[특허]Heat exchanger suspension system with pipe-to-linkage spring rate ratio

Heat exchanger suspension system with pipe-to-linkage spring rate ratio 원문보기

IPC분류정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	F02C-007/32 F28D-007/06 F02K-003/115 F02C-006/08 F02C-007/141 F02C-007/18 F04D-029/58 F28F-009/00 F28F-009/02 F28D-021/00
출원번호	US-0074829 (2016-03-18)
등록번호	US-10151247 (2018-12-11)
발명자 / 주소	Duesler, Paul W. Schwarz, Frederick M.
출원인 / 주소	United Technologies Corporation
대리인 / 주소	Snell & Wilmer L.L.P.
인용정보	피인용 횟수 : 0 인용 특허 : 30

초록 ▼

A heat exchanger (HEX) arrangement for cooling air in a gas turbine engine is provided. The HEX arrangement may include a heat exchanger coupled to a plurality of ducts comprising a hot-side inlet duct and a hot-side outlet duct. The hot-side outlet duct may be in fluid communication with a compressor section of the gas turbine engine and in mechanical communication with a diffuser case. The HEX arrangement may further include a plurality of supporting links coupled between the heat exchanger and the gas turbine engine for securing the heat exchanger relative to the gas turbine engine. The supporting links may comprise a statically determined system. A spring rate ratio of between 1% and 30% may exist between the plurality of ducts and the plurality of supporting links.

대표청구항 ▼

1. A heat exchanger for cooling air in a gas turbine engine, comprising: a plurality of ducts comprising: a hot-side inlet duct;a hot-side outlet duct in fluid communication with a compressor section of the gas turbine engine and in mechanical communication with a diffuser case; anda plurality of supporting links coupled between the heat exchanger and an engine case for securing the heat exchanger relative to the gas turbine engine, wherein a spring rate ratio between the plurality of ducts and the plurality of supporting links is between 1% and 30%;wherein the hot-side outlet duct is directly coupled to the diffuser case;wherein the heat exchanger comprises a first connector, the plurality of supporting links comprising a first link coupled to the first connector, a second link coupled to the first connector, and a third link coupled to the first connector;wherein the first link extends in an axial direction, a first end of the first link coupled to the diffuser case and a second end of the first link coupled to the first connector, wherein the first end of the first link is prevented from moving in a radial direction and prevented from moving in the axial direction;wherein the second link extends in a circumferential direction, a first end of the second link coupled to the diffuser case and a second end of the second link coupled to the first connector, wherein the first end of the second link is prevented from moving in a radial direction and is prevented from moving in the circumferential direction, with respect to the diffuser case; andwherein the third link extends in the circumferential direction, a first end of the third link coupled to the diffuser case and a second end of the third link coupled to the first connector, wherein the first end of the third link is prevented from moving in the radial direction and is prevented from moving in the circumferential direction, with respect to the diffuser case. 2. The heat exchanger of claim 1, wherein the first connector is prevented from moving in the axial direction and in the radial direction, with respect to the diffuser case. 3. The heat exchanger of claim 1, wherein the first connector is prevented from moving in the radial direction and in the circumferential direction, with respect to the diffuser case. 4. The heat exchanger of claim 1, wherein the heat exchanger comprises a second connector, the second connector coupled to the gas turbine engine, the second connector prevented from moving in a circumferential direction with respect to the gas turbine engine. 5. The heat exchanger of claim 4, wherein the second connector is coupled to the gas turbine engine via a mounting bracket coupled directly to an engine case. 6. The heat exchanger of claim 1, wherein the heat exchanger comprises a third connector coupled to the gas turbine engine and a fourth connector coupled to the gas turbine engine, wherein the third connector is prevented from moving in a radial direction and the fourth connector is prevented from moving in the radial direction. 7. The heat exchanger of claim 6, wherein the third connector is coupled to the gas turbine engine via a fifth mounting bracket coupled directly to the diffuser case and the fourth connector is coupled to the gas turbine engine via a sixth mounting bracket coupled directly to the diffuser case. 8. The heat exchanger of claim 1, wherein the heat exchanger comprises a cold-side inlet and a cold-side outlet through which fan bypass air is conducted.

