GB965966A - Improvements in or relating to propeller airscrews - Google Patents

Improvements in or relating to propeller airscrews

Info

Publication number
GB965966A
GB965966A GB2592061A GB2592061A GB965966A GB 965966 A GB965966 A GB 965966A GB 2592061 A GB2592061 A GB 2592061A GB 2592061 A GB2592061 A GB 2592061A GB 965966 A GB965966 A GB 965966A
Authority
GB
United Kingdom
Prior art keywords
blade
duct
propeller
air
effect
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
GB2592061A
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.)
RHEIN FLUGZEUGBAU GmbH
Original Assignee
RHEIN FLUGZEUGBAU GmbH
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 RHEIN FLUGZEUGBAU GmbH filed Critical RHEIN FLUGZEUGBAU GmbH
Publication of GB965966A publication Critical patent/GB965966A/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
    • B64C11/001Shrouded propellers
    • 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
    • B64C11/24Hollow blades
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/06Aircraft not otherwise provided for having disc- or ring-shaped wings
    • B64C39/062Aircraft not otherwise provided for having disc- or ring-shaped wings having annular wings

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

965,966. Screw propellers; de-icing annular wing aircraft. RHEIN - FLUGZEUGBAU G.m.b.H. July 18, 1961 [July 23, 1960], No. 25920/61. Headings B7V and B7W. [Also in Division F2] A cushion of compressed gas 15 is maintained in the annular region between the circle swept by the blade tip of the propeller 3 and the internal periphery of the tunnel 1 within which the propeller rotates. The compressed gas, e.g. air, is supplied through a duct 4 in the propeller blade and also a duct 8 and 9 in the tunnel housing. The source of air may be a compressor or the ram effect of the airstream together with the centrifugal effect of the rotating blade. A further embodiment also makes use of nozzles connecting with the boundary layer of the blade and the blade duct to induce a flow of air to augment that already in the duct. Exhaust gases may be mixed with compressed air to effect de-icing.
GB2592061A 1960-07-23 1961-07-18 Improvements in or relating to propeller airscrews Expired GB965966A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DER28396A DE1219807B (en) 1960-07-23 1960-07-23 Device for improving the efficiency of a propulsion propeller for aircraft rotating in a tunnel

Publications (1)

Publication Number Publication Date
GB965966A true GB965966A (en) 1964-08-06

Family

ID=7402721

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2592061A Expired GB965966A (en) 1960-07-23 1961-07-18 Improvements in or relating to propeller airscrews

Country Status (2)

Country Link
DE (1) DE1219807B (en)
GB (1) GB965966A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3705700A (en) * 1970-10-23 1972-12-12 Willard R Custer Air flow control means for channel winged aircraft

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5480284A (en) * 1993-12-20 1996-01-02 General Electric Company Self bleeding rotor blade

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE304296C (en) *
DE375598C (en) * 1923-05-15 Jackenkroll Optische Anstalt A Propellers for aircraft
DE400813C (en) * 1922-03-10 1924-08-20 Johann Zagorski Dipl Ing Installation on water or air screws
AT118039B (en) * 1927-06-11 1930-06-10 Leonard Francis Coe Kite plane.
DE636617C (en) * 1932-11-22 1936-10-14 Willy Hof Process for the production of propellers
FR775847A (en) * 1933-09-25 1935-01-10 Method and devices for increasing the efficiency of surfaces working in a mobile environment

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3705700A (en) * 1970-10-23 1972-12-12 Willard R Custer Air flow control means for channel winged aircraft

Also Published As

Publication number Publication date
DE1219807B (en) 1966-06-23

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