About 14 results
https://drivepatents.com/patents/1398301 · 8 Apr 2026
An aircraft sensor system (100) includes a first sensor (90; 110; 430) configured to detect a parameter of an aircraft system and a first micro electromechanical-system (MEMS) (120, 122, 124, 126, 128; 410) disposed local to a first component within the ai...
https://drivepatents.com/patents/1392140 · 3 Sep 2025
The present disclosure provides for electrical connectivity to high temperature film sensor devices (e.g., temperature sensor devices). More particularly, the present disclosure provides for high temperature, thin film sensor devices (e.g., temperature sen...
https://drivepatents.com/patents/970828 · 27 Aug 2014
The aircraft gas turbine (1) has a first rotating shaft (16), through which torque is interchanged between the two units, and a coaxial-arranged second shaft (17), which is rotationally connected to an area near to a shaft end of the first shaft. A second ...
https://drivepatents.com/patents/990945 · 8 May 2013
An aircraft jet engine system includes at least one gas turbine engine (10) having a fan (14) including a rotor and a plurality of fan blades (100). A sensor system (102, 104) in the fan section (14) senses information about the operation of the blades (10...
https://drivepatents.com/patents/996060 · 14 Nov 2012
A controller, for use in a power plant having a liquid cooling system and an air cooling system, comprising one or more inputs, configured to receive a signal from at least one deposit sensor, wherein the signal from the deposit sensor is indicative of dep...
https://drivepatents.com/patents/997520 · 10 Oct 2012
A system for stabilizing combustion in a gas turbine engine comprises a) optical sensing means embedded within a fuel injector for observing conditions within a combustion chamber of a gas turbine engine; b) means for detecting combustion instabilities bas...
https://drivepatents.com/patents/1011697 · 22 Jun 2011
A transducer assembly (100) for connecting a transducer (102) to a device, the transducer assembly comprising: a transducer mount (110) adapted to receive the transducer; and a clamp (120) comprising first and second jaws (122, 124), the first and second j...
https://drivepatents.com/patents/1014082 · 6 Apr 2011
A gas turbine engine (10) and an apparatus for operating the gas turbine engine (10) comprises at least one microphone (62) to detect the sound of impacts of particles on a surface of the gas turbine engine (10) or a surface of an associated aircraft, a re...
https://drivepatents.com/patents/1014092 · 6 Apr 2011
The method involves providing a definite hot gas mass flow with a definite time-dependent pressure pulses. A turbine of an exhaust turbo charger is operated using a pressure pulse hot gas mass flow in an internal combustion motor relevant operating region....
https://drivepatents.com/patents/1072669 · 9 Nov 2005
A fuel injector for a gas turbine combustor is disclosed which includes a feed arm (22) having a flange (24) for mounting the injector within the combustor and a fuel nozzle (26) depending from the feed arm for injecting fuel into the combustor for combust...