WO2009127885A3 - Flexible crankshaft for software controllable aircraft wheel drive - Google Patents
Flexible crankshaft for software controllable aircraft wheel drive Download PDFInfo
- Publication number
- WO2009127885A3 WO2009127885A3 PCT/HR2009/000014 HR2009000014W WO2009127885A3 WO 2009127885 A3 WO2009127885 A3 WO 2009127885A3 HR 2009000014 W HR2009000014 W HR 2009000014W WO 2009127885 A3 WO2009127885 A3 WO 2009127885A3
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- wheel
- flexible
- power
- aircraft wheel
- motor
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C1/00—Flexible shafts; Mechanical means for transmitting movement in a flexible sheathing
- F16C1/02—Flexible shafts; Mechanical means for transmitting movement in a flexible sheathing for conveying rotary movements
- F16C1/06—Flexible shafts; Mechanical means for transmitting movement in a flexible sheathing for conveying rotary movements with guiding sheathing, tube or box
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C3/00—Shafts; Axles; Cranks; Eccentrics
- F16C3/04—Crankshafts, eccentric-shafts; Cranks, eccentrics
- F16C3/06—Crankshafts
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2326/00—Articles relating to transporting
- F16C2326/43—Aeroplanes; Helicopters
-
- 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)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
- Health & Medical Sciences (AREA)
- Oral & Maxillofacial Surgery (AREA)
- Aviation & Aerospace Engineering (AREA)
- Handcart (AREA)
- Testing Of Balance (AREA)
- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
Abstract
The flexible crankshaft (4) for software controllable aircraft wheel drive represents a steel flexible cable (4), located in a flexible plastic-rubber guide which is adapted for the transfer of the torque along all axis, and is connected on one end to a power distributor (11), (or directly to a power generator unit if the construction is with one wheel) and with the other end, i.e. a small drive adapter (5), rests on the tyre of the aircraft wheel. The power distributor (11) receives entry power from the power generator motor (10) (electrical motor with gearshift switches, couplings, etc. Or from air pressure in "pneumatic" construction). The flexible crankshaft rotates moved by the power distributor or the motor (across the redactor, multiplicators, gearshift, valves, couplings, etc.) and transfers the torque through the adapter, to the tyre wheel itself, and in this way rotation of the wheel occurs. The rotation speed is regulated with the aid of a program CPU or own microcontroller, and always turns the wheel at the exact program calculated optimal rotation speed, adjusted for landing.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
HR20080181A HRP20080181A2 (en) | 2008-04-17 | 2008-04-17 | Aircraft wheel rotation assembly with separated power unit |
HRP20080181A | 2008-04-17 |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2009127885A2 WO2009127885A2 (en) | 2009-10-22 |
WO2009127885A3 true WO2009127885A3 (en) | 2010-01-21 |
Family
ID=41199512
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/HR2009/000014 WO2009127885A2 (en) | 2008-04-17 | 2009-04-16 | Flexible crankshaft for software controllable aircraft wheel drive |
Country Status (2)
Country | Link |
---|---|
HR (1) | HRP20080181A2 (en) |
WO (1) | WO2009127885A2 (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107016219B (en) * | 2017-05-09 | 2020-06-09 | 中国石油天然气股份有限公司 | Early warning method and system for carbonate reservoir drilling emptying |
CN107169192B (en) * | 2017-05-10 | 2020-06-09 | 中国石油天然气股份有限公司 | Method and device for identifying size of karst cave while drilling |
CN112394739B (en) * | 2020-10-29 | 2021-11-05 | 南京航空航天大学 | Active-deformation active-disturbance-rejection flight control method for four-rotor aircraft |
Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2287491A (en) * | 1940-09-19 | 1942-06-23 | Percy B Wolverton | Aircraft landing gear |
US2320547A (en) * | 1942-01-30 | 1943-06-01 | Roy L Tiger | Landing wheel rotating device for airplanes |
US2338699A (en) * | 1939-09-26 | 1944-01-11 | Joseph D Wilhoit | Airplane landing gear |
US2376621A (en) * | 1944-09-14 | 1945-05-22 | Milton L Reed | Safety landing gear and wheel for airplanes |
US2414849A (en) * | 1944-12-08 | 1947-01-28 | Robert H Beazley | Aircraft wheel spinner and control |
US2481600A (en) * | 1945-07-06 | 1949-09-13 | Samuel S Knox | Optical instrument for use in aircraft for visually synchronizing the landing wheelsand ground movement |
US2521864A (en) * | 1945-07-30 | 1950-09-12 | Morse Malcolm Wilcox | Aircraft landing wheel prerotation means |
US3428274A (en) * | 1966-09-19 | 1969-02-18 | Wally Ellis | Aircraft touchdown wheel synchronizer |
BE897959A (en) * | 1983-10-10 | 1984-01-30 | Borgers Jozef | Powered and braked landing wheels for jet aircraft - has main jet flow-driven turbine driving hydraulic pump to power landing wheel motor |
DE29900944U1 (en) * | 1999-01-20 | 1999-04-08 | Merlaku Kastriot | Airplane landing gear protection system |
-
2008
- 2008-04-17 HR HR20080181A patent/HRP20080181A2/en not_active Application Discontinuation
-
2009
- 2009-04-16 WO PCT/HR2009/000014 patent/WO2009127885A2/en active Application Filing
Patent Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2338699A (en) * | 1939-09-26 | 1944-01-11 | Joseph D Wilhoit | Airplane landing gear |
US2287491A (en) * | 1940-09-19 | 1942-06-23 | Percy B Wolverton | Aircraft landing gear |
US2320547A (en) * | 1942-01-30 | 1943-06-01 | Roy L Tiger | Landing wheel rotating device for airplanes |
US2376621A (en) * | 1944-09-14 | 1945-05-22 | Milton L Reed | Safety landing gear and wheel for airplanes |
US2414849A (en) * | 1944-12-08 | 1947-01-28 | Robert H Beazley | Aircraft wheel spinner and control |
US2481600A (en) * | 1945-07-06 | 1949-09-13 | Samuel S Knox | Optical instrument for use in aircraft for visually synchronizing the landing wheelsand ground movement |
US2521864A (en) * | 1945-07-30 | 1950-09-12 | Morse Malcolm Wilcox | Aircraft landing wheel prerotation means |
US3428274A (en) * | 1966-09-19 | 1969-02-18 | Wally Ellis | Aircraft touchdown wheel synchronizer |
BE897959A (en) * | 1983-10-10 | 1984-01-30 | Borgers Jozef | Powered and braked landing wheels for jet aircraft - has main jet flow-driven turbine driving hydraulic pump to power landing wheel motor |
DE29900944U1 (en) * | 1999-01-20 | 1999-04-08 | Merlaku Kastriot | Airplane landing gear protection system |
Also Published As
Publication number | Publication date |
---|---|
HRP20080181A2 (en) | 2010-01-31 |
WO2009127885A2 (en) | 2009-10-22 |
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