GAS TURBINE ENGINE WITH ACTIVE TIP CLEARANCE CONTROL

Fritz Prinz; Sangkyun Kang; Tibor Fabian; Georg Brasseur; Jordan Tresser; Frank Holman; Hideaki Tsuru; Minoru Matsunaga

GAS TURBINE ENGINE WITH ACTIVE TIP CLEARANCE CONTROL

Fritz Prinz (Erfinder), Sangkyun Kang (Erfinder), Tibor Fabian (Erfinder), Georg Brasseur (Erfinder), Jordan Tresser (Erfinder), Frank Holman (Erfinder), Hideaki Tsuru (Erfinder), Minoru Matsunaga (Erfinder)

Institut für Elektrische Messtechnik und Sensorik (4530)

Publikation: Schutzrecht › Patent

Abstract

In a gas turbine engine, a capacitive sensor is used for measuring a tip clearance of a radial compressor section (13) thereof, and an actuator (25) is used for axially displacing a rotor shaft (12, 20) in response to an output from the capacitive sensor. Because the capacitive change gives an accurate measure of the size of the tip clearance, where the tip clearance is small and tip clearance control is possible.

Originalsprache	englisch
Veröffentlichungsnummer	WO03095801
IPC	H02K 7/ 18 A I
Prioritätsdatum	14/06/02
Publikationsstatus	Veröffentlicht - 20 Nov. 2003

Dieses zitieren

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abstract = "In a gas turbine engine, a capacitive sensor is used for measuring a tip clearance of a radial compressor section (13) thereof, and an actuator (25) is used for axially displacing a rotor shaft (12, 20) in response to an output from the capacitive sensor. Because the capacitive change gives an accurate measure of the size of the tip clearance, where the tip clearance is small and tip clearance control is possible.",

author = "Fritz Prinz and Sangkyun Kang and Tibor Fabian and Georg Brasseur and Jordan Tresser and Frank Holman and Hideaki Tsuru and Minoru Matsunaga",

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TY - PAT

T1 - GAS TURBINE ENGINE WITH ACTIVE TIP CLEARANCE CONTROL

AU - Prinz, Fritz

AU - Kang, Sangkyun

AU - Fabian, Tibor

AU - Brasseur, Georg

AU - Tresser, Jordan

AU - Holman, Frank

AU - Tsuru, Hideaki

AU - Matsunaga, Minoru

PY - 2003/11/20

Y1 - 2003/11/20

N2 - In a gas turbine engine, a capacitive sensor is used for measuring a tip clearance of a radial compressor section (13) thereof, and an actuator (25) is used for axially displacing a rotor shaft (12, 20) in response to an output from the capacitive sensor. Because the capacitive change gives an accurate measure of the size of the tip clearance, where the tip clearance is small and tip clearance control is possible.

AB - In a gas turbine engine, a capacitive sensor is used for measuring a tip clearance of a radial compressor section (13) thereof, and an actuator (25) is used for axially displacing a rotor shaft (12, 20) in response to an output from the capacitive sensor. Because the capacitive change gives an accurate measure of the size of the tip clearance, where the tip clearance is small and tip clearance control is possible.

M3 - Patent

M1 - WO03095801

ER -