[특허]Fuel air heat exchanger

PRATT & WHITNEY CANADA CORP.

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Fuel air heat exchanger

특허상세정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	F02C-007/224 F02C-007/12 F28D-007/10 F01D-025/14 F28D-007/00 F28D-007/14
출원번호	US-0404789 (2012-02-24)
등록번호	US-9109842 (2015-08-18)
발명자 / 주소	Prociw, Lev Alexander Hawie, Eduardo
출원인 / 주소	PRATT & WHITNEY CANADA CORP.
대리인 / 주소	Norton Rose Fulbright Canada
인용정보	피인용 횟수 : 0 인용 특허 : 24

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A fuel air heat exchanger for a gas turbine engine having fuel and air conduits in heat exchange relationship with one another, and a distribution conduit in heat exchange relationship with a component to be cooled. The distribution conduit is in fluid communication with the outlet of each air conduit. The heat exchanger also includes a secondary air inlet in fluid communication with the distribution conduit and a flow selection member selectively movable between first and second configurations. In the first configuration, the flow selection member close...

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1. A fuel air heat exchanger for a gas turbine engine, the heat exchanger comprising: an annular duct configured to surround a component to be cooled, the annular duct having a first arcuate portion and a second arcuate portion defining a remainder of the annular duct;at least one fuel conduit and at least one air conduit extending in heat exchange relationship with one another, each fuel conduit having an inlet for communication with a fuel source and an outlet for communication with fuel distribution conduits of the engine, each air conduit having an inlet and an outlet each fuel conduit and each air conduit extending circumferentially within the first arcuate portion of the annular duct;a distribution conduit in heat exchange relationship with the component to be cooled, the distribution conduit being in fluid communication with the outlet of each air conduit, the distribution conduit being defined by the second arcuate portion of the annular duct, the second arcuate portion being free of the at least one fuel conduit;a secondary air inlet in fluid communication with the distribution conduit; anda flow selection member selectively movable between first and second configurations, the flow selection member in the first configuration closing the fluid communication between the secondary inlet and the distribution conduit, the flow selection member in the second configuration opening the fluid communication between the secondary air inlet and the distribution conduit. 2. The heat exchanger as defined in claim 1, wherein the flow selection member in the second configuration closes the fluid communication between the outlet of each air conduit and the distribution conduit. 3. The heat exchanger as defined in claim 2, wherein the flow selection member is a valve received in a conduit junction providing the fluid communication between the outlet of each air conduit and the distribution conduit and between the secondary air inlet and the distribution conduit. 4. The heat exchanger as defined in claim 1, wherein the flow selection member is a first flow selection member and is located in a conduit providing the fluid communication between the secondary air inlet and the distribution conduit, the heat exchanger further comprising a second flow selection member located in a conduit providing the fluid communication between the outlet of each air conduit and the distribution conduit and selectively movable between first and second configurations independently of the first flow selection member, the second flow selection member in the first configuration opening the fluid communication between the outlet of each air conduit and the distribution conduit, the second flow selection member in the second configuration closing the fluid communication between the outlet of each air conduit and the distribution conduit. 5. The heat exchanger as defined in claim 1, wherein the heat exchanger further comprises an annular wall element extending from the duct along an approximately axial direction and a perforated baffle extending from the duct along an approximately axial direction and connected to the wall element spaced apart from the duct, the wall element, baffle and an adjacent portion of at least one wall of the duct together forming a closed cross-section defining an annular cooling plenum, the distribution conduit being in fluid communication with the annular cooling plenum. 6. The heat exchanger as defined in claim 1, wherein the at least one air conduit includes a space within the annular duct defined around the at least one fuel conduit. 7. The heat exchanger as defined in claim 1, wherein each fuel conduit is defined by an annular gap between two concentric tubes, and the at least one air conduit includes a conduit defined inside a smallest one of the two concentric tubes. 8. A gas turbine engine comprising: a compressor section;an annular high pressure plenum in fluid flow communication with a discharge of the compressor section for receiving compressed air;a combustor contained in the high pressure plenum;a fuel-air heat exchanger including: at least one fuel conduit and at least one air conduit located in the high pressure plenum and extending in direct heat exchange relationship with one another, each fuel conduit having an inlet in fluid communication with a fuel source of the engine and an outlet in fluid communication with fuel distribution conduits of the combustor, each air conduit having an inlet in fluid communication with the high pressure plenum and an outlet,a distribution conduit located in the high pressure plenum for distribution of air to a component to be cooled, the distribution conduit being in fluid communication with the outlet of each air conduit,an annular duct surrounding the engine component to be cooled. each fuel conduit and each air conduit extending circumferentially within the annular duct. the annular duct haying a first arcuate portion containing the at least one fuel conduit and the at least one air conduit, and a second arcuate portion defining a remainder of the annular duct and being free of the at least one fuel conduit. the distribution conduit being defined by the second arcuate portion:a secondary air inlet located in the high pressure plenum and providing a bypass fluid communication between the high pressure plenum and the distribution conduit, the bypass fluid communication bypassing each air conduit, anda flow selection member selectively movable between first and second configurations, the flow selection member in the first configuration closing the secondary inlet and preventing the bypass fluid communication between the high pressure plenum and the distribution conduit, the flow selection member in the second configuration opening the secondary air inlet and allowing the bypass fluid communication between the high pressure plenum and the distribution conduit. 9. The engine as defined in claim 8, wherein the flow selection member is a valve received in a conduit junction providing the fluid communication between the outlet of each air conduit and the distribution conduit and a fluid communication between the secondary air inlet and the distribution conduit, the flow selection member in the second configuration closing the fluid communication between the outlet of each air conduit and the distribution conduit. 10. The engine as defined in claim 8, wherein the flow selection member is a first flow selection member, the heat exchanger further comprising a second flow selection member selectively movable between first and second configurations independently of the first flow selection member, the second flow selection member in the first configuration opening the fluid communication between the outlet of each air conduit and the distribution conduit, the second flow selection member in the second configuration closing the fluid communication between the outlet of each air conduit and the distribution conduit. 11. The engine as defined in claim 8, wherein the engine component to be cooled is a turbine support case of a turbine section of the engine which is surrounded by an annular cavity, the distribution conduit being in fluid communication with an annular plenum surrounding the annular cavity. 12. The engine as defined in claim 11, wherein the annular cavity surrounding the turbine support case is enclosed by an annular baffle, the plenum being partially defined by the annular baffle, the baffle including perforations providing fluid flow communication between the plenum and the annular cavity for impingement cooling on the turbine support case. 13. A method of regulating a cooling of an engine component of a gas turbine engine, the method comprising: circulating compressed air from a compressor discharge of the engine to a high pressure plenum containing a combustor of the engine;circulating fuel from a fuel source of the engine through at least one fuel conduit of a heat exchanger located in the high pressure plenum, the fuel circulating in the at least one fluid conduit around only part of a circumference of an annular duct surrounding the engine component; andmodulating a flow of the compressed air circulating from the high pressure plenum through at least one air conduit of the heat exchanger in direct heat exchange relationship with the at least one fuel conduit thereof in the part of the circumference of the annular duct, and into a distribution conduit defined by a remainder of the circumference of the annular duct and in heat exchange relationship with the engine component. 14. The method as defined in claim 13, wherein modulating the flow includes modulating a bypass flow of compressed air circulating directly from the high pressure plenum into the distribution conduit. 15. The method as defined in claim 13, wherein the engine component is a turbine shroud.

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Fuel air heat exchanger

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Fuel air heat exchanger

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