GB556109A - Resilient mountings - Google Patents

Resilient mountings

Info

Publication number
GB556109A
GB556109A GB3218/42A GB321842A GB556109A GB 556109 A GB556109 A GB 556109A GB 3218/42 A GB3218/42 A GB 3218/42A GB 321842 A GB321842 A GB 321842A GB 556109 A GB556109 A GB 556109A
Authority
GB
United Kingdom
Prior art keywords
forks
rubber
casing
faces
engines
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
GB3218/42A
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.)
Lord Manufacturing Co
Original Assignee
Lord Manufacturing Co
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 Lord Manufacturing Co filed Critical Lord Manufacturing Co
Publication of GB556109A publication Critical patent/GB556109A/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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)

Abstract

556,109. Shock absorbers. LORD MANUFACTURING CO. March 11, 1942, No. 3218. Convention date, Feb. 11, 1941. [Class 108 (iii)] Engines, such as aeroplane engines, mounted in an overhung manner by means of a number of flexible rubber joints are given additional flexibility to allow pitch and yaw movements more readily than torque movements, by providing pivots between the rubber joint and the engine and frame. Two rubber elements 8 are interposed between the two faces of the casing 6 and the two faces of the interior plate 7 having extensions to the exterior forming forks 12 carrying the pivot pin 16 mounted in the shank 18, roller bearings 15 being employed. A similar connection to an engine bracket 31 is provided by forks 24 on the casing 6. One rubber element may be made larger than the other to compensate for the apertures passing the forks 12. Specification 552,888 is referred to.
GB3218/42A 1941-02-11 1942-03-11 Resilient mountings Expired GB556109A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US556109XA 1941-02-11 1941-02-11

Publications (1)

Publication Number Publication Date
GB556109A true GB556109A (en) 1943-09-21

Family

ID=21999014

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3218/42A Expired GB556109A (en) 1941-02-11 1942-03-11 Resilient mountings

Country Status (1)

Country Link
GB (1) GB556109A (en)

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