ES262183U - Composite leading edge for aircraft. - Google Patents

Composite leading edge for aircraft.

Info

Publication number
ES262183U
ES262183U ES1980262183U ES262183U ES262183U ES 262183 U ES262183 U ES 262183U ES 1980262183 U ES1980262183 U ES 1980262183U ES 262183 U ES262183 U ES 262183U ES 262183 U ES262183 U ES 262183U
Authority
ES
Spain
Prior art keywords
leading edge
aircraft
deicer
erosion
replaceable
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.)
Granted
Application number
ES1980262183U
Other languages
Spanish (es)
Other versions
ES262183Y (en
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
Publication of ES262183U publication Critical patent/ES262183U/en
Application granted granted Critical
Publication of ES262183Y publication Critical patent/ES262183Y/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
    • B64D15/16—De-icing or preventing icing on exterior surfaces of aircraft by mechanical means, e.g. pulsating mats or shoes attached to, or built into, surface
    • B64D15/166—De-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
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00—Details of, or arrangements associated with, antennas
    • H01Q1/42—Housings not intimately mechanically associated with radiating elements, e.g. radome
    • H01Q1/422—Housings 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)
  • Moulding By Coating Moulds (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)

Abstract

A mold-formed, replaceable nonmetallic aircraft leading edge portion (14) comprises an inner, rigid member (24) and an outer, flexible, elastomeric member (20). The outer member may be a deicer or erosion shoe while the inner member may be of suitable plastic. The mold-formed, replaceable nonmetallic leading edge portion (14) forming the leading edge of the wings or the aircraft nose section ensure that these critically contoured aircraft components remain aerodynamically suitable even though they carry elastomeric deicer or erosion shoes.
ES1980262183U 1979-10-03 1980-10-03 A PORTION OF REMOVABLE ATTACK EDGE. Expired ES262183Y (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US8159779A 1979-10-03 1979-10-03

Publications (2)

Publication Number Publication Date
ES262183U true ES262183U (en) 1982-06-01
ES262183Y ES262183Y (en) 1982-12-16

Family

ID=22165149

Family Applications (1)

Application Number Title Priority Date Filing Date
ES1980262183U Expired ES262183Y (en) 1979-10-03 1980-10-03 A PORTION OF REMOVABLE ATTACK EDGE.

Country Status (7)

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

Families Citing this family (13)

* 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
US5098037A (en) * 1989-11-06 1992-03-24 The B. F. Goodrich Company Structural airfoil having integral expulsive system
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 (en) * 2004-10-08 2005-10-26 株式会社昭和 Lining structure
US8043065B2 (en) * 2009-05-01 2011-10-25 General Electric Company Wind turbine blade with prefabricated leading edge segments
WO2014081355A1 (en) * 2012-11-20 2014-05-30 Saab Ab An erosion protection strip for a leading edge of an airfoil article
CN103318419B (en) * 2013-05-20 2016-01-20 西安电子工程研究所 Airborne electronic equipment pod body and radome muff-coupling sealing structure
CN115992793A (en) * 2016-06-24 2023-04-21 Lm风力发电国际技术有限公司 Wind turbine blade and method of manufacturing a wind turbine blade
US10273012B2 (en) * 2016-09-08 2019-04-30 Ge Aviation Systems Llc Deicing module for an aircraft and method for deicing
JP6860683B2 (en) 2017-03-21 2021-04-21 エムエイチアイ ヴェスタス オフショア ウィンド エー／エス Windmill blades, windmill rotors and wind power generators
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 (en) * 1976-06-11 1978-01-06 Paulstra Sa IMPROVEMENTS MADE TO RANGING SURFACES, MORE SPECIFICALLY TO HELICOPTER BLADES, EQUIPPED WITH DEFROSTING MEANS

Also Published As

Publication number Publication date
EP0036875A4 (en) 1982-07-12
CA1161014A (en) 1984-01-24
BR8008855A (en) 1981-09-01
JPS5657598A (en) 1981-05-20
EP0036875A1 (en) 1981-10-07
IT1132967B (en) 1986-07-09
IT8024753A0 (en) 1980-09-18
WO1981000993A1 (en) 1981-04-16
ES262183Y (en) 1982-12-16

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