GB802859A - Improvements relating to engine transmissions - Google Patents

Improvements relating to engine transmissions

Info

Publication number
GB802859A
GB802859A GB8435/57A GB843557A GB802859A GB 802859 A GB802859 A GB 802859A GB 8435/57 A GB8435/57 A GB 8435/57A GB 843557 A GB843557 A GB 843557A GB 802859 A GB802859 A GB 802859A
Authority
GB
United Kingdom
Prior art keywords
propeller
engine
movement
aircraft
ring gear
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
GB8435/57A
Inventor
Victor Wiseheart Peterson
Herbert Heinrich Schnepel
Paul Bancel
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.)
Motors Liquidation Co
Original Assignee
Motors Liquidation Co
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 Motors Liquidation Co filed Critical Motors Liquidation Co
Priority to GB8435/57A priority Critical patent/GB802859A/en
Publication of GB802859A publication Critical patent/GB802859A/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
    • B64D35/00Transmitting power from power plants to propellers or rotors; Arrangements of transmissions

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Retarders (AREA)
  • Toys (AREA)

Abstract

802,859. Feathering aircraft propeller blades. GENERAL MOTORS CORPORATION. March 14, 1957, No. 8435/57. Class 4. [Also in Groups XIX and XXIV] Movement of the reaction ring gear 44 of an epicyclic train between the engine and propeller of an aircraft is utilized to indicate negative torque or feather the propeller on failure of the engine and consequent " windmilling " of the propeller. The movement of the ring gear against a spring device is transmitted by a rod 190 and bellcrank 198 to a plunger 220 which actuates an indicating instrument or control mechanism 223.
GB8435/57A 1957-03-14 1957-03-14 Improvements relating to engine transmissions Expired GB802859A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB8435/57A GB802859A (en) 1957-03-14 1957-03-14 Improvements relating to engine transmissions

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8435/57A GB802859A (en) 1957-03-14 1957-03-14 Improvements relating to engine transmissions

Publications (1)

Publication Number Publication Date
GB802859A true GB802859A (en) 1958-10-15

Family

ID=9852441

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8435/57A Expired GB802859A (en) 1957-03-14 1957-03-14 Improvements relating to engine transmissions

Country Status (1)

Country Link
GB (1) GB802859A (en)

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