이 특허에 인용된 특허 (30)

Maier Karl (Karlsfeld DEX) Grss Helmut (Esterhofen DEX) Greune Christian (Frstenfeldbruck DEX), Assembly of a heat exchanger on a gas turbine engine.
상세보기
Merket, Lesley, Circulating water filtering system and method of operation.
상세보기
Maier, William C., Combined heat exchanger expander mounting system.
상세보기
Dierksmeier, Douglas David; Grant, Steven Lester; Muskat, James Christopher, Compressor tip clearance control and gas turbine engine.
상세보기
Gros Jean-Pierre (Villemomble FRX) Foucher Grard (Tremblay en France FRX), Condenser envelope made of concrete for a structurally independent low pressure module.
상세보기
Wohrl Bernhard (Gauting DEX), Connection apparatus between the outlet of a heat exchanger and the inlet of a combustion chamber of a gas turbine engin.
상세보기
Liu, Xiaoliu, Cooler in nacelle with radial coolant.
상세보기
Andersen Richard H. (Cincinnati OH) Corsmeier Robert J. (Cincinnati OH) Rauf James P. (Blue Ash OH) Lenahan Dean T. (Cincinnati OH), Cooling air cooler for a gas turbine engine.
상세보기
Porte Alain,FRX, Device for bleeding off and cooling hot air in an aircraft engine.
상세보기
Porte Alain,FRX, Device for bleeding off and cooling hot air in an aircraft engine.
상세보기
Beeck Alexander,CHX ; Guthier Klaus,DEX ; Konig Marcel,CHX ; Senior Peter,GB3, Fuel feed for gas turbines having an annular combustion chamber.
상세보기
Leroux, Samuel; Lallemant, Mathieu; Rimpau, Arnold; Westphal, Christian, Gas intake device.
상세보기
Coffinberry, George Albert, Gas turbine engine fan bleed heat exchanger system.
상세보기
Shiraichi, Yukishige; Ohtsuka, Masaki, Heat exchanger and heat exchanging system.
상세보기
Ikeda, Tooru, Heat exchanger for cooling high-temperature gas.
상세보기
Mangus Ervin E. (Brimfield IL) Kizer Richard W. (Morton IL) Young D. Craig (Peoria IL), Heat exchanger mounting for a turbine engine.
상세보기
Young ; D. Craig, Heat exchanger support system.
상세보기
Montestruc ; III Alfred N. ; Liebkemann ; IV G. Frederick, High pressure dense heat transfer area heat exchanger.
상세보기
Bourassa, Corey; Gerstler, William Dwight, Integrated inducer heat exchanger for gas turbines.
상세보기
Leonard Ronald J. (Harvard IL) Johnson Kenneth M. (Lindenhurst IL) Drehobl Thomas L. (Lindenhurst IL), Mass transfer device having a heat-exchanger.
상세보기
Martinez, Ramon; Breig, Benjamin Paul; Joerger, Keith Alan; Wilson, Gregg Hunt; Hunt, Matthew John; Corsmeier, Donald Michael; Johnson, Paul Charles, Method and system for radial tubular heat exchangers.
상세보기
Honnorat, Olivier, Modular power plant and an aircraft provided with a lift rotor.
상세보기
Miller Franklin E. (Cincinnati OH), Precooling heat exchange arrangement integral with mounting structure fairing of gas turbine engine.
상세보기
Schoenenborn,Harald, Recuperative exhaust-gas heat exchanger for a gas turbine engine.
상세보기
Darragh Charles T. (San Diego CA), Sealing system for a circular heat exchanger.
상세보기
Gibson, Jr., Gary E.; Watkinson, Craig; Hlavacek, Niles, Split bearing assemblies, air-cooled heat exchangers and related methods.
상세보기
Child, Malcolm S., Spring mounted recuperator.
상세보기
Darragh Charles T. (San Diego CA) Parsons ; Jr. Edward L. (El Cajon CA), Thermally balanced restraint system for a heat exchanger.
상세보기
Nash, James S., Thermally responsive recuperator housing.
상세보기
Olver, Bryan; Ciampa, Alessandro; Marrano, Roberto; Trepanier, Richard; Lamarre, Sylvain; Bernard, Martin; Germain, Patrick, Turbofan bypass duct air cooled fluid cooler installation.
상세보기

내보내기 메뉴

내보내기 구분

파일저장
인쇄
메일전송

구성항목

기본정보
상세정보

관리번호, 국가코드, 자료구분, 상태, 출원번호, 출원일자, 공개번호, 공개일자, 등록번호, 등록일자, 발명명칭(한글), 발명명칭(영문), 출원인(한글), 출원인(영문), 출원인코드, 대표IPC

저장형식

Text(ASCII format)
Excel format
PIAS분석(.xls)

메일정보

받는사람 (필수): @
보내는사람 (선택): @
제목
내용: KISTI 검색결과 이메일 서비스

안내

총 건의 자료가 검색되었습니다.

