About 313 results
Showing the first 200 results.
https://drivepatents.com/patents/965509 · 31 Dec 2014
This application describes a leaf seal arrangement, comprising: a first component having a high pressure area and a low pressure area therein; a second component which passes from the high pressure area to the low pressure area; a leaf seal having an array...
https://drivepatents.com/patents/966079 · 17 Dec 2014
Combustion equipment for use in a gas turbine engine. The combustion equipment has an inner case and an outer case, wherein the outer case encloses the inner case so that a cavity is located between the inner and outer cases. The combustion equipment also ...
https://drivepatents.com/patents/967250 · 19 Nov 2014
A system for monitoring the performance of a fluid heat exchanger for use with an engine comprises a heat exchanger (120) having a first fluid flow path (130) therethrough and a second fluid flow path (140) therethrough. The system further comprises a firs...
https://drivepatents.com/patents/967188 · 19 Nov 2014
A heat exchange arrangement (40) for a gas turbine engine (10). The arrangement (40) comprises a first conduit (46) for an engine component cooling fluid and a second conduit (44) for a second fluid. The arrangement further comprises a heat exchange portio...
https://drivepatents.com/patents/967456 · 12 Nov 2014
The present invention provides a rigid raft. The raft has an electrical system comprising electrical conductors embedded in the raft. The raft further has one or more sensors embedded therein for monitoring parameters, for example the temperature and/or st...
https://drivepatents.com/patents/967460 · 12 Nov 2014
A vehicle is provided that has a rigid dressing raft 200. The rigid dressing raft 200 provides a part of a fluid and/or electrical system to the vehicle. The rigid dressing raft comprises elongate fibres 232, which may provide strength to the raft. The fib...
https://drivepatents.com/patents/967414 · 12 Nov 2014
An aircraft electrical network (50). The network (50) comprises a first starter generator (52) mechanically coupled to a first shaft (40) of an aircraft main engine (22). The first starter generator (52) is configured to turn the first shaft (40) of the ma...
https://drivepatents.com/patents/967606 · 5 Nov 2014
A composite structure is provided. The structure is formed of rigid composite material in which non-metallic continuous fibres reinforce a polymer matrix. The continuous fibres are electrically conductive. The structure has electrodes electrically connecte...
https://drivepatents.com/patents/967600 · 5 Nov 2014
A composite structure is provided. The structure is formed of rigid composite material in which particulates or fibres reinforce a polymer matrix. The structure has first and second electrically conductive metallic meshes embedded therein, and respective e...
https://drivepatents.com/patents/967596 · 5 Nov 2014
An electrical unit comprises an electrical connector having a set of elongate electrical terminals which are each a one-piece component. The terminals extend into the unit such that first ends of the terminals are connected to multiple electrical conductor...