GB607824A - Improvements relating to combustion chambers for prime movers - Google Patents
Improvements relating to combustion chambers for prime moversInfo
- Publication number
- GB607824A GB607824A GB436746A GB436746A GB607824A GB 607824 A GB607824 A GB 607824A GB 436746 A GB436746 A GB 436746A GB 436746 A GB436746 A GB 436746A GB 607824 A GB607824 A GB 607824A
- Authority
- GB
- United Kingdom
- Prior art keywords
- ring
- inner shell
- combustion chamber
- metal
- shell
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
- F23R3/60—Support structures; Attaching or mounting means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
Abstract
607,824. Gas turbine plant. LUCAS, Ltd., J., and HUYTON, A. Feb. 12, 1946, No. 4367. [Class 110 (iii)] [Also in Group XII] In a combustion chamber for a gas turbine or other prime movers comprising a pair of concentric metal shells the inner of which forms the combustion chamber and the two forming between them an annular air duct, the inner shell is supported from the outer by a sheet metal ring having a flat outer peripheral portion adapted to occupy a plane transverse the axis of the combustion chamber and having formed integrally with its inner periphery a plurality of supports for the inner shell. In the combustion chamber shown, Fig. 1, the inner shell a is supported from the outer shell b by a L- shaped member d gripped between a pair of flanges e on the outer shell. The cylindrical part of the ring d has three equidistantly spaced slits f formed in it and the metal between the slits and the edge of the ring is pressed inwardly to form substantially straight bridge pieces g which grip the inner shell a. In a modification, Fig. 3, the ring d<1> is formed with three T-shaped pieces d?. The stem d<3> of each T-piece is bent laterally to a U-form and the head d<4> is bent to a shallow V-form, the free ends of which are attached as by welding to the inner shell a. The Provisional Specification describes a modification of the arrangement shown in Fig. 1 in which the bridge pieces g are formed from the metal between two parallel slits f, in the cylindrical part of the ring d. Specification 584,820 is referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB436746A GB607824A (en) | 1946-02-12 | 1946-02-12 | Improvements relating to combustion chambers for prime movers |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB436746A GB607824A (en) | 1946-02-12 | 1946-02-12 | Improvements relating to combustion chambers for prime movers |
Publications (1)
Publication Number | Publication Date |
---|---|
GB607824A true GB607824A (en) | 1948-09-06 |
Family
ID=9775832
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB436746A Expired GB607824A (en) | 1946-02-12 | 1946-02-12 | Improvements relating to combustion chambers for prime movers |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB607824A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0014573A1 (en) * | 1979-02-01 | 1980-08-20 | Westinghouse Electric Corporation | Gas turbine combustion chamber |
FR2523646A1 (en) * | 1982-03-20 | 1983-09-23 | Rolls Royce | COMBUSTION EQUIPMENT SUPPORT DEVICE FOR GAS TURBINE ENGINE |
FR2599429A1 (en) * | 1986-05-28 | 1987-12-04 | Messerschmitt Boelkow Blohm | Support structure for a rocket-engine expansion nozzle |
FR2686683A1 (en) * | 1992-01-28 | 1993-07-30 | Snecma | TURBOMACHINE WITH REMOVABLE COMBUSTION CHAMBER. |
-
1946
- 1946-02-12 GB GB436746A patent/GB607824A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0014573A1 (en) * | 1979-02-01 | 1980-08-20 | Westinghouse Electric Corporation | Gas turbine combustion chamber |
FR2523646A1 (en) * | 1982-03-20 | 1983-09-23 | Rolls Royce | COMBUSTION EQUIPMENT SUPPORT DEVICE FOR GAS TURBINE ENGINE |
FR2599429A1 (en) * | 1986-05-28 | 1987-12-04 | Messerschmitt Boelkow Blohm | Support structure for a rocket-engine expansion nozzle |
FR2686683A1 (en) * | 1992-01-28 | 1993-07-30 | Snecma | TURBOMACHINE WITH REMOVABLE COMBUSTION CHAMBER. |
US5524430A (en) * | 1992-01-28 | 1996-06-11 | Societe National D'etude Et De Construction De Moteurs D'aviation S.N.E.C.M.A. | Gas-turbine engine with detachable combustion chamber |
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