CA1161014A - Bord d'attaque composite pour aeronef - Google Patents

Bord d'attaque composite pour aeronef

Info

Publication number
CA1161014A
CA1161014A CA000359080A CA359080A CA1161014A CA 1161014 A CA1161014 A CA 1161014A CA 000359080 A CA000359080 A CA 000359080A CA 359080 A CA359080 A CA 359080A CA 1161014 A CA1161014 A CA 1161014A
Authority
CA
Canada
Prior art keywords
component
leading edge
shoe
aircraft
deicer
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
CA000359080A
Other languages
English (en)
Inventor
Ted W. Blaser
Norbert A. Weisend, Jr.
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.)
Goodrich Corp
Original Assignee
BF Goodrich 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 BF Goodrich Corp filed Critical BF Goodrich Corp
Application granted granted Critical
Publication of CA1161014A publication Critical patent/CA1161014A/fr
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D15/00De-icing or preventing icing on exterior surfaces of aircraft
    • B64D15/16De-icing or preventing icing on exterior surfaces of aircraft by mechanical means, e.g. pulsating mats or shoes attached to, or built into, surface
    • B64D15/166De-icing or preventing icing on exterior surfaces of aircraft by mechanical means, e.g. pulsating mats or shoes attached to, or built into, surface using pneumatic boots
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/42Housings not intimately mechanically associated with radiating elements, e.g. radome
    • H01Q1/422Housings not intimately mechanically associated with radiating elements, e.g. radome comprising two or more layers of dielectric material

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Moulds For Moulding Plastics Or The Like (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)
  • Moulding By Coating Moulds (AREA)
CA000359080A 1979-10-03 1980-08-27 Bord d'attaque composite pour aeronef Expired CA1161014A (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US8159779A 1979-10-03 1979-10-03
US081,597 1979-10-03

Publications (1)

Publication Number Publication Date
CA1161014A true CA1161014A (fr) 1984-01-24

Family

ID=22165149

Family Applications (1)

Application Number Title Priority Date Filing Date
CA000359080A Expired CA1161014A (fr) 1979-10-03 1980-08-27 Bord d'attaque composite pour aeronef

Country Status (7)

Country Link
EP (1) EP0036875A4 (fr)
JP (1) JPS5657598A (fr)
BR (1) BR8008855A (fr)
CA (1) CA1161014A (fr)
ES (1) ES262183Y (fr)
IT (1) IT1132967B (fr)
WO (1) WO1981000993A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5288355A (en) * 1989-11-06 1994-02-22 The B.F. Goodrich Company Structural airfoil having integral expulsive system

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB8821741D0 (en) * 1988-09-14 1989-09-13 British Aerospace Radomes
US5449134A (en) * 1993-09-24 1995-09-12 The B. F. Goodrich Company Apparatus and method for providing a pneumatic de-icer with a replaceable environment resistant surface
US6662715B2 (en) * 2000-07-21 2003-12-16 Aida Engineering Co., Ltd. Slider link press
JP3709485B1 (ja) * 2004-10-08 2005-10-26 株式会社昭和 ライニング構造
US8043065B2 (en) * 2009-05-01 2011-10-25 General Electric Company Wind turbine blade with prefabricated leading edge segments
WO2014081355A1 (fr) 2012-11-20 2014-05-30 Saab Ab Bande de protection contre l'érosion pour bord d'attaque d'article à profil aérodynamique
CN103318419B (zh) * 2013-05-20 2016-01-20 西安电子工程研究所 机载电子吊舱舱体与天线罩套接密封结构
ES2929189T3 (es) * 2016-06-24 2022-11-25 Lm Wind Power As Pala de turbina eólica y procedimiento de fabricación de una pala de turbina eólica
US10273012B2 (en) * 2016-09-08 2019-04-30 Ge Aviation Systems Llc Deicing module for an aircraft and method for deicing
KR102197433B1 (ko) * 2017-03-21 2021-01-04 엠에이치아이 베스타스 오프쇼어 윈드 에이/에스 풍력 터빈 블레이드, 풍력 터빈 로터 및 풍력 터빈 발전 장치
GB2573286B (en) * 2018-04-27 2020-10-14 Airbus Operations Ltd Winglet
US12313031B2 (en) 2018-12-21 2025-05-27 Lm Wind Power Us Technology Aps Wind turbine blade and method of manufacturing a wind turbine blade

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2393635A (en) * 1942-04-17 1946-01-29 Robert H Wendt Ice removing device for aircraft
US2762897A (en) * 1951-06-28 1956-09-11 Lockheed Aircraft Corp De-icing means for aircraft and the like
US2956281A (en) * 1954-09-08 1960-10-11 Edward B Mcmillan Dielectric walls for transmission of electromagnetic radiation
US3085925A (en) * 1957-02-20 1963-04-16 Konenklijke Nl Vliegtuigenfabr Method of forming an aircraft part having a pliable deicer boot thereon
FR2354242A1 (fr) * 1976-06-11 1978-01-06 Paulstra Sa Perfectionnements apportes aux surfaces alaires, plus specialement aux pales d'helicopteres, munies de moyens de degivrage

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5288355A (en) * 1989-11-06 1994-02-22 The B.F. Goodrich Company Structural airfoil having integral expulsive system

Also Published As

Publication number Publication date
EP0036875A4 (fr) 1982-07-12
IT1132967B (it) 1986-07-09
ES262183Y (es) 1982-12-16
IT8024753A0 (it) 1980-09-18
WO1981000993A1 (fr) 1981-04-16
ES262183U (es) 1982-06-01
BR8008855A (pt) 1981-09-01
EP0036875A1 (fr) 1981-10-07
JPS5657598A (en) 1981-05-20

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Legal Events

Date Code Title Description
MKEX Expiry