GB496401A - Anti-vibrational mounting arrangement of an engine on its support - Google Patents
Anti-vibrational mounting arrangement of an engine on its supportInfo
- Publication number
- GB496401A GB496401A GB15400/37A GB1540037A GB496401A GB 496401 A GB496401 A GB 496401A GB 15400/37 A GB15400/37 A GB 15400/37A GB 1540037 A GB1540037 A GB 1540037A GB 496401 A GB496401 A GB 496401A
- Authority
- GB
- United Kingdom
- Prior art keywords
- engine
- plates
- axis
- support
- mounting
- 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
Links
- 238000000034 method Methods 0.000 abstract 2
- 238000012986 modification Methods 0.000 abstract 1
- 230000004048 modification Effects 0.000 abstract 1
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
496,401. Resilient engine-mountings. THIRY, L. June 3, 1937, Nos. 15400 and 15401. Convention dates, June 9, 1936 and Nov. 12, 1936. [Class 108 (iii)] A mounting for an engine, on its support, particularly for an aeroplane engine, comprising elastic connecting means distributed about the axis of the engine crank-shaft, each connecting means consisting of three or more parallel plates 101-103 clamped together and perpendicular to the axis of the crank-shaft and between which are disposed elastic cushions 104, 105 having an oblong form, the large axis of which is disposed at right-angles to a perpendicular to and the small axis at right-angles to the axis of the crank-shaft, the engine and the support each being connected to one set of alternate plates. The central plates 101 of the connecting means are mounted on bolts 119 mounted in plates 117, 118 fixed to the aeroplane fuselage. The outer plates 102, 103 are clamped together by a sleeve 106 which are mounted on bolts 123 fixed to the engine 114. The elastic cushions 104, 105 adhere to the plates and engage flanges 110 thereon. In a modification, the central plate is formed of two concave plates welded together and spaced at the centre by a washer, the mounting bolt passing through an aperture at the centre. The outer plates are clamped together at both ends by tubular rivets and are bent over at the edges and welded to one another. Two methods of connecting the central plate to a support are shown comprising a bolt surrounded by a sleeve or sleeves, and a method of mounting an aeroplane engine comprises an annular casing in which the mounting means are contained and which has openings for the securing bolts.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR496401X | 1936-06-09 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB496401A true GB496401A (en) | 1938-11-30 |
Family
ID=8904872
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB15400/37A Expired GB496401A (en) | 1936-06-09 | 1937-06-03 | Anti-vibrational mounting arrangement of an engine on its support |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB496401A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113184223A (en) * | 2020-03-13 | 2021-07-30 | 北京星际荣耀空间科技股份有限公司 | Engine supporting device and carrier rocket |
-
1937
- 1937-06-03 GB GB15400/37A patent/GB496401A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113184223A (en) * | 2020-03-13 | 2021-07-30 | 北京星际荣耀空间科技股份有限公司 | Engine supporting device and carrier rocket |
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