CA1161014A - Composite leading edge for aircraft - Google Patents
Composite leading edge for aircraftInfo
- 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
Links
- 239000002131 composite material Substances 0.000 title claims description 28
- 230000003628 erosive effect Effects 0.000 claims abstract description 10
- 239000004033 plastic Substances 0.000 claims abstract description 8
- 229920003023 plastic Polymers 0.000 claims abstract description 8
- 239000000835 fiber Substances 0.000 claims 1
- 239000000306 component Substances 0.000 description 53
- 239000000463 material Substances 0.000 description 6
- 229920002430 Fibre-reinforced plastic Polymers 0.000 description 2
- 239000000853 adhesive Substances 0.000 description 2
- 230000001070 adhesive effect Effects 0.000 description 2
- 239000011151 fibre-reinforced plastic Substances 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 238000000465 moulding Methods 0.000 description 2
- 230000001681 protective effect Effects 0.000 description 2
- 230000037303 wrinkles Effects 0.000 description 2
- SLZWEMYSYKOWCG-UHFFFAOYSA-N Etacelasil Chemical compound COCCO[Si](CCCl)(OCCOC)OCCOC SLZWEMYSYKOWCG-UHFFFAOYSA-N 0.000 description 1
- 239000004568 cement Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 239000003365 glass fiber Substances 0.000 description 1
- 230000001788 irregular Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
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
- B64D15/166—De-icing or preventing icing on exterior surfaces of aircraft by mechanical means 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)
- Lining Or Joining Of Plastics Or The Like (AREA)
- Moulding By Coating Moulds (AREA)
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 (en) | 1984-01-24 |
Family
ID=22165149
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA000359080A Expired CA1161014A (en) | 1979-10-03 | 1980-08-27 | Composite leading edge for aircraft |
Country Status (7)
Country | Link |
---|---|
EP (1) | EP0036875A4 (es) |
JP (1) | JPS5657598A (es) |
BR (1) | BR8008855A (es) |
CA (1) | CA1161014A (es) |
ES (1) | ES262183Y (es) |
IT (1) | IT1132967B (es) |
WO (1) | WO1981000993A1 (es) |
Cited By (1)
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 (11)
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 (en) * | 2012-11-20 | 2014-05-30 | Saab Ab | An erosion protection strip for a leading edge of an airfoil article |
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 |
US20190211801A1 (en) * | 2016-06-24 | 2019-07-11 | Lm Wind Power Us Technology Aps | 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 |
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 |
Family Cites Families (5)
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 |
-
1980
- 1980-08-25 WO PCT/US1980/001095 patent/WO1981000993A1/en not_active Application Discontinuation
- 1980-08-25 BR BR8008855A patent/BR8008855A/pt unknown
- 1980-08-27 CA CA000359080A patent/CA1161014A/en not_active Expired
- 1980-09-18 IT IT24753/80A patent/IT1132967B/it active
- 1980-10-02 JP JP13681780A patent/JPS5657598A/ja active Pending
- 1980-10-03 ES ES1980262183U patent/ES262183Y/es not_active Expired
-
1981
- 1981-04-21 EP EP19800901913 patent/EP0036875A4/en not_active Withdrawn
Cited By (1)
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 |
---|---|
ES262183Y (es) | 1982-12-16 |
IT8024753A0 (it) | 1980-09-18 |
WO1981000993A1 (en) | 1981-04-16 |
BR8008855A (pt) | 1981-09-01 |
JPS5657598A (en) | 1981-05-20 |
EP0036875A4 (en) | 1982-07-12 |
ES262183U (es) | 1982-06-01 |
EP0036875A1 (en) | 1981-10-07 |
IT1132967B (it) | 1986-07-09 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
MKEX | Expiry |