A lubricant supply system for a gas turbine engine has a lubricant lube pump delivering lubricant to an outlet line. The outlet line is split into at least a hot line and into a cool line, with the hot line directed primarily to locations associated with an engine that are not intended to receive cooler lubricant, and the cool line directed through one or more heat exchangers at which lubricant is cooled. The cool line then is routed to a fan drive gear for an associated gas turbine engine. A method and apparatus are disclosed.
Federico Papa - Ellington CT, US Thomas G. Phillips - Coventry CT, US Kathleen R. Phillips - Coventry CT, US
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
F02C 7/06 F02C 1/00 F02K 99/00
US Classification:
60 3908, 60266, 60267, 60772
Abstract:
A thermal management system for a gas turbine engine includes a first heat exchanger that provides a first conditioned fluid, a second heat exchanger in series flow communication with the first heat exchanger and that exchanges heat with the first conditioned fluid to provide a second conditioned fluid, and a third heat exchanger in parallel flow communication with the second heat exchanger and that selectively exchanges heat with the first conditioned fluid to provide a third conditioned fluid. The second conditioned fluid and the third conditioned fluid combine to provide a mixed conditioned fluid. A first portion of the mixed conditioned fluid including a first temperature is communicated to a first engine system. A second portion of the mixed conditioned fluid including a second temperature is communicated to a second engine system. The second temperature includes a greater temperature than the first temperature.
Xiaojun Campbell - East Hampton CT, US Thomas G. Phillips - Coventry CT, US Kathleen R. Phillips - Coventry CT, US
International Classification:
F02C 6/08
US Classification:
60785
Abstract:
A gas turbine engine has a fan, a compressor section, a combustor, and a turbine section. The fan delivers a portion of air into the compressor, and into a duct, as bypass air. A bleed air system bleeds a quantity of air from the compressor into a chamber at least at low power conditions of the engine. The bleed air system has an opening which may be selectively closed to block bleed air, or opened to allow bleed flow from the compressor into the chamber. A heat exchanger is positioned such that a first surface of the heat exchanger is contacted by bypass air in the duct, and a second surface of the heat exchanger is contacted by bleed air when the bleed air system directs air from the compressor into the chamber.
United Technologies Corporation - Hartford CT, US Thomas G. Phillips - Coventry CT, US Kathleen R. Phillips - Coventry CT, US Ethan K. Stearns - Lebanan CT, US Justin W. Heiss - East Hartford CT, US
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
F01D 25/12
US Classification:
415 1, 415177
Abstract:
A thermal management system for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a heat exchanger and a valve that controls an amount of a first fluid that is communicated through the heat exchanger A first sensor senses a first characteristic of a second fluid that is communicated through the heat exchanger to exchange heat with the first fluid and a second sensor senses a second characteristic of the second fluid. A positioning of the valve is based on at least one of the first characteristic and the second characteristic.
Thomas G. Phillips - Coventry CT, US Kathleen R. Phillips - Coventry CT, US
International Classification:
F02C 7/14
US Classification:
165 51
Abstract:
A thermal management system according to an exemplary aspect of the present disclosure includes, among other things, a first fluid circuit that selectively communicates a first portion of a first conditioned fluid having a first temperature to a first gas turbine engine system and a second portion of the first conditioned fluid having a second temperature to a second gas turbine engine system. The second temperature is a greater temperature than the first temperature. A second fluid circuit circulates a second conditioned fluid that is different from the first conditioned fluid to a third gas turbine engine system.
Kathleen R. Phillips - Coventry CT, US Thomas G. Phillips - Coventry CT, US Ethan K. Stearns - Mansfield CT, US Federico Papa - Ellington CT, US
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
F01D 25/18
US Classification:
415112, 415175, 415177, 184 612, 1841041
Abstract:
An exemplary geared turbomachine fluid delivery system includes a first fluid path configured to communicate fluid from a supply to a gear system of a geared turbomachine, and a second fluid path configured to communicate fluid from the supply to the gear system. The fluid introduced to the gear system by the first fluid path is cooler than that the fluid introduced to the gear system by the second fluid path.
- Farmington CT, US Thomas G. PHILLIPS - Coventry CT, US Kathleen R. PHILLIPS - Coventry CT, US Ethan K. STEARNS - Lebanon CT, US Justin W. HEISS - East Hartford CT, US
International Classification:
F02C 7/14 F02C 7/224
Abstract:
A thermal management system for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a heat exchanger and a valve that controls an amount of a first fluid that is communicated through the heat exchanger. A first sensor senses a first characteristic of a second fluid that is communicated through the heat exchanger to exchange heat with the first fluid and a second sensor senses a second characteristic of the second fluid. A positioning of the valve is based on at least one of the first characteristic and the second characteristic.
- Hartford CT, US Thomas G. Phillips - Coventry CT, US Kathleen R. Phillips - Coventry CT, US Ethan K. Stearns - Lebanan CT, US Justin W. Heiss - East Hartford CT, US
A gas turbine engine according to an exemplary embodiment of this disclosure, among other possible things includes a fan. A geared architecture is configured for driving the fan. A turbine section is configured for driving the geared architecture. A thermal management system that includes a first fluid circuit and a second fluid circuit that manage heat generated in at least a portion of the gas turbine engine. A first heat exchanger is incorporated into each of the first fluid circuit and the second fluid circuit. A second heat exchanger is incorporated into the first fluid circuit. A valve controls an amount of a first fluid that is communicated to the first heat exchanger and the second heat exchanger. A controller is configured to control a positioning of the valve. The amount of the first fluid communicated to the first heat exchanger is based on a first characteristic of a second fluid and the amount of the first fluid communicated to the second heat exchanger is based on a second characteristic of the second fluid. A method and a system are also disclosed.
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Kathleen Phillips
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Kathleen Phillips
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I was born and raised in Germany. Jon and I met in high school. We both attended the University of Oregon (GO DUCKS). I received my Master's degree in 06 and began my teaching career in Kansas. I ...
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