GB595812A - Improvements in resilient mountings adapted more particularly for supporting aircraft engine cowls - Google Patents
Improvements in resilient mountings adapted more particularly for supporting aircraft engine cowlsInfo
- Publication number
- GB595812A GB595812A GB17338/45A GB1733845A GB595812A GB 595812 A GB595812 A GB 595812A GB 17338/45 A GB17338/45 A GB 17338/45A GB 1733845 A GB1733845 A GB 1733845A GB 595812 A GB595812 A GB 595812A
- Authority
- GB
- United Kingdom
- Prior art keywords
- plate
- plates
- casing
- secured
- aircraft engine
- 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
- 230000006835 compression Effects 0.000 abstract 1
- 238000007906 compression Methods 0.000 abstract 1
- 239000002184 metal Substances 0.000 abstract 1
- 238000012856 packing Methods 0.000 abstract 1
- 239000012858 resilient material Substances 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 POWERÂ PLANTSÂ 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F7/00—Vibration-dampers; Shock-absorbers
- F16F7/08—Vibration-dampers; Shock-absorbers with friction surfaces rectilinearly movable along each other
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Vibration Prevention Devices (AREA)
- Springs (AREA)
- Gasket Seals (AREA)
Abstract
595,812. Resilient mountings. LORD MANUFACTURING CO. July 6, 1945, No. 17338. Convention date, July 11, 1944. [Class 108 (iii)] [Also in Group XXXIII] A mounting for mutually attaching two relatively movable members comprises a pair of plates 5, 6 having a body 7 of resilient material bonded to their opposed faces, a casing 14, 20 formed for attachment to one of the members and fixedly engaging one of the plates (5) and having sliding frictional engagement with the other plate (6) which is formed to have fixed engagement with the other member. As shown applied to the support of a radial aircraft engine cowl 1, the plate 5 is secured to a portion 14 of the casing which is integral with a plate 10 secured to the cowl 1. A flange 11 of the casing portion 20 carries a friction disc 25 engaging the plate 6. A pin 4 rigidly secured to the engine 2 and to the plate 6 has a shoulder locating a securing nut 33. A washer spaced between the nut 33 and the sandwich plate 5 and having frictional engagement with the latter, comprises metal rings 30, 32 separated by a rubber annulus 31, the compression of which is limited by a central ring 34 of less thickness. Interchangeable packing rings 21 enable the pressure between plates 6, 11 to be adjusted.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US595812XA | 1944-07-11 | 1944-07-11 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB595812A true GB595812A (en) | 1947-12-17 |
Family
ID=22023906
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB17338/45A Expired GB595812A (en) | 1944-07-11 | 1945-07-06 | Improvements in resilient mountings adapted more particularly for supporting aircraft engine cowls |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB595812A (en) |
-
1945
- 1945-07-06 GB GB17338/45A patent/GB595812A/en not_active Expired
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