GB2315723B - A low-vulnerability helicopter rotor blade - Google Patents

A low-vulnerability helicopter rotor blade

Info

Publication number
GB2315723B
GB2315723B GB8623981A GB8623981A GB2315723B GB 2315723 B GB2315723 B GB 2315723B GB 8623981 A GB8623981 A GB 8623981A GB 8623981 A GB8623981 A GB 8623981A GB 2315723 B GB2315723 B GB 2315723B
Authority
GB
United Kingdom
Prior art keywords
vulnerability
low
rotor blade
helicopter rotor
helicopter
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 - Fee Related
Application number
GB8623981A
Other versions
GB8623981D0 (en
GB2315723A (en
Inventor
Gilbert Francois Baziac
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.)
Airbus Group SAS
Original Assignee
Airbus Group SAS
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 Airbus Group SAS filed Critical Airbus Group SAS
Publication of GB8623981D0 publication Critical patent/GB8623981D0/en
Publication of GB2315723A publication Critical patent/GB2315723A/en
Application granted granted Critical
Publication of GB2315723B publication Critical patent/GB2315723B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/32—Rotors
    • B64C27/46—Blades
    • B64C27/473—Constructional features
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/32—Rotors
    • B64C27/46—Blades
    • B64C27/473—Constructional features
    • B64C2027/4733—Rotor blades substantially made from particular materials
    • B64C2027/4736—Rotor blades substantially made from particular materials from composite materials

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)
  • Moulding By Coating Moulds (AREA)
GB8623981A 1985-10-09 1986-10-06 A low-vulnerability helicopter rotor blade Expired - Fee Related GB2315723B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8514926A FR2748718B1 (en) 1985-10-09 1985-10-09 REDUCED VULNERABILITY BLADE FOR ROTORS OF GIRAVIONS, AND MANUFACTURING METHOD THEREOF

Publications (3)

Publication Number Publication Date
GB8623981D0 GB8623981D0 (en) 1997-11-19
GB2315723A GB2315723A (en) 1998-02-11
GB2315723B true GB2315723B (en) 1998-06-24

Family

ID=9323654

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8623981A Expired - Fee Related GB2315723B (en) 1985-10-09 1986-10-06 A low-vulnerability helicopter rotor blade

Country Status (5)

Country Link
CA (1) CA1340478C (en)
DE (1) DE3634510C1 (en)
FR (1) FR2748718B1 (en)
GB (1) GB2315723B (en)
IT (1) IT8621803A0 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11767098B2 (en) 2019-01-15 2023-09-26 Safran Aircraft Engines Propeller blade or vane for an aircraft with particular weaving of a fibre preform receiving a bladder filled with a shaping foam

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8282040B1 (en) 2009-04-30 2012-10-09 Lockheed Martin Corporation Composite aircraft wing
US11015461B2 (en) * 2017-12-21 2021-05-25 General Electric Company Composite hollow blade and a method of forming the composite hollow blade

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1275279B (en) * 1965-10-06 1968-08-14 Boelkow Gmbh Process for the production of a composite component from glass fiber reinforced plastic
US4083656A (en) * 1975-03-21 1978-04-11 Textron, Inc. Composite rotor blade
US4316701A (en) * 1976-08-30 1982-02-23 The Boeing Company Composite aerodynamic rotor blade assembly
US4316700A (en) * 1979-04-03 1982-02-23 Schramm Burford J Unitary, bonded-together helicopter rotorblade
ZA849482B (en) * 1983-12-19 1985-07-31 Goodyear Tire & Rubber A braided spiral reinforced hose and method for producing same

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11767098B2 (en) 2019-01-15 2023-09-26 Safran Aircraft Engines Propeller blade or vane for an aircraft with particular weaving of a fibre preform receiving a bladder filled with a shaping foam

Also Published As

Publication number Publication date
CA1340478C (en) 1999-04-06
GB8623981D0 (en) 1997-11-19
DE3634510C1 (en) 1998-02-26
IT8621803A0 (en) 1986-09-24
FR2748718B1 (en) 1998-12-24
FR2748718A1 (en) 1997-11-21
GB2315723A (en) 1998-02-11

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Legal Events

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

Effective date: 20021006