GB225007A - An improved engine mounting for aircraft - Google Patents

An improved engine mounting for aircraft

Info

Publication number
GB225007A
GB225007A GB24064/23A GB2406423A GB225007A GB 225007 A GB225007 A GB 225007A GB 24064/23 A GB24064/23 A GB 24064/23A GB 2406423 A GB2406423 A GB 2406423A GB 225007 A GB225007 A GB 225007A
Authority
GB
United Kingdom
Prior art keywords
stay
sheets
plate
fuselage
pivoted
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
GB24064/23A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB24064/23A priority Critical patent/GB225007A/en
Publication of GB225007A publication Critical patent/GB225007A/en
Expired legal-status Critical Current

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 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)
  • Toys (AREA)
  • Pivots And Pivotal Connections (AREA)

Abstract

225,007. Bolas, H., and Parnall, G. G. Sept. 27,1923. Propelling. - An engine of the radial fixedcylinder type and the front section of its cowling are carried by an engine plate of girder formation detachably connected to a rigid triangulated stay structure having pivotal connections with the fuselage of the craft. The plate is formed by sheets 7 and 8, spaced and braced by channel strips 9, 9<a>, the sheet 7 being formed with an hexagonal opening 7<a>, and the sheet 8, to which the crank case is bolted, with a circular opening 8<a>. The strips 9<a> between the vertical edges of the sheets extend above and below the sheets and are provided near their ends with holes 10 to receive bolts 18. Each bolt passes through a lug on the front end of an inclined tubular stay 12 pivoted at its rear end to a bracket 13 on the fuselage, and is secured by a nut 19. The plate 8 is formed with slots 11 to accommodate the stays 12, the bottom of each slot being reinforced by a channel member 9<b>. Two diagonal tubular struts 15 are provided, each pivoted at its upper end to the front portion of the corresponding stay 12 and at its lower end to the corresponding lower bracket 13, and a short strut 16 connects each strut 15 to the front portion of the corresponding lower stay 12. Additional bracing is provided by wires or cables 17.
GB24064/23A 1923-09-27 1923-09-27 An improved engine mounting for aircraft Expired GB225007A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB24064/23A GB225007A (en) 1923-09-27 1923-09-27 An improved engine mounting for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB24064/23A GB225007A (en) 1923-09-27 1923-09-27 An improved engine mounting for aircraft

Publications (1)

Publication Number Publication Date
GB225007A true GB225007A (en) 1924-11-27

Family

ID=10205785

Family Applications (1)

Application Number Title Priority Date Filing Date
GB24064/23A Expired GB225007A (en) 1923-09-27 1923-09-27 An improved engine mounting for aircraft

Country Status (1)

Country Link
GB (1) GB225007A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110844090A (en) * 2019-10-11 2020-02-28 中国直升机设计研究所 Supporting type mounting device of piston engine of helicopter

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110844090A (en) * 2019-10-11 2020-02-28 中国直升机设计研究所 Supporting type mounting device of piston engine of helicopter
CN110844090B (en) * 2019-10-11 2022-11-22 中国直升机设计研究所 Supporting type mounting device of piston engine of helicopter

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