JP2007522017A - 航空機用のランディングフラップガイド - Google Patents
航空機用のランディングフラップガイド Download PDFInfo
- Publication number
- JP2007522017A JP2007522017A JP2006552558A JP2006552558A JP2007522017A JP 2007522017 A JP2007522017 A JP 2007522017A JP 2006552558 A JP2006552558 A JP 2006552558A JP 2006552558 A JP2006552558 A JP 2006552558A JP 2007522017 A JP2007522017 A JP 2007522017A
- Authority
- JP
- Japan
- Prior art keywords
- landing flap
- guide
- sliding
- landing
- flap
- 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
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
- B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Bearings For Parts Moving Linearly (AREA)
- Tires In General (AREA)
- Laminated Bodies (AREA)
- Coating By Spraying Or Casting (AREA)
Abstract
【選択図】図1
Description
Claims (5)
- 航空機用のランディングフラップガイドであって、
ガイド要素がランディングフラップに接続され、該フラップがガイドレールに支持されて、離陸位置と着陸位置との間で調整可能とされており、
基本的に直線状のランディングフラップキャリヤ(3)、つまり、当該ランディングフラップキャリヤ(3)の1つ以上の滑りガイド(41、42;43、44)を用いたガイドとしてのキャリヤの形態において、前記ガイド要素(4)が調整可能なスライドとして実現される、ランディングフラップガイド。 - 前記滑りガイドが、1つ以上の滑り要素(41;43)及び割り当てられた凹部(42;44)を備え、該滑り要素が該凹部内へと延びてその内部で滑動するように案内される、請求項1に記載のランディングフラップガイド。
- 第1及び第2の滑りガイド(41、42;43、44)が設けられ、それぞれが3つの滑り対を構成するとともに、基本的にランディングフラップキャリヤ(3)上で垂直に作用する力を、少なくとも吸収するように設計されている、請求項1又は2に記載のランディングフラップガイド。
- ランディングフラップ(1)にかかる空気負荷が第1及び第2の滑り対(43、44)によって吸収され、かつ、質量力が第3の滑り対(43、44)によって吸収される、請求項1乃至3のいずれか一項に記載のランディングフラップガイド。
- 1つ以上の滑りガイド(41、42;43、44)が、以下のグループ、つまり、被覆された金属、被覆なしの金属、セラミック、セラミック又は金属が組み込まれた合成材料、繊維強化合成材料、繊維強化セラミック、プラズマ中で基材に形成されるカーボン層のうち、1つ以上の材料で形成された滑り表面を有する、請求項1乃至4のいずれか一項に記載のランディングフラップガイド。
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102004006940A DE102004006940B4 (de) | 2004-02-12 | 2004-02-12 | Landeklappenführung für Luftfahrzeuge |
US60664604P | 2004-09-02 | 2004-09-02 | |
PCT/EP2005/001391 WO2005077756A1 (en) | 2004-02-12 | 2005-02-11 | Landing flap guide for aircraft |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2007522017A true JP2007522017A (ja) | 2007-08-09 |
JP4571953B2 JP4571953B2 (ja) | 2010-10-27 |
Family
ID=34832624
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2006552558A Expired - Fee Related JP4571953B2 (ja) | 2004-02-12 | 2005-02-11 | 航空機用のランディングフラップガイド |
Country Status (8)
Country | Link |
---|---|
US (1) | US7857263B2 (ja) |
EP (1) | EP1713688B1 (ja) |
JP (1) | JP4571953B2 (ja) |
CN (1) | CN1918033B (ja) |
BR (1) | BRPI0506586A (ja) |
CA (1) | CA2554067C (ja) |
DE (1) | DE102004006940B4 (ja) |
WO (1) | WO2005077756A1 (ja) |
Families Citing this family (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102006036464B4 (de) * | 2006-08-04 | 2009-08-20 | Airbus Deutschland Gmbh | Hochauftriebssystem für ein Flugzeug |
DE102007036996A1 (de) * | 2007-08-06 | 2009-02-19 | Airbus Deutschland Gmbh | Hochauftriebssystem für ein Flugzeug |
GB0810460D0 (en) * | 2008-06-09 | 2008-07-09 | Airbus Uk Ltd | Support assembly |
GB0810584D0 (en) * | 2008-06-11 | 2008-07-16 | Airbus Uk Ltd | Aircraft wing assembly |
DE102009039967A1 (de) * | 2009-09-03 | 2011-03-10 | Airbus Operations Gmbh | Verstellmechanismus zur kinematischen Führung eines Verstellkörpers bei dessen Verstellung an einem tragenden Strukturteil, Verstellmechanismus zur kinematischen Verstellung eines Hochauftriebskörpers sowie Hochauftriebssystem mit einem solchen Verstellmechanismus |
US9359972B2 (en) | 2011-08-31 | 2016-06-07 | United Technologies Corporation | Multi axis slide carriage system |
DE102011082888B4 (de) * | 2011-09-16 | 2016-01-07 | Airbus Defence and Space GmbH | Auftriebsklappenanordnung, Tragflügel sowie Flugzeug |
GB201209686D0 (en) | 2012-05-31 | 2012-07-18 | Airbus Operations Ltd | A slat support assembly |
WO2014209714A1 (en) * | 2013-06-26 | 2014-12-31 | Learjet Inc. | Mechanism for trailing edge control surface |
EP2942272A1 (en) * | 2014-05-09 | 2015-11-11 | Airbus Operations GmbH | An aircraft wing and an aircraft comprising such aircraft wing |
EP3025955B1 (de) | 2014-11-26 | 2019-06-19 | Airbus Defence and Space GmbH | Hochauftriebssystem |
BE1024276B1 (fr) * | 2016-11-04 | 2018-01-11 | Sonaca Sa | Aile d’aeronef comprenant un volet mobile de bord de fuite entraine par un moteur electrique lineaire |
ES2878314T3 (es) | 2017-04-26 | 2021-11-18 | Asco Ind Nv | Conjunto de guía para una pista portadora del dispositivo hipersustentador del borde delantero aerodinámico |
US20190127047A1 (en) * | 2017-10-30 | 2019-05-02 | Airbus Operations Gmbh | Carriage for supporting and guiding a flap and airfoil flap system for use in an aircraft |
EP3501977B1 (en) | 2017-12-19 | 2021-08-11 | Asco Industries NV | Deployment system for an airfoil high lift leading edge device |
EP3878734B1 (en) * | 2020-03-11 | 2023-07-19 | Airbus Operations GmbH | Guiding element for a high lift airfoil arrangement of an aircraft, high lift airfoil arrangement and production method |
CN113697087B (zh) * | 2021-08-13 | 2024-06-11 | 航天时代飞鹏有限公司 | 一种大型货运无人机着陆构型及其设计方法 |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3767140A (en) * | 1971-11-03 | 1973-10-23 | Mc Donnell Douglas Corp | Airplane flaps |
US4381093A (en) * | 1980-10-07 | 1983-04-26 | The Boeing Company | Flap assembly for aircraft wing |
JPS6467495A (en) * | 1987-08-11 | 1989-03-14 | British Aerospace | Trailing edge flap for aircraft wing |
US5094412A (en) * | 1989-10-13 | 1992-03-10 | Bell Helicopter Textron Inc. | Flaperon system for tilt rotor wings |
US5199538A (en) * | 1989-02-23 | 1993-04-06 | Zahnradfabrik Friedrichshafen Ag | Drive device with variable torque-limiting system |
US5230487A (en) * | 1991-03-08 | 1993-07-27 | Deutsche Aerospace Airbus Gmbh | Apparatus for driving and guiding a flap secured to an aircraft wing |
WO2003035469A1 (de) * | 2001-10-24 | 2003-05-01 | Fischer Advanced Composite Components Ag | Trag- bzw. führungsvorrichtung für flugzeugkomponenten |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1075439B (de) * | 1960-02-11 | Societe de Brevets H.D., Paris | Flugzeugtragfläche mit Klappen längs der Hinterkante zur Auftriebserhöhung | |
DE698114C (de) * | 1938-03-26 | 1940-11-01 | Dornier Werke Gmbh | Rollfluegel |
AT335101B (de) | 1972-10-28 | 1977-02-25 | Rensch Eberhard | Bausatz zur montage von mobeln |
DE2949293A1 (de) | 1979-12-07 | 1981-06-11 | GRS Gesellschaft für Raketen-Systeme mbH, 5300 Bonn | Klappleitwerk fuer durch raketentreibsaetze angetriebene flugkoerper |
DE3713465A1 (de) | 1987-04-22 | 1988-11-10 | Messerschmitt Boelkow Blohm | Tandem-landeklappenwagen |
RU2022879C1 (ru) | 1991-04-09 | 1994-11-15 | Авиационный научно-технический комплекс им.О.К.Антонова | Носок крыла самолета |
US5681013A (en) | 1995-12-26 | 1997-10-28 | The Boeing Company | Vortex leading edge flap assembly for supersonic airplanes |
DE19732953C1 (de) | 1997-07-31 | 1999-03-11 | Daimler Benz Ag | Tragflügel mit Landeklappe |
JP2001127969A (ja) | 1999-10-26 | 2001-05-11 | Canon Inc | 画像通信装置 |
-
2004
- 2004-02-12 DE DE102004006940A patent/DE102004006940B4/de not_active Expired - Fee Related
-
2005
- 2005-02-11 CA CA2554067A patent/CA2554067C/en not_active Expired - Fee Related
- 2005-02-11 CN CN2005800047581A patent/CN1918033B/zh not_active Expired - Fee Related
- 2005-02-11 WO PCT/EP2005/001391 patent/WO2005077756A1/en active Application Filing
- 2005-02-11 BR BRPI0506586-0A patent/BRPI0506586A/pt not_active Application Discontinuation
- 2005-02-11 JP JP2006552558A patent/JP4571953B2/ja not_active Expired - Fee Related
- 2005-02-11 US US10/589,120 patent/US7857263B2/en not_active Expired - Fee Related
- 2005-02-11 EP EP05707337A patent/EP1713688B1/en not_active Not-in-force
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3767140A (en) * | 1971-11-03 | 1973-10-23 | Mc Donnell Douglas Corp | Airplane flaps |
US4381093A (en) * | 1980-10-07 | 1983-04-26 | The Boeing Company | Flap assembly for aircraft wing |
JPS6467495A (en) * | 1987-08-11 | 1989-03-14 | British Aerospace | Trailing edge flap for aircraft wing |
US5199538A (en) * | 1989-02-23 | 1993-04-06 | Zahnradfabrik Friedrichshafen Ag | Drive device with variable torque-limiting system |
US5094412A (en) * | 1989-10-13 | 1992-03-10 | Bell Helicopter Textron Inc. | Flaperon system for tilt rotor wings |
US5230487A (en) * | 1991-03-08 | 1993-07-27 | Deutsche Aerospace Airbus Gmbh | Apparatus for driving and guiding a flap secured to an aircraft wing |
WO2003035469A1 (de) * | 2001-10-24 | 2003-05-01 | Fischer Advanced Composite Components Ag | Trag- bzw. führungsvorrichtung für flugzeugkomponenten |
Also Published As
Publication number | Publication date |
---|---|
CA2554067A1 (en) | 2005-08-25 |
BRPI0506586A (pt) | 2007-05-02 |
WO2005077756A1 (en) | 2005-08-25 |
EP1713688B1 (en) | 2010-07-28 |
US20080042009A1 (en) | 2008-02-21 |
CN1918033B (zh) | 2011-11-09 |
DE102004006940A1 (de) | 2005-09-08 |
CN1918033A (zh) | 2007-02-21 |
CA2554067C (en) | 2012-10-09 |
EP1713688A1 (en) | 2006-10-25 |
DE102004006940B4 (de) | 2009-02-26 |
US7857263B2 (en) | 2010-12-28 |
JP4571953B2 (ja) | 2010-10-27 |
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