About 32 results
https://drivepatents.com/patents/946546 · 20 Jan 2016
A method of determining the integrity of an electric or hydraulic braking control system. A reduction rate of a voltage or hydraulic pressure in the braking control system is determined, and the integrity of the braking control system is determined by comp...
https://drivepatents.com/patents/946544 · 20 Jan 2016
A method of determining the integrity of an electric or hydraulic energy source of a braking control system. The energy source is charged or discharged, and two or more measurements of voltage or hydraulic pressure are taken from the braking control system...
https://drivepatents.com/patents/947024 · 13 Jan 2016
An assembly providing an abutment for a door is disclosed. The assembly is arranged to hold the abutment (58) remotely from a side of an opening which is closed by the door (53). The abutment (58) may be moveable between deployed and retracted configuratio...
https://drivepatents.com/patents/960247 · 3 Jun 2015
An electrically actuated braking system for an aircraft, comprising: an electro-mechanical brake actuator (EMAbrake) proximate a wheel of the aircraft, the EMAbrake including a motor; an electro-mechanical actuator controller (EMAC) including a motor contr...
https://drivepatents.com/patents/960244 · 3 Jun 2015
An electrically actuated braking system for an aircraft. The system includes: an electro-mechanical brake actuator (EMAbrake) proximate a wheel of the aircraft, the EMAbrake including a motor; an electro-mechanical actuator controller (EMAC) including a mo...
https://drivepatents.com/patents/960238 · 3 Jun 2015
An electrically actuated braking system for an aircraft, comprising: an electro-mechanical brake actuator (EMAbrake) proximate a wheel of the aircraft, the EMAbrake including a motor; an electro-mechanical actuator controller (EMAC) including a first motor...
https://drivepatents.com/patents/971877 · 30 Jul 2014
The present invention concerns a device for use in an aircraft fuel pressure sensor line (28, 30). More particularly, but not exclusively, this invention concerns a fuel pressure sensor line (28, 30) connecting an aircraft fuel pump (22) to a pressure sens...
https://drivepatents.com/patents/974901 · 14 May 2014
The present application relates to a mount (10) for mounting a cable harness to a support. The mount (10) comprises a harness receiving portion (42), and a fastener attachment portion (80) from which a fastener for securing the mount (10) to a support is e...
https://drivepatents.com/patents/987430 · 14 Aug 2013
A battery case for a power tool, comprising a body defining a cavity configured to receive a battery, a body surface of the battery case being formed to have a curved outward profile.
https://drivepatents.com/patents/985380 · 27 Mar 2013
A bleed air duct joint insulation means (204) is disclosed in which a leak vent (205) comprises valve means (303).