About 318 results
Showing the first 200 results.
https://drivepatents.com/patents/992604 · 27 Feb 2013
An asset operational health monitoring system, in which a plurality of sensors are arranged to determine values of asset operation parameters pertaining to an instance of asset operation. One or more processing unit receives data corresponding to said asse...
https://drivepatents.com/patents/992589 · 27 Feb 2013
A turbine engine comprising an engine core bounded by a bypass duct, a first portion of the bypass duct defined by a fan casing having a radially inner wall and a radially outer wall, a second portion of the bypass duct defined by a radially inner wall and...
https://drivepatents.com/patents/993350 · 30 Jan 2013
The invention relates to a gas discharge tube (30) of a type that may be used for example in gas turbine engine (10) ignition systems. The gas discharge tube (30) has an envelope (42) containing a gas therein and the envelope has a pair of spaced electrode...
https://drivepatents.com/patents/993332 · 30 Jan 2013
A ducted fan gas turbine assembly has a thrust reverser assembly having a vane arrangement including a first set of turning vanes (37) for channelling airflow from the duct in a rearward direction and a second set of turning vanes (38) for channelling airf...
https://drivepatents.com/patents/993502 · 23 Jan 2013
A method of inhibiting ice accretion within a turbine engine 4, 6, comprising the steps: (a) operating the turbine engine 4, 6 at a predetermined engine speed; and (b) driving the compressor 8, 10 of the turbine engine 4, 6 at an elevated speed which is gr...
https://drivepatents.com/patents/993773 · 16 Jan 2013
A gas turbine engine exhaust nozzle comprises a nozzle body (8) defining a nozzle exit (6). An array of movable slats (16, 18) is disposed round the nozzle exit (6). Flow control walls (20) are fixed to the nozzle body (8) and provide flow control surfaces...
https://drivepatents.com/patents/994394 · 2 Jan 2013
A heat exchanger is provided for warming fuel prior to introduction of the fuel to an engine, the heat exchanger including: a fuel inlet and a fuel outlet; a heat exchange matrix having heat transfer components past which the fuel flows between said inlet ...
https://drivepatents.com/patents/994280 · 2 Jan 2013
An electrical generating system for aircraft with one or more engines (1,1a) includes a plurality of generators (13,23;33,43) associated with the engines so as to produce respective AC outputs. The frequencies of these outputs can differ from each other, a...
https://drivepatents.com/patents/994667 · 26 Dec 2012
A heat and/or fire protection assembly (100) for a component (104), the assembly comprising: a plurality of protrusions (110) distributed about a surface of the component, the protrusions protruding with respect to the surface of the component; the protrus...
https://drivepatents.com/patents/994646 · 26 Dec 2012
A mounting assembly for attaching a ducted fan gas turbine engine to an aircraft is provided. The engine has an intake (111), a propulsive fan, a fan case (125) surrounding the fan, and a core engine (126). The air intake (111) is attached to the front of ...