WO2014070033A3 - Automated wheel turn speed adjustment system for aircraft landing aimed at reducing aircraft tire wear - Google Patents
Automated wheel turn speed adjustment system for aircraft landing aimed at reducing aircraft tire wear Download PDFInfo
- Publication number
- WO2014070033A3 WO2014070033A3 PCT/RO2013/000004 RO2013000004W WO2014070033A3 WO 2014070033 A3 WO2014070033 A3 WO 2014070033A3 RO 2013000004 W RO2013000004 W RO 2013000004W WO 2014070033 A3 WO2014070033 A3 WO 2014070033A3
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- aircraft
- landing
- speed
- wheel
- wheels
- 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
-
- 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)
- Tires In General (AREA)
- Automobile Manufacture Line, Endless Track Vehicle, Trailer (AREA)
Abstract
Automated wheel turn speed adjustment system for aircraft landing aimed at reducing aircraft tire wear. This invention is in essence an automated wheel rotation speed control system that will intervene in the landing stage of a flight. It will eliminate tire wear by eliminating the high friction force that results when the aircraft's tires make contact with the runway. At this moment in time there is no such system implemented for any type of aircraft in service. As such, during landing, upon contact between the tires and the runway a violent friction process occurs and the wheel is rapidly spun up to a rotation speed equal to the liniar speed of the aircraft at landing all within fractions of a second ( a rise of tangential speed from 0 to almost 300 km/h). This process subjects the tire to a very high degree of wear that limits its operational cycle and at the same time exposes the aircraft to high risks such as tire explosion. Our proposed invention would seek to imprint a rotation speed equal to the landing speed of the aircraft to all of said aircraft's wheels. By doing this the tangential speed of any given wheel will be equal to the linear speed of the aircraft during landing, thus eliminating the high friction the wheels are exposed to during contact with the runway. This system can be implemented on any type of aircraft and is essentially made up of : a central controller (A-fig. 1) that commands an electric motor (C-fig. 2). The motor in turn will either directly or through a reductor mechanism turn a wheel or pair of wheels (A-fig. 2) on the landing gear (E-fig. 2). The controller will have a specific type of input parameters aircraft landing gear position, landing speed, altitude, etc) The type of controller and electric motor used will be determined by the aircraft's size and by the number of wheels on the landing gear assembly.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ROA201200386 | 2012-05-31 | ||
ROA201200386A RO127819A0 (en) | 2012-05-31 | 2012-05-31 | Automatic system for adjusting the rotary speed of aircraft wheels upon landing with a view to reducing tire wear |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2014070033A2 WO2014070033A2 (en) | 2014-05-08 |
WO2014070033A3 true WO2014070033A3 (en) | 2014-06-26 |
Family
ID=46880853
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/RO2013/000004 WO2014070033A2 (en) | 2012-05-31 | 2013-02-22 | Automated wheel turn speed adjustment system for aircraft landing aimed at reducing aircraft tire wear |
Country Status (2)
Country | Link |
---|---|
RO (1) | RO127819A0 (en) |
WO (1) | WO2014070033A2 (en) |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE29900944U1 (en) * | 1999-01-20 | 1999-04-08 | Merlaku, Kastriot, 84347 Pfarrkirchen | Airplane landing gear protection system |
US20050224642A1 (en) * | 2003-12-15 | 2005-10-13 | Sullivan Steven L | Landing gear method and apparatus for braking and maneuvering |
US20070284478A1 (en) * | 2006-06-08 | 2007-12-13 | Soderberg Rod F | Magnetically induced aircraft landing wheel rotation |
-
2012
- 2012-05-31 RO ROA201200386A patent/RO127819A0/en unknown
-
2013
- 2013-02-22 WO PCT/RO2013/000004 patent/WO2014070033A2/en active Application Filing
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE29900944U1 (en) * | 1999-01-20 | 1999-04-08 | Merlaku, Kastriot, 84347 Pfarrkirchen | Airplane landing gear protection system |
US20050224642A1 (en) * | 2003-12-15 | 2005-10-13 | Sullivan Steven L | Landing gear method and apparatus for braking and maneuvering |
US20070284478A1 (en) * | 2006-06-08 | 2007-12-13 | Soderberg Rod F | Magnetically induced aircraft landing wheel rotation |
Also Published As
Publication number | Publication date |
---|---|
RO127819A0 (en) | 2012-09-28 |
WO2014070033A2 (en) | 2014-05-08 |
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