GB493651A - Mounting of aircraft engines - Google Patents

Mounting of aircraft engines

Info

Publication number
GB493651A
GB493651A GB16569/37A GB1656937A GB493651A GB 493651 A GB493651 A GB 493651A GB 16569/37 A GB16569/37 A GB 16569/37A GB 1656937 A GB1656937 A GB 1656937A GB 493651 A GB493651 A GB 493651A
Authority
GB
United Kingdom
Prior art keywords
braced
point
mounting
seat
members
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
GB16569/37A
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.)
WILLIAM ARNOLD HORROCKS
Original Assignee
WILLIAM ARNOLD HORROCKS
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 WILLIAM ARNOLD HORROCKS filed Critical WILLIAM ARNOLD HORROCKS
Priority to GB16569/37A priority Critical patent/GB493651A/en
Publication of GB493651A publication Critical patent/GB493651A/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
    • B64D27/02Aircraft characterised by the type or position of power plants
    • B64D27/04Aircraft characterised by the type or position of power plants of piston type

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Portable Outdoor Equipment (AREA)

Abstract

493,651. Propelling aircraft. HORROCKS, W. A. June 15, 1937, No. 16569. [Class 4] A mounting for aero-engines comprises independent tubular frames disposed on each side of the engine and each frame is connected at vertically spaced points A, B to the aircraft structure and includes a normally substantially horizontal member E<3> carrying two engine seats C<1>, C<2>, a laterally-extending king post E braced by members E<1>, E<2> to the points A and B and by a member E<3> to the seat C<1>, the seats C<1>, C<2> being braced to the point B by members D<1>, D<2> and the seat C' being braced to the point A by a member D or an intermediate point of the member D' being braced to the point A. In the latter alternative construction, the intermediate point is braced to the seating C<2> and to the outer end of the port E.
GB16569/37A 1937-06-15 1937-06-15 Mounting of aircraft engines Expired GB493651A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB16569/37A GB493651A (en) 1937-06-15 1937-06-15 Mounting of aircraft engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB16569/37A GB493651A (en) 1937-06-15 1937-06-15 Mounting of aircraft engines

Publications (1)

Publication Number Publication Date
GB493651A true GB493651A (en) 1938-10-12

Family

ID=10079674

Family Applications (1)

Application Number Title Priority Date Filing Date
GB16569/37A Expired GB493651A (en) 1937-06-15 1937-06-15 Mounting of aircraft engines

Country Status (1)

Country Link
GB (1) GB493651A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4213585A (en) * 1978-05-22 1980-07-22 The Boeing Company Mounting system for a wing mounted aircraft engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4213585A (en) * 1978-05-22 1980-07-22 The Boeing Company Mounting system for a wing mounted aircraft engine

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