GB331801A - Improvements in or relating to the arrangement and disposition of motors on aircraft - Google Patents

Improvements in or relating to the arrangement and disposition of motors on aircraft

Info

Publication number
GB331801A
GB331801A GB38151/29A GB3815129A GB331801A GB 331801 A GB331801 A GB 331801A GB 38151/29 A GB38151/29 A GB 38151/29A GB 3815129 A GB3815129 A GB 3815129A GB 331801 A GB331801 A GB 331801A
Authority
GB
United Kingdom
Prior art keywords
disposition
aircraft
motors
relating
arrangement
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
GB38151/29A
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
Publication of GB331801A publication Critical patent/GB331801A/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

Landscapes

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

Abstract

331,801. Renault, L. Feb. 7, 1929, [Convention date]. Propelling; planes, construction of.-A radial cylinder engine is arranged horizontally within the leading edge of a wing and its vertical shaft drives a horizontal propeller shaft 5 through gearing 4. A casing 7 with openings 8. 9 directs air from the propeller over the cylinders, and the carburettors 10 are supplied with air heated by its passage over the cylinders.
GB38151/29A 1929-02-07 1929-12-12 Improvements in or relating to the arrangement and disposition of motors on aircraft Expired GB331801A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR331801X 1929-02-07

Publications (1)

Publication Number Publication Date
GB331801A true GB331801A (en) 1930-07-10

Family

ID=8890964

Family Applications (1)

Application Number Title Priority Date Filing Date
GB38151/29A Expired GB331801A (en) 1929-02-07 1929-12-12 Improvements in or relating to the arrangement and disposition of motors on aircraft

Country Status (1)

Country Link
GB (1) GB331801A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11180243B2 (en) 2019-06-05 2021-11-23 Anchor Concrete Inc. Rotary engine/centrifugal fan aircraft propulsion

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11180243B2 (en) 2019-06-05 2021-11-23 Anchor Concrete Inc. Rotary engine/centrifugal fan aircraft propulsion

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