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GB478752A - Improvements in or relating to the mounting of aircraft engines - Google Patents

Improvements in or relating to the mounting of aircraft engines

Info

Publication number
GB478752A
GB478752A GB25669/36A GB2566936A GB478752A GB 478752 A GB478752 A GB 478752A GB 25669/36 A GB25669/36 A GB 25669/36A GB 2566936 A GB2566936 A GB 2566936A GB 478752 A GB478752 A GB 478752A
Authority
GB
United Kingdom
Prior art keywords
mounting
relating
sept
aircraft engines
blocks
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
GB25669/36A
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.)
GETEFO Gesellschaft Fuer Technischen Fortschritt mbH
Original Assignee
GETEFO Gesellschaft Fuer Technischen Fortschritt mbH
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 GETEFO Gesellschaft Fuer Technischen Fortschritt mbH filed Critical GETEFO Gesellschaft Fuer Technischen Fortschritt mbH
Publication of GB478752A publication Critical patent/GB478752A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02Aircraft characterised by the type or position of power plants
    • B64D27/04Aircraft characterised by the type or position of power plants of piston type

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Steroid Compounds (AREA)

Abstract

478,752. Resilient mountings. GETEFO GES. FUR TECHNISCHEN FORTSCHRITT. Sept. 21, 1936, No. 25669. Convention date, Sept. 28, 1935. [Class 108 (iii)] [Also in Group XXXIII] A resilient mounting for aero-engines comprises rubber blocks 7, 10 bonded to flanged metal plates 5, 6. The blocks may be of different hardness and may be subject to differing initial stress.
GB25669/36A 1935-09-28 1936-09-21 Improvements in or relating to the mounting of aircraft engines Expired GB478752A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE478752X 1935-09-28

Publications (1)

Publication Number Publication Date
GB478752A true GB478752A (en) 1938-01-25

Family

ID=6542297

Family Applications (1)

Application Number Title Priority Date Filing Date
GB25669/36A Expired GB478752A (en) 1935-09-28 1936-09-21 Improvements in or relating to the mounting of aircraft engines

Country Status (1)

Country Link
GB (1) GB478752A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4717094A (en) * 1986-05-19 1988-01-05 The Boeing Company Aircraft engine mount system with vibration isolators

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4717094A (en) * 1986-05-19 1988-01-05 The Boeing Company Aircraft engine mount system with vibration isolators
EP0250659A2 (en) * 1986-05-19 1988-01-07 The Boeing Company Aircraft engine mount system with vibration isolators
EP0250659A3 (en) * 1986-05-19 1989-05-31 The Boeing Company Aircraft engine mount system with vibration isolators

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