GB461010A - Improvements in and relating to propulsive systems for aircraft - Google Patents

Improvements in and relating to propulsive systems for aircraft

Info

Publication number
GB461010A
GB461010A GB22448/35A GB2244835A GB461010A GB 461010 A GB461010 A GB 461010A GB 22448/35 A GB22448/35 A GB 22448/35A GB 2244835 A GB2244835 A GB 2244835A GB 461010 A GB461010 A GB 461010A
Authority
GB
United Kingdom
Prior art keywords
wing
stub
airscrew
shafts
fuselage
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
GB22448/35A
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
Priority to GB22448/35A priority Critical patent/GB461010A/en
Publication of GB461010A publication Critical patent/GB461010A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Details Of Gearings (AREA)

Abstract

461,010. Propelling aircraft. BAYNES, L. E. Aug. 8, 1935, No. 22448. [Class 4] A propelling system particularly for light aircraft comprises at least two lateral airscrews carried by a hollow stub wing which projects fixedly on opposite sides of the fuselage, and is adapted to carry extensions with which to form a supporting wing proper, each airscrew being driven by a power plant mounted at or adjacent the centre of the wing span through power transmission means situated in the stub wing. As applied to a high wing cantilever monoplane, wing 1 is detachable at joints 2 (in halves) from the top of the fuselage. A fixed stub wing 4 extends laterally on either side of the body and forwardly to main spar 5 of the wing proper. Stub wing 4 accommodates two airscrew shafts 6 journalled in bearings carried by spars 7, 8, each shaft carrying a pusher airscrew 9. The central part of stub-wing 4 houses in the manner described in Specification 460,975, an engine 10 which drives shafts 6 through transmission means 12 which may comprise belt or chain gear, or shaft and bevel gearing, the arrangement being in each case such that a reduction in rate of revolution is effected between the engine and airscrew shafts.
GB22448/35A 1935-08-08 1935-08-08 Improvements in and relating to propulsive systems for aircraft Expired GB461010A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB22448/35A GB461010A (en) 1935-08-08 1935-08-08 Improvements in and relating to propulsive systems for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB22448/35A GB461010A (en) 1935-08-08 1935-08-08 Improvements in and relating to propulsive systems for aircraft

Publications (1)

Publication Number Publication Date
GB461010A true GB461010A (en) 1937-02-08

Family

ID=10179509

Family Applications (1)

Application Number Title Priority Date Filing Date
GB22448/35A Expired GB461010A (en) 1935-08-08 1935-08-08 Improvements in and relating to propulsive systems for aircraft

Country Status (1)

Country Link
GB (1) GB461010A (en)

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