GB542747A - Improvements in joints for engine mountings and like purposes - Google Patents
Improvements in joints for engine mountings and like purposesInfo
- Publication number
- GB542747A GB542747A GB1826/41A GB182641A GB542747A GB 542747 A GB542747 A GB 542747A GB 1826/41 A GB1826/41 A GB 1826/41A GB 182641 A GB182641 A GB 182641A GB 542747 A GB542747 A GB 542747A
- Authority
- GB
- United Kingdom
- Prior art keywords
- bolt
- plates
- expander
- members
- split sleeve
- 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
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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
Abstract
542,747. Strut connections. MARTIN, J., and MARTIN-BAKER AIRCRAFT CO., Ltd. Feb. 11, 1941, No. 1826. [Class 20 (ii)] [Also in Group XXXIII] A joint, particularly for securing a detachable aero engine to a fuselage frame comprises a split sleeve or bush fitted into the members to be joined, a tapered expander fitted in the split sleeve and a bolt for displacing the expander axially. Fig. 2 shows a section of a joint comprising two parallel plates 8, 9 between which the ends of some of the frame members 5 and stays 6 are received and secured by bolts 11. The end 12 of a detachable engine mounting strut also is received between the plates and secured in position by a split sleeve 16 which is expanded into tight contact with holes in the plates 8, 9 and member 12, by a tapered expander 15 forced into position by a bolt 13 screwed into a boss on the plate 8. This boss has a socket 10 to receive one of the frame members 5. Each sleeve expander and bolt of a set is fixed or removed from the same side of the assemblage. The members 15, 16 have threaded parts 15a, 16a at their outer ends to enable them to be withdrawn by nuts screwed over their ends. The engine mounting struts, with attached bulkhead 7, Fig. 3, can therefore be readily removed without disturbing the fuselage frame. The lower pair of plates are connected by a hollow bolt 4a to receive a landing carriage strut connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1826/41A GB542747A (en) | 1941-02-11 | 1941-02-11 | Improvements in joints for engine mountings and like purposes |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1826/41A GB542747A (en) | 1941-02-11 | 1941-02-11 | Improvements in joints for engine mountings and like purposes |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB542747A true GB542747A (en) | 1942-01-26 |
Family
ID=9728674
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1826/41A Expired GB542747A (en) | 1941-02-11 | 1941-02-11 | Improvements in joints for engine mountings and like purposes |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB542747A (en) |
-
1941
- 1941-02-11 GB GB1826/41A patent/GB542747A/en not_active Expired
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