GB520463A - Improvements in and relating to mounting structure for the power units of aeroplanes - Google Patents

Improvements in and relating to mounting structure for the power units of aeroplanes

Info

Publication number
GB520463A
GB520463A GB31466/38A GB3146638A GB520463A GB 520463 A GB520463 A GB 520463A GB 31466/38 A GB31466/38 A GB 31466/38A GB 3146638 A GB3146638 A GB 3146638A GB 520463 A GB520463 A GB 520463A
Authority
GB
United Kingdom
Prior art keywords
engine
aeroplanes
relating
aircraft
links
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
GB31466/38A
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 GB31466/38A priority Critical patent/GB520463A/en
Publication of GB520463A publication Critical patent/GB520463A/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
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/04—Aircraft characterised by the type or position of power plants of piston type
    • B64D27/06—Aircraft characterised by the type or position of power plants of piston type within, or attached to, wings

Landscapes

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

Abstract

520,463. Aero-engine mountings. GOHN, A. A. Oct. 31, 1938, No. 31466. [Class 4] The engine of an aircraft is mounted in a frame rockably connected with the aircraft and situated between the fuselage and wing. The engine 23, propeller 25 and shaft 24 are mounted in a frame 18 supported by links 11, 13 on a cradle 6 fixed to the fuselage 1. The wing 9 is carried above the cradle. When the aircraft is on the ground a lever 14 is adapted to swing the engine unit forward on the links 11, 13 until a stop 22 is engaged, whereupon the unit is locked by the links 15 passing a dead centre.
GB31466/38A 1938-10-31 1938-10-31 Improvements in and relating to mounting structure for the power units of aeroplanes Expired GB520463A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB31466/38A GB520463A (en) 1938-10-31 1938-10-31 Improvements in and relating to mounting structure for the power units of aeroplanes

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB31466/38A GB520463A (en) 1938-10-31 1938-10-31 Improvements in and relating to mounting structure for the power units of aeroplanes

Publications (1)

Publication Number Publication Date
GB520463A true GB520463A (en) 1940-04-24

Family

ID=10323504

Family Applications (1)

Application Number Title Priority Date Filing Date
GB31466/38A Expired GB520463A (en) 1938-10-31 1938-10-31 Improvements in and relating to mounting structure for the power units of aeroplanes

Country Status (1)

Country Link
GB (1) GB520463A (en)

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