초록 ▼

An electric taxi system (ETS) for an aircraft may comprise drive motors mounted coaxially with wheels of the aircraft. A clutch assembly may be interposed between the drive motor the wheel. The clutch assembly may transmit torque from the motor to the wheel when the wheel and a rotor of the motor ro

An electric taxi system (ETS) for an aircraft may comprise drive motors mounted coaxially with wheels of the aircraft. A clutch assembly may be interposed between the drive motor the wheel. The clutch assembly may transmit torque from the motor to the wheel when the wheel and a rotor of the motor rotate at the same rotational speed. The clutch assembly may self-disengage a rotor of the motor from the wheel when the wheel rotates faster than the rotor.

대표청구항 ▼

1. A clutch assembly comprising: a driving member;a driven member; anda transfer member axially movable between a retracted position and an extended position;the transfer member being coupled to the driving member with one or more links when the transfer member is in its retracted position so that t

1. A clutch assembly comprising: a driving member;a driven member; anda transfer member axially movable between a retracted position and an extended position;the transfer member being coupled to the driving member with one or more links when the transfer member is in its retracted position so that the transfer member is driven to rotate with the driving member as a result of force transmitted through the one or more links;the transfer member configured to engage with a driving lug of the driving member when the transfer member is in its extended position so that the transfer member is driven to rotate with the driving member as a result of force transmitted through the driving lug;the transfer member being configured to engage with a driven lug of the driven member to rotate the driven member when the transfer member is in its extended position;the transfer member being disengaged from the driven member when the transfer member is in its retracted position;wherein the one or more links are attached to the driving member at one or more first pivot points;wherein the one or more links are attached to the transfer member at one or more second pivot points; andwherein a circumferential displacement of the one or more first pivot points relative to the one or more second pivot points results in change of axial distance between the first and second pivot points and a corresponding axial displacement of the transfer member relative to the driving member. 2. The clutch assembly of claim 1 wherein at least three of the links are disposed uniformly around the driving member so that a plane of the driving member and a plane of the transfer member are parallel to one another. 3. The clutch assembly of claim 1 wherein the driving member is a ring gear. 4. The clutch assembly of claim 1: wherein the transfer member comprises at least one outer lug; wherein the driven member is provided with a driven lug; and wherein the outer lug is in contact with the driven lug when the transfer member is in its extended position. 5. The clutch assembly of claim 1: wherein the outer lug of the transfer member has a clockwise side and a counterclockwise side;wherein the driven lug of the driven member has a clockwise side and a counterclockwise side;wherein the counterclockwise side of the outer lug is configured to engage with the clockwise side of the driven lug of the driven member when the wheel of the aircraft rotates at the same rotational speed as the transfer member in a counterclockwise direction;wherein the clockwise side of the outer lug is configured to engage with the counterclockwise side of the driven lug of the driven member when the wheel of the aircraft rotates at the same rotational speed as the transfer member in a clockwise direction;wherein the counterclockwise side of the driven lug is configured to engage with the clockwise side of the outer lug when the wheel of the aircraft rotates at a faster rotational speed than the transfer member in a counterclockwise direction so that the transfer member is circumferentially displaced relative to the driving member and so that the transfer member moves to its retracted position thereby disengaging the rotor from the wheel; andwherein the clockwise side of the driven lug is configured to engage with the counterclockwise side of the outer lug when the wheel of the aircraft rotates at a faster rotational speed than the transfer member in a clockwise direction so that the transfer member is circumferentially displaced relative to the driving member and so that the transfer member moves to its retracted position thereby disengaging the rotor from the wheel. 6. The clutch assembly of claim 1 wherein the one or more links are attached to the driving member with a spherical bearing. 7. The clutch assembly of claim 1 further comprising: a brake pad configured to be selectively engageable with the transfer member; andwherein the transfer member is configured to be displaced circumferentially relative to the driving member upon engagement of the brake pad so that the first and second pivot points are axially displaced relative to each other and the transfer member is correspondingly axially displaced relative to the driving member. 8. The clutch assembly of claim 7 wherein the transfer member is configured to move to its extended position when the brake pad is engaged with the transfer member. 9. The clutch assembly of claim 1 further comprising a selectively engageable lock configured to engage with a locking groove on the transfer member and to hold the transfer member in its retracted position. 10. The clutch assembly of claim 1 further comprising at least one spring interposed between the transfer member and the driving member and configured to apply spring force to the transfer member to hold the transfer member in its retracted position.