US3977631A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Aircraft wheel drive apparatus and method
Assignee: Boeing Co
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Filing: 1975-06-04
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Granted: 1976-08-31
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Expires: 1995-06-04
Abstract
Abstract In order to drive the wheels of an aircraft with an auxiliary, ground handling drive, a wheel drive motor is selectively coupled to the aircraft wheel through a rotatably mounted aircraft brake assembly. The normally nonrotating stator portion of a conventional aircraft brake assembly is rotatably mounted about the wheel axle and is rotatably driven through a planetary gear system by the wheel drive motor. During ground handling, the brake assembly is actuated to cause a clutch-like engagement between the rotatably mounted brake stator elements and the conventional brake rotor elements, mounted on the aircraft wheel, to couple the motor to and for driving the wheel. Disengagement of the brake stator elements and wheel rotor elements decouples the motor drive and allows the aircraft wheel to freely rotate for the high rotational velocities occurring during take-off and landing. To utilize the brake assembly for its normal braking function, the rotatably mounted brake stator elements are locked against rotation by an auxiliary brake applied to a drive shaft coupling the motor to the planetary gear system.
Inventors
- 👤 Robert William Jenny
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-04 10:17
CPC Classifications
B; B64; B64C; B64C25/00; B64C25/32; B64C25/405; B64C25/42; B64C25/44; F; F16; F16D; F16D55/00; F16D55/24; F16D55/26; F16D55/36; F16D55/40; F16D2055/0004; F16D2055/0058; Y; Y02; Y02T; Y02T50/00; Y02T50/80
Claims Analysis
Total Claims: 10
Claim 1
Independent Claim
193 words
In an apparatus including an aircraft wheel axle, an aircraft wheel rotatably mounted on said axle, and a brake assembly having first and second braking element means and actuator means therefor, the combination therewith comprising: rotatably drivable brake carrier means rotatably mounted on said axle concentrically with said wheel, said first braking element means being mounted on said carrier means and said second braking element means being mounted on said wheel and said first and second braking element means being relatively movable by said actuator means between a condition of disengagement therebetween allowing relative rotation between said wheel and carrier means, and a condition of engagement therebetween restraining relative rotation between said wheel and carrier means; drive means coupled to said brake carrier means and having selective drive and nondrive conditions, said drive means being operable in its drive condition to rotate said carrier means; and controllable means coupled to said carrier means and having a restraint condition restraining relative rotation of said carrier means with respect to said axle and a nonrestraint condition in which said carrier means is free to be rotatably driven by said drive means in its drive condition.
Claim 2
Dependent Claim
193 words
In an apparatus including an aircraft wheel axle, an aircraft wheel rotatably mounted on said axle, and a brake assembly having first and second braking element means and actuator means therefor, the combination therewith comprising: rotatably drivable brake carrier means rotatably mounted on said axle concentrically with said wheel, said first braking element means being mounted on said carrier means and said second braking element means being mounted on said wheel and said first and second braking element means being relatively movable by said actuator means between a condition of disengagement therebetween allowing relative rotation between said wheel and carrier means, and a condition of engagement therebetween restraining relative rotation between said wheel and carrier means; drive means coupled to said brake carrier means and having selective drive and nondrive conditions, said drive means being operable in its drive condition to rotate said carrier means; and controllable means coupled to said carrier means and having a restraint condition restraining relative rotation of said carrier means with respect to said axle and a nonrestraint condition in which said carrier means is free to be rotatably driven by said drive means in its drive condition.
Claim 3
Dependent Claim
31 words
In the apparatus set forth in claim 1, said drive means including a motor means and reduction gear means, said reduction gear means coupling said motor means to said carrier means.
Claim 4
Dependent Claim
41 words
In the apparatus of claim 1, wherein said controllable means comprises: auxiliary brake means connected to said drive means for selectively restraining rotation of said carrier means by controlled braking of said drive means, thereby providing said restraint and nonrestraint conditions.
