[특허]Plate for directing flow and film cooling of components

Plate for directing flow and film cooling of components 원문보기

IPC분류정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	F01D-005/18 F01D-025/24 F01D-025/16
출원번호	US-0730898 (2012-12-29)
등록번호	US-9850780 (2017-12-26)
발명자 / 주소	Chuong, Conway Budnick, Matthew
출원인 / 주소	United Technologies Corporation
대리인 / 주소	Kinney & Lange, P.A.
인용정보	피인용 횟수 : 0 인용 특허 : 71

초록

An assembly includes a gas turbine engine component and a plate. The plate is spaced from a surface of the component and generally conforms to the shape of the surface. The plate and component form a passageway that allows for passage of a secondary gas flow between the component and the plate.

대표청구항 ▼

1. An assembly comprising: a gas turbine engine component; anda plate spaced from a surface of the component and generally conforming to the shape of the surface, wherein the plate and the component form a passageway that allows for passage of a secondary gas flow between the component and the plate, and wherein the plate has a plurality of standoffs that contact the surface of the component to space the plate from the surface. 2. The assembly of claim 1, further comprising a mount affixed to the component and wherein a portion of the plate is affixed to the mount. 3. The assembly of claim 1, wherein the component comprises a turbine frame. 4. The assembly of claim 3, wherein the plate is mounted to an outer radial casing of the turbine frame. 5. The assembly of claim 1, wherein the component comprises a fairing that defines a main gas flow path of the gas turbine engine. 6. The assembly of claim 5, wherein the fairing includes a rib with one or more apertures therein that allow for the secondary air flow to enter the passageway between the plate and the fairing. 7. The assembly of claim 1, wherein the plate is fixed with respect to the component at a first end and is free with respect to the component at a second end. 8. An assembly for a gas turbine engine, comprising: an outer radial casing; anda plate attached to the outer radial casing and extending along and generally conforming with a surface of the casing to form a passageway that allows for a secondary gas flow between the casing and the plate, and wherein the plate has a plurality of standoffs that contact the surface of the casing to space the plate from the surface. 9. The assembly of claim 8, wherein the outer radial casing comprises a portion of a turbine frame. 10. The assembly of claim 8, wherein the plate is fixed with respect to the outer radial casing at a first end and is free with respect to the outer radial casing at a second end. 11. An assembly for a gas turbine engine, comprising: a first casing;a fairing disposed within the casing to form a main gas flow path for the gas turbine engine, wherein the fairing has a rib that extends therefrom; anda plate mounted to the rib and extending along a surface of a component to form a passageway therealong, wherein the passageway allows for a secondary gas flow between the component and the plate, and wherein the rib has one or more apertures therein that allow the secondary air to flow into the passageway between the plate and the fairing. 12. The assembly of claim 11, wherein the rib extends away from the main gas flow path of the gas turbine engine. 13. The assembly of claim 11, wherein the plate has a plurality of projections that contact the surface of the component to standoff the plate from the surface. 14. The assembly of claim 11, wherein the plate is fixed with respect to the rib at a first end and is free with respect to the rib at a second end.

이 특허에 인용된 특허 (71)

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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

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연합인증

Plate for directing flow and film cooling of components 원문보기

초록

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Plate for directing flow and film cooling of components 원문보기

초록

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연구과제 타임라인

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