Aircraft selectively engageable electric taxi system

Patent metadata

Field	Value
Publication number	US-9290264-B2
Application number	US-201314099162-A
Country	US
Kind code	B2
Filing date	Dec 6, 2013
Priority date	May 13, 2013
Publication date	Mar 22, 2016
Grant date	Mar 22, 2016

Abstract

An electric taxi system (ETS) for an aircraft may include an annular output gearbox positioned between a wheel and a main strut of a main landing gear of the aircraft. The output gearbox may surround a brake piston assembly of the wheel of the aircraft. One or more selectively operable engaging assemblies, for selectively coupling the ETS with the wheel of the aircraft, may be positioned between the output gearbox and the wheel of the aircraft. The one or more selectively operable engaging assemblies may be coupled with an output gear of the output gearbox to rotate with the output gear.

First claim

We claim:

1. An apparatus for selectively engaging an electric taxi system (ETS) with a wheel of an aircraft, the apparatus comprising:
one or more engaging assemblies drivably coupled to an electric motor of the ETS, the one or more engaging assemblies having a hemispherically shaped leading end;
a wheel-drive device attached to a wheel of the aircraft, the wheel-drive device including a hemispherical socket positioned to be engageable with the leading end of an engaging member of one of the engaging assemblies when the engaging member is extended outwardly;
a first one of the one or more engaging assemblies has a first engaging member with a leading end oriented in a clockwise direction; and
a second one of the one or more engaging assemblies has a second engaging member with a leading end oriented in a counterclockwise direction.

2. The apparatus of claim 1 further comprising:
an engaging ring positioned coaxially with the wheel, the engaging ring being drivably coupled with the electric motor of the ETS;
wherein the one or more engaging assemblies are coupled to the engaging ring, the one or more engaging assemblies being positioned outwardly of a brake piston assembly of the wheel; and
wherein the engaging members of the one or more engaging assemblies are spring biased and selectively extend outwardly to engage with the wheel-drive device, thereby selectively transmitting rotational force from the electric motor to the wheel.

3. The apparatus of claim 1 wherein the wheel-drive device includes: a first socket oriented in a clockwise direction and positioned axially to be engageable with the first engaging member when the first engaging member is extended axially outwardly; and a second socket oriented in a counterclockwise direction and positioned axially to be engageable with the second engaging member when the second engaging member is extended axially outwardly.

4. The apparatus of claim 1 : wherein the one or more engaging assemblies include a base member; and wherein the engaging members are coupled to the base members with a ball and socket connector.

5. The apparatus of claim 1 further comprising: a stowing device coupled to the wheel, wherein the stowing device has one or more pivotable levers positioned to engage with a projection of a axially extended one of the one or more engaging assemblies and force the engaging assembly into a stowed position whenever the wheel rotates faster than the engaging ring.

6. The apparatus of claim 1 wherein: the one or more engaging assemblies are positioned radially inwardly of a rim of the wheel; and the one or more engaging assemblies selectively extend axially outwardly to engage with the wheel-drive device.

Assignees

• Honeywell Int Inc

Inventors

• Charles David Lane
• Christensen Donald Jeffrey

Classifications

• B64C25/405 Primary

  Powered wheels, e.g. for taxing · CPC title

• Y02T50/823

  Cross-Sectional Technologies · mapped topic

• Y02T50/80

  Energy efficient operational measures, e.g. ground operations or mission management · CPC title