GB506645A - Improvements in or relating to the mounting of aircraft engines and propellers - Google Patents

Improvements in or relating to the mounting of aircraft engines and propellers

Info

Publication number
GB506645A
GB506645A GB33087/37A GB3308737A GB506645A GB 506645 A GB506645 A GB 506645A GB 33087/37 A GB33087/37 A GB 33087/37A GB 3308737 A GB3308737 A GB 3308737A GB 506645 A GB506645 A GB 506645A
Authority
GB
United Kingdom
Prior art keywords
engine
crankshaft
aircraft
airscrew
shaft
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
GB33087/37A
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.)
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 GB33087/37A priority Critical patent/GB506645A/en
Publication of GB506645A publication Critical patent/GB506645A/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
    • B64D27/06Aircraft characterised by the type or position of power plants of piston type within, or attached to, wings

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)

Abstract

506,645. Propelling aircraft. ELLIOTT, A. C. Nov. 30, 1937, No. 33087. [Class 4] An aircraft, engine, mounted in the aircraft structure by means of trunnion pins at each end coaxial or parallel with the crankshaft, drives a propeller and shaft/rigidly mounted in the structure independently of' the engine, through a universally-jointed transmission, resilient means being provided for resisting torque reaction of the engine. The trunnion pins may,be resiliently mounted and frictional or hydraulic means provided to damp engine vibrations. As shown, an engine 5 is mounted in a wing 21 by means of trunnions 7<1> coaxial with the crankshaft and carried in rubber bearings in the spars 7, S. Torque arms 10 are provided connected at 13, 14 to subsidiary fore-and-aft spars 11, 12 by rubber or springs. The arms may be resiliently connected to the engine. The airscrew 15 is mounted in bearings carried by a housing 16 supported by an outrigger 17 from the spar 7 and is connected to the crankshaft by a shaft 18 and flexible or universal joints 19, 20.. A reduction gear may be interposed between the airscrew and crankshafts. Specification 498,224 is referred to.
GB33087/37A 1937-11-30 1937-11-30 Improvements in or relating to the mounting of aircraft engines and propellers Expired GB506645A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB33087/37A GB506645A (en) 1937-11-30 1937-11-30 Improvements in or relating to the mounting of aircraft engines and propellers

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB33087/37A GB506645A (en) 1937-11-30 1937-11-30 Improvements in or relating to the mounting of aircraft engines and propellers

Publications (1)

Publication Number Publication Date
GB506645A true GB506645A (en) 1939-05-30

Family

ID=10348391

Family Applications (1)

Application Number Title Priority Date Filing Date
GB33087/37A Expired GB506645A (en) 1937-11-30 1937-11-30 Improvements in or relating to the mounting of aircraft engines and propellers

Country Status (1)

Country Link
GB (1) GB506645A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2753140A (en) * 1951-07-28 1956-07-03 United Aircraft Corp Engine mount
US4266741A (en) * 1978-05-22 1981-05-12 The Boeing Company Mounting apparatus for fan jet engine having mixed flow nozzle installation

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2753140A (en) * 1951-07-28 1956-07-03 United Aircraft Corp Engine mount
US4266741A (en) * 1978-05-22 1981-05-12 The Boeing Company Mounting apparatus for fan jet engine having mixed flow nozzle installation

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