Apparatus for positioning an igniter within a liner port of a gas turbine engine
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F02C-007/264
출원번호
US-0090192
(2002-02-04)
발명자
/ 주소
White, Tracy Lowell
출원인 / 주소
General Electric Company
대리인 / 주소
Andes, William ScottDavidson, James P.
인용정보
피인용 횟수 :
9인용 특허 :
11
초록▼
An igniter tube for a gas turbine engine combustor has an inner surface, an outer surface, and a longitudinal axis therethrough. More specifically, the igniter tube includes: a first portion positioned within a port of a liner for the combustor, the first portion having an inner surface with an inne
An igniter tube for a gas turbine engine combustor has an inner surface, an outer surface, and a longitudinal axis therethrough. More specifically, the igniter tube includes: a first portion positioned within a port of a liner for the combustor, the first portion having an inner surface with an inner diameter and an outer surface with an outer diameter; a second portion located adjacent the first portion, the second portion having an inner surface with an inner diameter and an outer surface with an outer diameter, wherein the second portion outer diameter increases from the first portion outer diameter at a first end to a predetermined outer diameter at a second end; and, a third portion located adjacent the second portion, the third portion having an inner surface with an inner diameter and an outer surface with an outer diameter, wherein the third portion outer diameter is substantially the same as the predetermined outer diameter. Moreover, the second portion inner diameter of the igniter tube is substantially equal to the first portion inner diameter and the third portion inner diameter of the igniter tube is greater than the inner diameter of the second portion.
대표청구항▼
An igniter tube for a gas turbine engine combustor has an inner surface, an outer surface, and a longitudinal axis therethrough. More specifically, the igniter tube includes: a first portion positioned within a port of a liner for the combustor, the first portion having an inner surface with an inne
An igniter tube for a gas turbine engine combustor has an inner surface, an outer surface, and a longitudinal axis therethrough. More specifically, the igniter tube includes: a first portion positioned within a port of a liner for the combustor, the first portion having an inner surface with an inner diameter and an outer surface with an outer diameter; a second portion located adjacent the first portion, the second portion having an inner surface with an inner diameter and an outer surface with an outer diameter, wherein the second portion outer diameter increases from the first portion outer diameter at a first end to a predetermined outer diameter at a second end; and, a third portion located adjacent the second portion, the third portion having an inner surface with an inner diameter and an outer surface with an outer diameter, wherein the third portion outer diameter is substantially the same as the predetermined outer diameter. Moreover, the second portion inner diameter of the igniter tube is substantially equal to the first portion inner diameter and the third portion inner diameter of the igniter tube is greater than the inner diameter of the second portion. has a first end and a second end, the first ends of the legs are connected to one another, and the blades are received in the first recess with the second ends of the legs distal from the first recess. 13. The apparatus of claim 1, wherein the nails are made of metal. 14. The apparatus of claim 2, wherein the nails are made of metal. 15. The apparatus of claim 3, wherein the nails are made of metal. 16. The apparatus of claim 4, wherein the nails are made of metal. 17. The apparatus of claim 5, wherein the nails are made of metal. 18. The apparatus of claim 6, wherein the nails are made of metal. 19. The apparatus of claim 7, wherein the nails are made of metal. 20. The apparatus of claim 8, wherein the nails are made of metal.
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이 특허에 인용된 특허 (11)
Becker James T. (Jupiter FL) Auxier Thomas A. (Palm Beach Gardens FL), Cooled combustor dome heatshield.
Koshoffer John M. (Forest Park OH) Ekstedt Edward E. (Montgomery OH) Samuel Billy P. (Madeira OH) Stamm Edward I. (Madeira OH), Gas turbine engine carburetor.
Farmer, Gilbert; Kutter, Ella Christine; Vise, Steven Clayton; Staker, John Robert; Al-Roub, Marwan; Harris, Tariq Kay, Method and apparatus for cooling gas turbine engine igniter tubes.
Stenger Richard E. (Cincinnati OH) Monson Kenneth E. (Cincinnati OH) Frederick Robert A. (West Chester OH) Fessler Madeleine E. (Cincinnati OH) Tuley Eugene N. (Hamilton OH), Segmented centerbody for a double annular combustor.
Farmer Gilbert ; Groeschen James A. ; Rettig Mark G., Venturi for use in the swirl cup package of a gas turbine combustor having water injected therein.
Sullivan, Peter C.; Olejarski, Michael J., Combustion turbine engine combustor basket igniter port alignment verification tool and method for validating igniter alignment.
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