GB452841A - Improvements in screw propellers for aircraft - Google Patents

Improvements in screw propellers for aircraft

Info

Publication number
GB452841A
GB452841A GB10160/36A GB1016036A GB452841A GB 452841 A GB452841 A GB 452841A GB 10160/36 A GB10160/36 A GB 10160/36A GB 1016036 A GB1016036 A GB 1016036A GB 452841 A GB452841 A GB 452841A
Authority
GB
United Kingdom
Prior art keywords
aircraft
screw propellers
april
wood
screw
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
GB10160/36A
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 GB452841A publication Critical patent/GB452841A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/16Blades
    • B64C11/20Constructional features
    • B64C11/205Constructional features for protecting blades, e.g. coating

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)

Abstract

452,841. Screw propellers. RHODIUS, R., 42, Waller Heerstrasse, Bremen, Germany. April 6, 1936, No. 10160. Convention date, April 12, 1935. [Class 114] An aircraft screw-propeller blade of wood 1 having metal sheet edge covering 2 is providedwith a thin permanently elastic impermeable packing such as a thin rubber sheet 3 between the metal and the wood.
GB10160/36A 1935-04-12 1936-04-06 Improvements in screw propellers for aircraft Expired GB452841A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE452841X 1935-04-12

Publications (1)

Publication Number Publication Date
GB452841A true GB452841A (en) 1936-08-31

Family

ID=6538713

Family Applications (1)

Application Number Title Priority Date Filing Date
GB10160/36A Expired GB452841A (en) 1935-04-12 1936-04-06 Improvements in screw propellers for aircraft

Country Status (1)

Country Link
GB (1) GB452841A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2431184A (en) * 1943-09-23 1947-11-18 United Aireraft Corp Composite blade
US4097193A (en) * 1975-12-24 1978-06-27 Messerschmitt-Boelkow-Blohm Gmbh Elastomeric damping arrangement
US4667906A (en) * 1985-04-02 1987-05-26 Grumman Aerospace Corporation Replaceable tip for aircraft leading edge
US5165859A (en) * 1992-06-26 1992-11-24 Hudson Products Corporation Leading edge protection for fan blade
US6273676B1 (en) * 1998-06-17 2001-08-14 United Technologies Corporation Method and assembly for masking a flow directing assembly
FR2943102A1 (en) * 2009-03-12 2010-09-17 Snecma DAWN IN COMPOSITE MATERIAL COMPRISING A DAMPING DEVICE.
GB2518640A (en) * 2013-09-26 2015-04-01 Ge Aviat Systems Group Ltd Propeller blade assembly

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2431184A (en) * 1943-09-23 1947-11-18 United Aireraft Corp Composite blade
US4097193A (en) * 1975-12-24 1978-06-27 Messerschmitt-Boelkow-Blohm Gmbh Elastomeric damping arrangement
US4667906A (en) * 1985-04-02 1987-05-26 Grumman Aerospace Corporation Replaceable tip for aircraft leading edge
US5165859A (en) * 1992-06-26 1992-11-24 Hudson Products Corporation Leading edge protection for fan blade
EP0576117A1 (en) * 1992-06-26 1993-12-29 Hudson Products Corporation Edge protection for a fan blade
US6273676B1 (en) * 1998-06-17 2001-08-14 United Technologies Corporation Method and assembly for masking a flow directing assembly
FR2943102A1 (en) * 2009-03-12 2010-09-17 Snecma DAWN IN COMPOSITE MATERIAL COMPRISING A DAMPING DEVICE.
US8500410B2 (en) 2009-03-12 2013-08-06 Snecma Blade made of composite material comprising a damping device
GB2518640A (en) * 2013-09-26 2015-04-01 Ge Aviat Systems Group Ltd Propeller blade assembly
CN104512536A (en) * 2013-09-26 2015-04-15 通用电气航空系统有限公司 Propeller blade assembly
GB2518640B (en) * 2013-09-26 2016-01-20 Ge Aviat Systems Ltd Propeller blade assembly

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