOL capability in COIN operations)
Short takeoff of high-speed aircraft(Takeoff distance reduction in v/stol aircraft, taking into account thrust-velocity characteristics and engine tilt angle)
The dornier do 31 jet-lift concept, a light military transport with vtol capability(Jet lift concept in dornier do 31 aircraft, a light military transport with vtol capability)
Utilization of the kinetic energy of a turbojet-engine exhaust jet to create an additional lifting force on the aircraft wing(Turbojet engine exhaust kinetic energy utilization to create additional lift on wing, using static tests)
The impact of flight operating techniques upon engine maintenance costs(Flight operating techniques influence upon engine maintenance costs and new engine design, specifically Pratt and Whitney JT 3 C-12 on Boeing 720 aircraft)
Economics of propulsion systems for air transport. I(Air transport propulsion systems, discussing aircraft operating economics with reference to weight, size, powerplant efficiency, noise and air pollution)
Exploration of the effect of thrust and lift augmentation of the operating speed capability of a given helicopter rotor system/see accession no. a 63-14839, issue no. 10