GB534280A - Improvements in engine mounting in aircraft - Google Patents

Improvements in engine mounting in aircraft

Info

Publication number
GB534280A
GB534280A GB25037/39A GB2503739A GB534280A GB 534280 A GB534280 A GB 534280A GB 25037/39 A GB25037/39 A GB 25037/39A GB 2503739 A GB2503739 A GB 2503739A GB 534280 A GB534280 A GB 534280A
Authority
GB
United Kingdom
Prior art keywords
engine
secured
cantilever
frames
aircraft
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
GB25037/39A
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 GB25037/39A priority Critical patent/GB534280A/en
Publication of GB534280A publication Critical patent/GB534280A/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)
  • Vibration Prevention Devices (AREA)

Abstract

534,280. Aircraft engine mountings. HIRST, A. J. Aug. 31, 1939, No. 25037. [Class 4] [Also in Group XXXII] An aircraft engine 11 is mounted between cantilever triangulated frames which are attached at 13, 14 to the fuselage, are secured rigidly at their forward ends to feet 15 on the engine, and are secured resiliently to the engine at 20 near the inner ends of the cantilever frames. The resilient mounting comprises plates secured by interleaved rubber sheets, alternate plates being secured to the frames and to the engine crankcase. The plates may be horizontal, or vertical and transverse to the crankshaft axis. The resilience of the forward end of the cantilever and that of the resilient mounting 20 may be matched to provide the required frequency of free vibration of the engine.
GB25037/39A 1939-08-31 1939-08-31 Improvements in engine mounting in aircraft Expired GB534280A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB25037/39A GB534280A (en) 1939-08-31 1939-08-31 Improvements in engine mounting in aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB25037/39A GB534280A (en) 1939-08-31 1939-08-31 Improvements in engine mounting in aircraft

Publications (1)

Publication Number Publication Date
GB534280A true GB534280A (en) 1941-03-04

Family

ID=10221194

Family Applications (1)

Application Number Title Priority Date Filing Date
GB25037/39A Expired GB534280A (en) 1939-08-31 1939-08-31 Improvements in engine mounting in aircraft

Country Status (1)

Country Link
GB (1) GB534280A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2441673A3 (en) * 2010-10-14 2014-04-16 Rolls-Royce plc Support structure

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2441673A3 (en) * 2010-10-14 2014-04-16 Rolls-Royce plc Support structure

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