Combustion chamber, in particular of a gas turbine
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F02C-007/20
F23R-003/50
F23R-003/00
출원번호
US-0694192
(2003-10-27)
발명자
/ 주소
Tiemann,Peter
출원인 / 주소
Siemens Aktiengesellschaft
인용정보
피인용 횟수 :
12인용 특허 :
11
초록▼
The invention relates to a combustion chamber, in particular of a gas turbine, comprising an external wall structure that surrounds an internal area and an internal wall, which is formed by the surface of a housing that is located in the internal area. Said combustion chamber can be cooled essential
The invention relates to a combustion chamber, in particular of a gas turbine, comprising an external wall structure that surrounds an internal area and an internal wall, which is formed by the surface of a housing that is located in the internal area. Said combustion chamber can be cooled essentially by convection by an air stream that flows between the external wall structure and the internal wall, whereby the air stream is conducted in a closed cooling air canal. The housing can be mounted in the internal area of the combustion chamber by means of a suspension device, which comprises a large number of fixing elements that are arranged on the periphery of the housing and are braced against the wall structure.
대표청구항▼
The invention claimed is: 1. A combustion chamber comprising: an outer wall structure surrounding an internal area; a cooling air inlet orifice arranged on the outer wall structure for cooling air near a hot gas outlet orifice, the cooling air inlet orifice opening into a cooling air channel; a bur
The invention claimed is: 1. A combustion chamber comprising: an outer wall structure surrounding an internal area; a cooling air inlet orifice arranged on the outer wall structure for cooling air near a hot gas outlet orifice, the cooling air inlet orifice opening into a cooling air channel; a burner projecting into the internal area; a housing extending from the burner to the hot gas outlet orifice; a stiffening rib arranged on a surface of the housing and oriented in an axial direction in the direction of hot gas flow, the stiffening rib sized and configured to reduce stress in the housing; an inner wall offset from the outer wall structure, the inner wall formed by a surface of the housing and cooled by convection by an air stream flowing between the outer wall structure and the inner wall, the air stream being conducted in a closed cooling air channel; and an outlet opening for the cooling air from the cooling air channel via which the cooling air is conducted to the burner for combustion purposes, whereby between the cooling air inlet orifice and the outlet opening the majority of the surface of the housing is cooled by convection by the cooling air stream; an interlocking joint comprising a flange of the housing proximate the hot outlet orifice extending into a slot formed in the outer wall structure, the interlocking joint providing positional support for the housing within the outer wall structure while allowing both axial and radial thermal growth there between; and a suspension device comprising a plurality of fixing elements each urging the housing radially toward the outer wall structure under a spring tension to provide a rest position for the housing within the outer wall structure, each fixing element comprising a bolt passing through a respective conical shaped guide hole compromising a narrowing diameter formed through the outer wall structure effective to create a rubbing by the respective bolt against the respective narrowing during operation of the combustion chamber thereby suppressing unwanted vibration of the housing. 2. The combustion chamber as claimed in claim 1, wherein the housing is made of sheet metal having a wall thickness between 3 mm and 10 mm. 3. The combustion chamber as claimed in claim 2, wherein the wall structure has at least one cooling air inlet orifice in the area of the hot gas outlet orifice. 4. The combustion chamber as claimed in claim 1, wherein the housing has stiffening ribs on its outer surface. 5. The combustion chamber as claimed in claim 1, wherein in the area of the burner the housing has a device for insertion of the burner. 6. The combustion chamber as claimed in claim 1, wherein the fixing elements are spring mounted at the end adjoining the wall structure. 7. The combustion chamber as claimed in claim 1, wherein the suspension device is designed such that the suspended housing can move both axially and radially with respect to an axis extending in a lengthwise direction of the combustion chamber. 8. The combustion chamber as claimed in claim 1, wherein each of the fixing element bolts have at a first end an essentially hemispherical bolt head that is seated so as to allow tilting in a recess in a bolt holder mounted on the housing end, said recess being essentially hemispherical in cross-sectional view. 9. The combustion chamber as claimed in claim 8, wherein the second end of each bolt is fed through the respective guide hole in the wall structure and through a compression spring on the outer side of the wall structure, the compression spring being compressed against the outer side of the wall structure by means of a washer held at the second end of the bolt. 10. The combustion chamber as claimed in claim 1, wherein the housing is split in one sectional plane. 11. The combustion chamber as claimed in claim 1, wherein the cooling air inlet orifice is sized and configured to reduce impingement cooling and enhance convective cooling. 12. The combustion chamber as claimed in claim 11, wherein the axial length of cooling air inlet orifices is less that 50% of the total axial length of the housing. 13. The combustion chamber as claimed in claim 12, wherein the axial length of the cooling air inlet orifices is less that 20% of the total axial length of the housing. 14. The combustion chamber as claimed in claim 13, wherein a single cooling air inlet orifice is located in each portion of the housing split in one sectional plane. 15. The combustion chamber as claimed in claim 11, wherein two cooling air inlet orifices provide the cooling air. 16. A combustion chamber comprising: an outer wall structure surrounding an internal combustion area; a cooling air inlet orifice arranged adjacent to an interlocking joint on the outer wall structure such that where cooling air enters a cooling air channel, a section of a housing is cooled by impingement cooling and the housing extends from the burner to the hot gas outlet orifice; a burner projecting into the internal combustion area; an inner wall offset from the outer wall structure, the inner wall formed by a surface of the housing and cooled by convection by an air stream flowing between the outer wall structure and the inner wall, the air stream being conducted in a closed cooling air channel; and an outlet opening for the cooling air from the cooling air channel via which the cooling air is conducted to the burner for combustion purposes, whereby between the cooling air inlet orifice and the outlet opening the majority of the surface of the housing is cooled by convection by the cooling air stream; the housing supported in a rest position within the outer wall structure by a plurality of fixing elements urging the housing toward the outer wall structure in spring tension and by an interlocking joint comprising a flange of the housing extending into a slot formed in the outer wall structure, the interlocking joint providing positional support for the housing proximate a hot gas outlet orifice while allowing both axial and radial thermal growth there between; each fixing element compromising a bolt passing through a respective conical shaped guide hole compromising a narrowing diameter formed through the outer wall structure effective to create a rubbing by the respective bolt against the respective narrowing during operation of the combustion chamber thereby suppressing unwanted vibration of the housing.
연구과제 타임라인
LOADING...
LOADING...
LOADING...
LOADING...
LOADING...
이 특허에 인용된 특허 (11)
Maclin Harvey M. (Cincinnati OH), Combustion chamber construction.
Barbier Grard Y. G. (Morangis FRX) Laboure Grard J. P. B. (Avon FRX) Desaulty Michel A. A. (Vert-Saint-Denis FRX) Duchene Francois (Melun FRX) Truvillot Pascal M. (Courbevoie FRX), Combustion chamber structure for a turbojet engine.
Eriksson Torsten L. (Vargn SEX) Andersson John O. (Sjuntorp SEX) Nystrm Olle (Trollhttan SEX), Unit for combustion of process exhaust gas and production of hot air.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.