다운받으실 자료의 인덱스를 입력하세요. (1-10,000)

검색결과의 순서대로 최대 10,000건 까지 다운로드가 가능합니다.

데이타가 많을 경우 속도가 느려질 수 있습니다.(최대 2~3분 소요)

다운로드 파일은 UTF-8 형태로 저장됩니다.
파일의 내용이 제대로 보이지 않을실 때는 웹브라우저 상단의 보기 -> 인코딩 -> 자동선택 여부를 확인하십시오.

Text(ASCII format)
Excel format

AI-Helper ※ AI-Helper는 을 사용합니다.

AI-Helper

안녕하세요, AI-Helper입니다. 좌측 "선택된 텍스트"에서 텍스트를 선택하여 요약, 번역, 용어설명을 실행하세요.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.

IPC	Description
A	생활필수품
A62	인명구조; 소방(사다리 E06C)
A62B	인명구조용의 기구, 장치 또는 방법(특히 의료용에 사용되는 밸브 A61M 39/00; 특히 물에서 쓰이는 인명구조 장치 또는 방법 B63C 9/00; 잠수장비 B63C 11/00; 특히 항공기에 쓰는 것, 예. 낙하산, 투출좌석 B64D; 특히 광산에서 쓰이는 구조장치 E21F 11/00)
A62B-1/08	.. 윈치 또는 풀리에 제동기구가 있는 것

연합인증

Heat exchanger suspension system with pipe-to-linkage spring rate ratio 원문보기

초록 ▼

대표청구항 ▼

연구과제 타임라인

이 특허에 인용된 특허 (30)

관련 콘텐츠

특허 원문 보기

IPC 상위 출원인

AI-Helper ※ AI-Helper는 오픈소스 모델을 사용합니다.

선택된 텍스트

내보내기 구분	파일저장 인쇄 메일전송
구성항목	기본정보 상세정보 관리번호, 국가코드, 자료구분, 상태, 출원번호, 출원일자, 공개번호, 공개일자, 등록번호, 등록일자, 발명명칭(한글), 발명명칭(영문), 출원인(한글), 출원인(영문), 출원인코드, 대표IPC 관리번호, 국가코드, 자료구분, 상태, 출원번호, 출원일자, 공개번호, 공개일자, 공고번호, 공고일자, 등록번호, 등록일자, 발명명칭(한글), 발명명칭(영문), 출원인(한글), 출원인(영문), 출원인코드, 대표출원인, 출원인국적, 출원인주소, 발명자, 발명자E, 발명자코드, 발명자주소, 발명자 우편번호, 발명자국적, 대표IPC, IPC코드, 요약, 미국특허분류, 대리인주소, 대리인코드, 대리인(한글), 대리인(영문), 국제공개일자, 국제공개번호, 국제출원일자, 국제출원번호, 우선권, 우선권주장일, 우선권국가, 우선권출원번호, 원출원일자, 원출원번호, 지정국, Citing Patents, Cited Patents
저장형식	Text(ASCII format) Excel format PIAS분석(.xls)
메일정보	받는사람 (필수) @ 보내는사람 (선택) @ 제목 내용 KISTI 검색결과 이메일 서비스
안내	총 건의 자료가 검색되었습니다. 다운받으실 자료의 인덱스를 입력하세요. (1-10,000) 검색결과의 순서대로 최대 10,000건 까지 다운로드가 가능합니다. 데이타가 많을 경우 속도가 느려질 수 있습니다.(최대 2~3분 소요) 다운로드 파일은 UTF-8 형태로 저장됩니다. 파일의 내용이 제대로 보이지 않을실 때는 웹브라우저 상단의 보기 -> 인코딩 -> 자동선택 여부를 확인하십시오. ~ Text(ASCII format) Excel format

연합인증

Heat exchanger suspension system with pipe-to-linkage spring rate ratio 원문보기

초록 ▼

대표청구항 ▼

연구과제 타임라인

전체(0) 논문(0) 특허(0) 보고서(0)

전체(0) 논문(0) 특허(0) 보고서(0)

이 특허에 인용된 특허 (30)

관련 콘텐츠

특허 원문 보기

IPC 상위 출원인

AI-Helper ※ AI-Helper는 오픈소스 모델을 사용합니다.

선택된 텍스트