GB542747A - Improvements in joints for engine mountings and like purposes - Google Patents

Improvements in joints for engine mountings and like purposes

Info

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
Application number
GB1826/41A
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.)
Martin Baker Aircraft Co Ltd
Original Assignee
Martin Baker Aircraft Co Ltd
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 Martin Baker Aircraft Co Ltd filed Critical Martin Baker Aircraft Co Ltd
Priority to GB1826/41A priority Critical patent/GB542747A/en
Publication of GB542747A publication Critical patent/GB542747A/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

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.
GB1826/41A 1941-02-11 1941-02-11 Improvements in joints for engine mountings and like purposes Expired GB542747A (en)

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)

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