GB470938A - Improvements in or relating to engine mounts - Google Patents

Improvements in or relating to engine mounts

Info

Publication number
GB470938A
GB470938A GB14410/36A GB1441036A GB470938A GB 470938 A GB470938 A GB 470938A GB 14410/36 A GB14410/36 A GB 14410/36A GB 1441036 A GB1441036 A GB 1441036A GB 470938 A GB470938 A GB 470938A
Authority
GB
United Kingdom
Prior art keywords
sleeves
ring
brackets
welded
spaced
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
GB14410/36A
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.)
Raytheon Technologies Corp
Original Assignee
United Aircraft Corp
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 United Aircraft Corp filed Critical United Aircraft Corp
Publication of GB470938A publication Critical patent/GB470938A/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
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/40Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Vibration Prevention Devices (AREA)

Abstract

470,938. Resilient mountings. UNITED AIRCRAFT CORPORATION. May 21, 1936, No. 14410. Convention date, May 21, 1935. [Class 108 (iii)] [Also in Group XXXIII] An engine mounting includes a mounting ring 26 a plurality of brackets, each comprising a pair of spaced-apart hangers 32, 34, and a mounting block 54 resiliently connected to the hangers by means of two connections 58 radially-spaced with respect to the ring. As shown, the resilient sleeves 58 are preferably vulcanized to sleeves 52, 62. The sleeves 52 are connected by an integral web 54 which is apertured to receive a bolt which engages bosses formed on the engine intake manifold. The sleeves 62 are connected by screw-threaded studs to the brackets which are welded to the ring 26. In a modification, the web 54 is welded to the sleeves 52 and in a further modification the brackets are flanged and bolted to the supporting-ring, one of the bolts being welded to the bracket.
GB14410/36A 1935-05-21 1936-05-21 Improvements in or relating to engine mounts Expired GB470938A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US470938XA 1935-05-21 1935-05-21

Publications (1)

Publication Number Publication Date
GB470938A true GB470938A (en) 1937-08-25

Family

ID=21947031

Family Applications (1)

Application Number Title Priority Date Filing Date
GB14410/36A Expired GB470938A (en) 1935-05-21 1936-05-21 Improvements in or relating to engine mounts

Country Status (1)

Country Link
GB (1) GB470938A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109715478A (en) * 2016-07-28 2019-05-03 雷诺尔特股份有限公司 Bearing structure

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109715478A (en) * 2016-07-28 2019-05-03 雷诺尔特股份有限公司 Bearing structure

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