Claim 5
Dependent Claim
96 words
In the apparatus of claim 1, said actuator means including hydraulic means for effecting relative movement of said first and second braking element means between said conditions of engagement and disengagement, said actuator means being mounted on said brake carrier means for rotation therewith relative to said wheel axle, brake fluid conducting means mounted on said axle adjacent an interface with said rotatably mounted brake carrier means, and fluid coupling means for coupling said brake fluid across said interface between said fluid conducting means and said actuator means carried by said rotatably mounted brake carrier means.
Claim 6
Dependent Claim
179 words
In the apparatus of claim 1, said drive means including a planetary gear drive assembly having an input shaft adapted to be rotatably driven, first bevel gear means fixed to said shaft for rotation therewith, second bevel gear means mounted for rotation coaxially with respect to said wheel axle, planet gear carrier means attached to and for rotation with said second bevel gear means coaxially with said axle, planet gear cluster means rotatably mounted on said planet gear carrier means and including at least one gear cluster having first and second axially spaced planet gears, a sun gear means coaxially, nonrotatably mounted with respect to said axle coacting with said first planet gear of said cluster means, and a driven gear means carried by said brake carrier means coaxially with respect to said axle and coacting with said second planet gear, said first planet gear and coacting sun gear means having a different gear ratio with respect to said second planet gear and coacting driven gear, whereby rotation of said input shaft produces rotation of said brake carrier means.
Claim 7
Dependent Claim
96 words
An aircraft wheel drive apparatus comprising the combination of: a wheel axle; an aircraft wheel rotatably mounted on said axle; controllable brake means having rotor means and stator means selectively engagable with said rotor means, said rotor means mounted on said wheel for rotation therewith; means for rotatably mounting said stator means of said controllable brake means concentrically with respect to said aircraft wheel for selective engagement with said wheel mounted rotor means; and means for selectively alternatively rotatably driving and restraining rotation of said means for rotatably mounting said stator means of said brake means.
Claim 8
Dependent Claim
96 words
An aircraft wheel drive apparatus comprising the combination of: a wheel axle; an aircraft wheel rotatably mounted on said axle; controllable brake means having rotor means and stator means selectively engagable with said rotor means, said rotor means mounted on said wheel for rotation therewith; means for rotatably mounting said stator means of said controllable brake means concentrically with respect to said aircraft wheel for selective engagement with said wheel mounted rotor means; and means for selectively alternatively rotatably driving and restraining rotation of said means for rotatably mounting said stator means of said brake means.
Claim 9
Independent Claim
106 words
A method of rotatably driving an aircraft wheel mounted for rotation on an axle and coacting with a controllable brake also mounted on said axle, comprising the steps of: rotatably mounting said brake on said axle for concentric rotation with said wheel; selectively alternatively rotatably driving and restraining rotation of said rotatably mounted brake; and selectively operating said brake between actuated and unactuated conditions to allow unrestrained rotation of said wheel while in said unactuated condition and to effectively alternatively drive and brake said wheel while in said actuated condition in response to said alternative selective steps of driving and restraining said rotatably mounted brake, respectively.
Claim 10
Independent Claim
106 words
A method of rotatably driving an aircraft wheel mounted for rotation on an axle and coacting with a controllable brake also mounted on said axle, comprising the steps of: rotatably mounting said brake on said axle for concentric rotation with said wheel; selectively alternatively rotatably driving and restraining rotation of said rotatably mounted brake; and selectively operating said brake between actuated and unactuated conditions to allow unrestrained rotation of said wheel while in said unactuated condition and to effectively alternatively drive and brake said wheel while in said actuated condition in response to said alternative selective steps of driving and restraining said rotatably mounted brake, respectively.
References Cited (Backward Citations)
US3482654A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1979-08-31 | 1980-03-01 | 1980-08-31 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1983-08-31 | 1984-03-01 | 1984-08-31 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1987-08-31 | 1988-03-01 | 1988-08-31 | $7700.00 | Window Closed / Lapsed |