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)

Similar Documents

Publication Publication Date Title
GB1066360A (en) Aircraft
GB1411601A (en) Ducted fan gas turbine engine supported by an aircraft wing mainspar
GB756837A (en) Captive toy aeroplane
GB520463A (en) Improvements in and relating to mounting structure for the power units of aeroplanes
GB753970A (en) Improvements in or relating to helicopters
GB167068A (en) Improvements in and relating to aeroplanes for commercial purposes
GB521218A (en) Improvements in helicopters
GB515562A (en) Improvements in or relating to the structure of aircraft
GB607924A (en) Improvements in and relating to helicopters
GB762785A (en) Improvements relating to aircraft
GB536865A (en) Improvements in or relating to aircraft
GB568035A (en) Aircraft engine mounting
GB349895A (en) Improvements in and relating to aircraft driven by engines with opposed pistons
GB605638A (en) Aircraft
GB507681A (en) Improvements in and relating to the mounting of power units in vehicles
GB522296A (en) Improvements in or relating to aerodynes
GB500541A (en) Improvements in and relating to aeroplanes
GB505201A (en) Improvements in or connected with wing construction of aircraft
GB223501A (en) Improvements in screw and like propellers for aeroplanes
GB145016A (en) Improvements in connexion with air screws
GB348528A (en) Improvements relating to aeroplanes
GB388574A (en) Aeroplane
GB525013A (en) Improvements in supporting wings for aircraft
GB264801A (en) Improvements in and relating to aeroplanes and the like
GB376789A (en) Improvements in or relating to aeroplanes