GB827916A - Aircraft propeller - Google Patents

Aircraft propeller

Info

Publication number
GB827916A
GB827916A GB16458/58A GB1645858A GB827916A GB 827916 A GB827916 A GB 827916A GB 16458/58 A GB16458/58 A GB 16458/58A GB 1645858 A GB1645858 A GB 1645858A GB 827916 A GB827916 A GB 827916A
Authority
GB
United Kingdom
Prior art keywords
blade
degrees
aircraft propeller
last
camber line
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
GB16458/58A
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.)
RTX Corp
Original Assignee
United Aircraft Corp
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 United Aircraft Corp filed Critical United Aircraft Corp
Publication of GB827916A publication Critical patent/GB827916A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/16—Blades
    • B64C11/18—Aerodynamic features

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Tires In General (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Shaping Of Tube Ends By Bending Or Straightening (AREA)

Abstract

827,916. Screw propellers. UNITED AIRCRAFT CORPORATION. May 22, 1858 [Nov. 1, 1957], No. 16458/58. Class 114. In an aircraft propeller blade of thin crosssection, the trailing edge over the outboard 25% of the blade span has a large camber between the last 15 % and the last 5% of the chord of the blade with the camber line deflected between 6 degrees and 13 degrees from the mean camber line of the blade. Specification 505,077 is referred to.
GB16458/58A 1957-11-01 1958-05-22 Aircraft propeller Expired GB827916A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US827916XA 1957-11-01 1957-11-01

Publications (1)

Publication Number Publication Date
GB827916A true GB827916A (en) 1960-02-10

Family

ID=22173482

Family Applications (1)

Application Number Title Priority Date Filing Date
GB16458/58A Expired GB827916A (en) 1957-11-01 1958-05-22 Aircraft propeller

Country Status (1)

Country Link
GB (1) GB827916A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1707485A1 (en) * 2004-01-20 2006-10-04 Obschestvo s Ogranichennoi Otvetstvennostyu Midera-k Propeller

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1707485A1 (en) * 2004-01-20 2006-10-04 Obschestvo s Ogranichennoi Otvetstvennostyu Midera-k Propeller
EP1707485A4 (en) * 2004-01-20 2007-10-03 Obschestvo S Ogranichennoi Otv Propeller

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