WO2012174306A3 - Split circumference aircraft wheel assembly with integrated drive motor assembly - Google Patents
Split circumference aircraft wheel assembly with integrated drive motor assembly Download PDFInfo
- Publication number
- WO2012174306A3 WO2012174306A3 PCT/US2012/042547 US2012042547W WO2012174306A3 WO 2012174306 A3 WO2012174306 A3 WO 2012174306A3 US 2012042547 W US2012042547 W US 2012042547W WO 2012174306 A3 WO2012174306 A3 WO 2012174306A3
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- wheel
- assembly
- aircraft
- motor driver
- maximized
- Prior art date
Links
Classifications
-
- 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
- B60—VEHICLES IN GENERAL
- B60B—VEHICLE WHEELS; CASTORS; AXLES FOR WHEELS OR CASTORS; INCREASING WHEEL ADHESION
- B60B25/00—Rims built-up of several main parts ; Locking means for the rim parts
- B60B25/002—Rims split in circumferential direction
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60B—VEHICLE WHEELS; CASTORS; AXLES FOR WHEELS OR CASTORS; INCREASING WHEEL ADHESION
- B60B25/00—Rims built-up of several main parts ; Locking means for the rim parts
- B60B25/04—Rims with dismountable flange rings, seat rings, or lock rings
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Arrangement And Driving Of Transmission Devices (AREA)
- Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)
Abstract
A split circumference wheel assembly is provided for an aircraft landing gear wheel configured to maximize the space available within a landing gear wheel well to support a motor driver assembly with drive means that drives the aircraft wheel on the ground. The split circumference wheel assembly includes separable inboard and outboard support walls that are spaced axially apart a maximized distance so that the motor driver assembly is completely contained within the maximized space defined. A preferred wheel assembly employs a demountable flange and a locking ring to integrally and removably support the motor driver assembly within the maximized wheel volume to drive one or more aircraft wheels and move the aircraft independently on the ground. The wheel and motor driver assembly described herein are designed to be retrofitted in an existing aircraft wheel.
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201161496766P | 2011-06-14 | 2011-06-14 | |
US61/496,766 | 2011-06-14 | ||
US201213021373A | 2012-06-14 | 2012-06-14 | |
US13/021,373 | 2012-06-14 |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2012174306A2 WO2012174306A2 (en) | 2012-12-20 |
WO2012174306A3 true WO2012174306A3 (en) | 2014-05-01 |
Family
ID=47357747
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US2012/042547 WO2012174306A2 (en) | 2011-06-14 | 2012-06-14 | Split circumference aircraft wheel assembly with integrated drive motor assembly |
Country Status (1)
Country | Link |
---|---|
WO (1) | WO2012174306A2 (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP6275699B2 (en) | 2012-05-25 | 2018-02-07 | ジェネシス アドバンスド テクノロジー インコーポレイテッド. | Transmission |
Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2834636A (en) * | 1953-10-28 | 1958-05-13 | Thomas L Fawick | Forged wheel |
US4209052A (en) * | 1978-10-23 | 1980-06-24 | Goodyear Aerospace Corporation | Wheel flange retaining ring |
US5086821A (en) * | 1990-01-23 | 1992-02-11 | The B. F. Goodrich Company | Aircraft wheel |
US20070158497A1 (en) * | 2003-10-09 | 2007-07-12 | Edelson Jonathan S | Geared wheel motor design |
US7445178B2 (en) * | 2004-09-28 | 2008-11-04 | The Boeing Company | Powered nose aircraft wheel system |
US20090114765A1 (en) * | 2007-11-06 | 2009-05-07 | Isaiah Watas Cox | Motor for driving aircraft, located adjacent to undercarriage wheel |
US20100206980A1 (en) * | 2008-12-16 | 2010-08-19 | Airbus | Motorized undercarriage for aircraft |
US20100276535A1 (en) * | 2009-04-24 | 2010-11-04 | Messier Bugatti | Method of taxiing an aircraft |
US20110089289A1 (en) * | 2008-04-11 | 2011-04-21 | Airbus Operations Limited | Aircraft landing gear arrangement and a nose landing gear assembly |
US20110284685A1 (en) * | 2010-03-29 | 2011-11-24 | Borealis Technical Limited | Wheel Structure for Integrating an Electric Drive Motor |
US20110297786A1 (en) * | 2010-04-08 | 2011-12-08 | Borealis Technical Limited | Integrated Electric Motor and Gear in an Aircraft Wheel |
-
2012
- 2012-06-14 WO PCT/US2012/042547 patent/WO2012174306A2/en active Application Filing
Patent Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2834636A (en) * | 1953-10-28 | 1958-05-13 | Thomas L Fawick | Forged wheel |
US4209052A (en) * | 1978-10-23 | 1980-06-24 | Goodyear Aerospace Corporation | Wheel flange retaining ring |
US5086821A (en) * | 1990-01-23 | 1992-02-11 | The B. F. Goodrich Company | Aircraft wheel |
US20070158497A1 (en) * | 2003-10-09 | 2007-07-12 | Edelson Jonathan S | Geared wheel motor design |
US7445178B2 (en) * | 2004-09-28 | 2008-11-04 | The Boeing Company | Powered nose aircraft wheel system |
US20090114765A1 (en) * | 2007-11-06 | 2009-05-07 | Isaiah Watas Cox | Motor for driving aircraft, located adjacent to undercarriage wheel |
US20110089289A1 (en) * | 2008-04-11 | 2011-04-21 | Airbus Operations Limited | Aircraft landing gear arrangement and a nose landing gear assembly |
US20100206980A1 (en) * | 2008-12-16 | 2010-08-19 | Airbus | Motorized undercarriage for aircraft |
US20100276535A1 (en) * | 2009-04-24 | 2010-11-04 | Messier Bugatti | Method of taxiing an aircraft |
US20110284685A1 (en) * | 2010-03-29 | 2011-11-24 | Borealis Technical Limited | Wheel Structure for Integrating an Electric Drive Motor |
US20110297786A1 (en) * | 2010-04-08 | 2011-12-08 | Borealis Technical Limited | Integrated Electric Motor and Gear in an Aircraft Wheel |
Also Published As
Publication number | Publication date |
---|---|
WO2012174306A2 (en) | 2012-12-20 |
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