GB501006A - Improvements in devices for the mounting of an engine or like apparatus on its support - Google Patents

Improvements in devices for the mounting of an engine or like apparatus on its support

Info

Publication number
GB501006A
GB501006A GB22284/37A GB2228437A GB501006A GB 501006 A GB501006 A GB 501006A GB 22284/37 A GB22284/37 A GB 22284/37A GB 2228437 A GB2228437 A GB 2228437A GB 501006 A GB501006 A GB 501006A
Authority
GB
United Kingdom
Prior art keywords
engine
members
support
mounting
aug
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
GB22284/37A
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
Publication of GB501006A publication Critical patent/GB501006A/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; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02—Aircraft characterised by the type or position of power plant
    • B64D27/04—Aircraft characterised by the type or position of power plant of piston type

Abstract

501,006. Resilient supports; dashpots. BENAUX. E. P., and RENAUX, L. J. Aug. 13, 1937, No. 22284. Convention date, Aug. 17, 1936. [Class 108 (iii)] [Also in Groups XXXIII and XXXI] An engine or other apparatus having parts rotating or oscillating about an axis is mounted on a support or frame by means which include at least one member mounted through the intermediary of an elastic ring adapted to damp vibrations of small amplitude on an axle substantially parallel to the axis of rotation, the member being connected with the apparatus and formed with an arm connected with a damping device carried by the support and adapted to damp vibrations of large amplitude. In one form, an aircraft engine 1 is supported in a cradle 2, 3. The members 2 are arranged parallel to the engine crankshaft and are connected by rubber bushes 7 to shafts 5 which are connected by links 8 and rubber bushes to beams 13 forming part of the aircraft framework 14. One or more of the links 8 are provided with extensions 15 connected to members 16, 17 between which and members 21 are disposed pneumatic members 18. In a modification the mounting is applied to a radial aero-engine in which case the engine mounting ring acts through gear teeth arranged between the mounting ring and the arm engaging the member. The pneumatic member may be replaced by a dashpot having a piston centralized by springs and provided with a metering orifice and a non-return valve in order to give a differential action.
GB22284/37A 1936-08-17 1937-08-13 Improvements in devices for the mounting of an engine or like apparatus on its support Expired GB501006A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR501006X 1936-08-17

Publications (1)

Publication Number Publication Date
GB501006A true GB501006A (en) 1939-02-13

Family

ID=8905437

Family Applications (1)

Application Number Title Priority Date Filing Date
GB22284/37A Expired GB501006A (en) 1936-08-17 1937-08-13 Improvements in devices for the mounting of an engine or like apparatus on its support

Country Status (1)

Country Link
GB (1) GB501006A (en)

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