GB1291562A - Improvements in or relating to the construction of elongated fibre-reinforced synthetic plastics members, such as propeller blades - Google Patents

Improvements in or relating to the construction of elongated fibre-reinforced synthetic plastics members, such as propeller blades

Info

Publication number
GB1291562A
GB1291562A GB5017168A GB5017168A GB1291562A GB 1291562 A GB1291562 A GB 1291562A GB 5017168 A GB5017168 A GB 5017168A GB 5017168 A GB5017168 A GB 5017168A GB 1291562 A GB1291562 A GB 1291562A
Authority
GB
United Kingdom
Prior art keywords
blade
propeller blades
reinforced
relating
construction
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
GB5017168A
Inventor
Gilroy Reginald Ketley
James William Stevens
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.)
Hawker Siddeley Dynamics Ltd
Original Assignee
Hawker Siddeley Dynamics Ltd
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 Hawker Siddeley Dynamics Ltd filed Critical Hawker Siddeley Dynamics Ltd
Priority to GB5017168A priority Critical patent/GB1291562A/en
Priority to DE19691954062 priority patent/DE1954062A1/en
Priority to FR6936177A priority patent/FR2040956A5/fr
Publication of GB1291562A publication Critical patent/GB1291562A/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
    • B64C11/20—Constructional features
    • B64C11/26—Fabricated blades

Abstract

1291562 Moulding propeller blades HAWKER SIDDELEY DYNAMICS Ltd 16 Oct 1969 [22 Oct 1968] 50171/68 Heading B5A [Also in Division B7] In a method of manufacturing a propeller blade a longitudinal load-carrying spar 11 built up from synthetic resin material reinforced with longitudinally extending carbon fibres is disposed within a containing shell 12. In the embodiment shown two individual half-blades are separately moulded, without a blade shank or root portion, in a reinforced resin material further reinforced with longitudinally laid carbon fibres and are then bonded together. The blade shank and root are then formed by compressing the protruding ends 19 of the carbon whiskers from both halves of the blade between male and female moulds 20, 21.
GB5017168A 1968-10-22 1968-10-22 Improvements in or relating to the construction of elongated fibre-reinforced synthetic plastics members, such as propeller blades Expired GB1291562A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
GB5017168A GB1291562A (en) 1968-10-22 1968-10-22 Improvements in or relating to the construction of elongated fibre-reinforced synthetic plastics members, such as propeller blades
DE19691954062 DE1954062A1 (en) 1968-10-22 1969-10-22 Propeller blade and process for its manufacture
FR6936177A FR2040956A5 (en) 1968-10-22 1969-10-22

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB5017168A GB1291562A (en) 1968-10-22 1968-10-22 Improvements in or relating to the construction of elongated fibre-reinforced synthetic plastics members, such as propeller blades

Publications (1)

Publication Number Publication Date
GB1291562A true GB1291562A (en) 1972-10-04

Family

ID=10454929

Family Applications (1)

Application Number Title Priority Date Filing Date
GB5017168A Expired GB1291562A (en) 1968-10-22 1968-10-22 Improvements in or relating to the construction of elongated fibre-reinforced synthetic plastics members, such as propeller blades

Country Status (3)

Country Link
DE (1) DE1954062A1 (en)
FR (1) FR2040956A5 (en)
GB (1) GB1291562A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5632602A (en) * 1993-10-15 1997-05-27 Deutsche Forschungsanstalt Fur Luft-Und Ramfarht E.V. Rotor blade
FR2955083A1 (en) * 2010-01-14 2011-07-15 Snecma Propeller blade, has member presenting longitudinal axis, where member includes part of oblong section and another part of cylindrical section presenting axis symmetry along longitudinal axis
GB2489546A (en) * 2011-03-30 2012-10-03 Gurit Uk Ltd Water turbine blade with composite spar
US9945389B2 (en) 2014-05-05 2018-04-17 Horton, Inc. Composite fan

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3710321C1 (en) * 1987-03-28 1988-06-01 Mtu Muenchen Gmbh Fan blade, especially for prop fan engines
DE3737894A1 (en) * 1987-11-07 1989-05-18 Ferdinand Dr Lutz Propeller having adjustable blades (variable pitch propeller)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5632602A (en) * 1993-10-15 1997-05-27 Deutsche Forschungsanstalt Fur Luft-Und Ramfarht E.V. Rotor blade
FR2955083A1 (en) * 2010-01-14 2011-07-15 Snecma Propeller blade, has member presenting longitudinal axis, where member includes part of oblong section and another part of cylindrical section presenting axis symmetry along longitudinal axis
GB2489546A (en) * 2011-03-30 2012-10-03 Gurit Uk Ltd Water turbine blade with composite spar
GB2489546B (en) * 2011-03-30 2015-09-23 Gurit Uk Ltd Water-turbine blade
US9945389B2 (en) 2014-05-05 2018-04-17 Horton, Inc. Composite fan
US10415587B2 (en) 2014-05-05 2019-09-17 Horton, Inc. Composite fan and method of manufacture
US10914314B2 (en) 2014-05-05 2021-02-09 Horton, Inc. Modular fan assembly

Also Published As

Publication number Publication date
DE1954062A1 (en) 1970-04-30
FR2040956A5 (en) 1971-01-22

Similar Documents

Publication Publication Date Title
JPS6452595A (en) Wing consisting of composite material and manufacture thereof
NL6614886A (en)
GB1526815A (en) Stress-reducing connecting assembly
GB1507631A (en) Composite rotor blade
GB1319235A (en) Devices of fibrous-reinforced plastics material
GB1250885A (en)
US2659444A (en) Molded aircraft sustaining rotor blade
RU93056603A (en) VENE FROM THERMOPLASTIC COMPOSITE MATERIAL, IN PARTICULAR FOR THE HELICOPTER TAIL OF SCREW, AND METHOD FOR ITS MANUFACTURE
GB1315788A (en) Decorative panel and method of making same
GB1461723A (en) Helicopter blade structuren1461724chun cheng lin feeding bottles
US4538780A (en) Ultralight composite wing structure
GB1291562A (en) Improvements in or relating to the construction of elongated fibre-reinforced synthetic plastics members, such as propeller blades
GB1047734A (en) Improvements in rotor blades for rotary wing assemblies of aircraft
GB1034738A (en) Improved method of bonding together thermo-plastic and thermo-setting materials
GB1228996A (en)
GB836501A (en) Rotor blade construction and retention fitting therefor
ES432010A1 (en) Mould for use in the manufacture of hollow turbine blades and method of use thereof
GB1185510A (en) Method of Manufacturing a Rotor Blade.
GB901075A (en) Improvements relating to compressor blades
GB1166700A (en) Improvements in or relating to the Mounting of Rotor Blades of Rotor Craft
GB860391A (en) A method of manufacturing aeroplane wings and tail units
GB778685A (en) Improvements in or relating to the construction and manufacture of aerofoils and thelike
EP0233700A3 (en) Moulding fibre reinforced composite armour
GB1267571A (en) Rotor blade and propeller blade mountings
GB1227885A (en)

Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee