JP5918185B2 - 車輪を保持する降着装置に航空機車輪の駆動部材を固定する方法 - Google Patents
車輪を保持する降着装置に航空機車輪の駆動部材を固定する方法 Download PDFInfo
- Publication number
- JP5918185B2 JP5918185B2 JP2013184938A JP2013184938A JP5918185B2 JP 5918185 B2 JP5918185 B2 JP 5918185B2 JP 2013184938 A JP2013184938 A JP 2013184938A JP 2013184938 A JP2013184938 A JP 2013184938A JP 5918185 B2 JP5918185 B2 JP 5918185B2
- Authority
- JP
- Japan
- Prior art keywords
- torque plate
- support
- drive member
- landing gear
- brake
- 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.)
- Active
Links
- 238000000034 method Methods 0.000 title claims description 14
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000013461 design Methods 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
Images
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/405—Powered wheels, e.g. for taxing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/34—Alighting gear characterised by elements which contact the ground or similar surface wheeled type, e.g. multi-wheeled bogies
- B64C25/36—Arrangements or adaptations of wheels, tyres or axles in general
-
- 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
- Y02T50/80—Energy efficient operational measures, e.g. ground operations or mission management
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49826—Assembling or joining
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49826—Assembling or joining
- Y10T29/49947—Assembling or joining by applying separate fastener
- Y10T29/49948—Multipart cooperating fastener [e.g., bolt and nut]
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Braking Arrangements (AREA)
Description
Claims (7)
- 航空機の車輪の駆動部材(30)を、車軸(1)を備える降着装置に取り付ける方法であって、前記車軸(1)は、前記車輪を保持するとともに、外側面を含むトルクプレート(3)を有し、該外側面に対してブレーキを取り付け可能である、方法において、
前記トルクプレートの前記外側面とは反対の、前記トルクプレートの内側面に対して当接する支持部(10、110、210)を取り付けるステップと、
前記支持部に前記駆動部材を取り付けるステップと、を備える、方法。 - 前記支持部(10)は、2つの支持部半体を備え、
該2つの支持部半体の各々は、前記トルクプレートの内側面に対して取り付けられ、前記トルクプレートにボルト止めされる、請求項1に記載の方法。 - 前記支持部は、少なくとも1つのボルト(20)を用いることによって、前記トルクプレートに固定され、
前記ボルト(20)は、前記トルクプレートの開口に挿入され、且つ、螺子付ボルトシャンク(21)を有し、
該螺子付ボルトシャンク(21)に、ナット(22)が取り付けられ、該螺子付ボルトシャンク(21)のヘッド(25)と該ナット(22)との間で、前記支持部と前記トルクプレートとが互いにクランプされる、請求項1に記載の方法。 - 前記ボルトシャンクは、該ボルトシャンクを前記トルクプレートの開口内でセンタリングするための滑らかな部分(23)を有する、請求項3に記載の方法。
- 前記ボルトのヘッド(25)は、前記ブレーキを前記トルクプレートに対して位置決めするために、小さな寸法の周方向のクリアランスを伴って、前記ブレーキのスポット面内に受容される、請求項4に記載の方法。
- 前記支持部は、1つの部材(110、210)として作製され、該支持部を前記トルクプレートの内側面に対して配置可能とするための開口を有する、請求項1に記載の方法。
- 前記支持部(210)は、該支持部(210)を前記トルクプレートの周縁上にてセンタリングするためのカラー部(211)を備える、請求項2に記載の方法。
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1258715A FR2995587B1 (fr) | 2012-09-17 | 2012-09-17 | Procede de fixation d'un organe d'entrainement de roue d'aeronef sur l'atterrisseur portant la roue. |
FR1258715 | 2012-09-17 |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2014058303A JP2014058303A (ja) | 2014-04-03 |
JP5918185B2 true JP5918185B2 (ja) | 2016-05-18 |
Family
ID=47257923
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2013184938A Active JP5918185B2 (ja) | 2012-09-17 | 2013-09-06 | 車輪を保持する降着装置に航空機車輪の駆動部材を固定する方法 |
Country Status (7)
Country | Link |
---|---|
US (1) | US9981737B2 (ja) |
EP (1) | EP2708465B1 (ja) |
JP (1) | JP5918185B2 (ja) |
CN (1) | CN103661933B (ja) |
BR (1) | BR102013022547B1 (ja) |
CA (1) | CA2826489C (ja) |
FR (1) | FR2995587B1 (ja) |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3977631A (en) * | 1975-06-04 | 1976-08-31 | The Boeing Company | Aircraft wheel drive apparatus and method |
JPS59118502A (ja) * | 1982-12-24 | 1984-07-09 | Hayashi Lacing:Kk | 自動車用ホイ−ルの着脱機構 |
JP3052090B2 (ja) * | 1990-11-28 | 2000-06-12 | 利臣 鈴木 | 航空機の降着装置及び制御システム |
US6354408B1 (en) * | 1999-12-13 | 2002-03-12 | Alliedsignal Truck Brake Systems Company | Adapter plate for disc brake installation |
FR2862280B1 (fr) * | 2003-11-14 | 2006-03-03 | Messier Bugatti | Atterrisseur, frein pour roue d'aeronef, ensemble de roue freinee d'aeronef, et procede de maintenance d'un tel atterrisseur |
US20070284939A1 (en) * | 2006-06-12 | 2007-12-13 | Honeywell International | Aircraft electric brake and generator therefor |
DE102008006295B4 (de) * | 2008-01-28 | 2018-05-03 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Angetriebenes flugzeugfahrwerk |
JP5306752B2 (ja) * | 2008-09-12 | 2013-10-02 | 株式会社ハーモニック・ドライブ・システムズ | 航空機の自走式車輪装置 |
FR2944775B1 (fr) * | 2009-04-24 | 2013-03-08 | Messier Bugatti | Procede de deplacement d'un aeronef au sol |
FR2954752B1 (fr) * | 2009-12-24 | 2012-03-09 | Messier Bugatti | Ensemble de roue et frein pour aeronef equipe d'un dispositif d'entrainement en rotation. |
US8714481B2 (en) * | 2010-04-08 | 2014-05-06 | Borealis Technical Limited | Integrated electric motor and gear in an aircraft wheel |
FR2961170B1 (fr) * | 2010-06-10 | 2013-02-22 | Messier Bugatti | Dispositif de deplacement autonome pour aeronef. |
FR2970698B1 (fr) * | 2011-01-21 | 2013-10-04 | Messier Dowty Sa | Dispositif de freinage et d'entrainement en rotation d'une roue d'aeronef |
-
2012
- 2012-09-17 FR FR1258715A patent/FR2995587B1/fr active Active
-
2013
- 2013-08-23 EP EP13181627.4A patent/EP2708465B1/fr active Active
- 2013-08-26 US US13/975,592 patent/US9981737B2/en active Active
- 2013-09-03 BR BR102013022547-9A patent/BR102013022547B1/pt active IP Right Grant
- 2013-09-05 CA CA2826489A patent/CA2826489C/fr active Active
- 2013-09-06 JP JP2013184938A patent/JP5918185B2/ja active Active
- 2013-09-11 CN CN201310413320.5A patent/CN103661933B/zh active Active
Also Published As
Publication number | Publication date |
---|---|
EP2708465A1 (fr) | 2014-03-19 |
US20140075739A1 (en) | 2014-03-20 |
BR102013022547A2 (pt) | 2015-08-11 |
CA2826489A1 (fr) | 2014-03-17 |
FR2995587A1 (fr) | 2014-03-21 |
CN103661933A (zh) | 2014-03-26 |
EP2708465B1 (fr) | 2016-11-30 |
CN103661933B (zh) | 2017-06-06 |
JP2014058303A (ja) | 2014-04-03 |
CA2826489C (fr) | 2017-05-16 |
FR2995587B1 (fr) | 2014-10-10 |
BR102013022547B1 (pt) | 2021-06-29 |
US9981737B2 (en) | 2018-05-29 |
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