GB476598A - Flying machine - Google Patents

Flying machine

Info

Publication number
GB476598A
GB476598A GB16474/36A GB1647436A GB476598A GB 476598 A GB476598 A GB 476598A GB 16474/36 A GB16474/36 A GB 16474/36A GB 1647436 A GB1647436 A GB 1647436A GB 476598 A GB476598 A GB 476598A
Authority
GB
United Kingdom
Prior art keywords
airscrew
rotor
reactionary
wing
engine
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
GB16474/36A
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
Publication of GB476598A publication Critical patent/GB476598A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters

Abstract

476,598. Aircraft provided with rotarywing systems. NAGLER, B. June 12, 1936, No. 16474. - Convention date, Feb. 8. [Class 4] A flying-machine comprises a normally autorotative rotary-wing system or rotor 5 adapted to be tilted, and an airscrew 3 driven during starting by a common engine 2, means, e.g. a variable pitch airscrew or a changespeed gear in the airscrew drive, being provided for varying the proportion of power transmitted from the engine to the rotor and airscrew ; two surfaces extend in the direction of the airscrew slipstream, one of the surfaces 10 being fixed and being adapted to counteract the airscrew reactionary torque, and the other 11 being adjustable to produce a reactionary couple about the rotor axis. The rotor drive includes a free-wheel coupling and the rotor is mounted on a universal joint 7. The surface 10 is formed by giving a wing-like cross-section to a fairing surrounding the rotor supporting- structure.
GB16474/36A 1936-02-08 1936-06-12 Flying machine Expired GB476598A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
AT476598X 1936-02-08

Publications (1)

Publication Number Publication Date
GB476598A true GB476598A (en) 1937-12-13

Family

ID=3674854

Family Applications (1)

Application Number Title Priority Date Filing Date
GB16474/36A Expired GB476598A (en) 1936-02-08 1936-06-12 Flying machine

Country Status (1)

Country Link
GB (1) GB476598A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2547255A (en) * 1942-12-05 1951-04-03 Bruel Andre Aime Lucien Helicopter with automatic antitorque vane

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2547255A (en) * 1942-12-05 1951-04-03 Bruel Andre Aime Lucien Helicopter with automatic antitorque vane

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