GB701099A - Improvements to combustion chambers - Google Patents
Improvements to combustion chambersInfo
- Publication number
- GB701099A GB701099A GB1273550A GB1273550A GB701099A GB 701099 A GB701099 A GB 701099A GB 1273550 A GB1273550 A GB 1273550A GB 1273550 A GB1273550 A GB 1273550A GB 701099 A GB701099 A GB 701099A
- Authority
- GB
- United Kingdom
- Prior art keywords
- plunger
- flame tube
- abutment piece
- body part
- supported
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
701,099. Generating combustion products under pressure. LUCAS, Ltd., J. April 5, 1951 [May 22, 1950], No. 12735/50. Class 51 (1) In an air-jacketed type of combustion chamber for a gas turbine or jet propulsion engine, the flame tube is supported within the outer casing by means of devices each comprising a hollow body part f having an inwardly-directed lip j at its inner end, an abutment piece k adjustably secured in the body part, a plunger n extending through the lipped end of the body and a spring p disposed between the plunger and the abutment piece. The abutment piece is in screw-threaded engagement with the body part and is locked by means of pegs m on the cover plate g. The flame tube is supported by three plungers, the upper one engaging a socket on the flame tube to prevent axial movement thereof and the two lower ones bearing against pads on the flame tube. In a second embodiment, the plunger has a central stem which engages in a recess in the abutment piece so as to guide the plunger, and coil type springs are employed in place of the resilient washers p shown in Fig. 3. Specification 656,012 is referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1273550A GB701099A (en) | 1950-05-22 | 1950-05-22 | Improvements to combustion chambers |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1273550A GB701099A (en) | 1950-05-22 | 1950-05-22 | Improvements to combustion chambers |
Publications (1)
Publication Number | Publication Date |
---|---|
GB701099A true GB701099A (en) | 1953-12-16 |
Family
ID=10010136
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1273550A Expired GB701099A (en) | 1950-05-22 | 1950-05-22 | Improvements to combustion chambers |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB701099A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1084087B (en) * | 1948-11-30 | 1960-06-23 | Joseph Szydlowski | Combustion chamber arrangement |
FR2467980A1 (en) * | 1979-10-22 | 1981-04-30 | Gen Electric | HIGH TEMPERATURE RESISTANT CUSHION FOR LOW DUCTILITY PART |
GB2147405A (en) * | 1983-09-28 | 1985-05-09 | Rolls Royce | Gas turbine engine combustion chamber mounting |
EP0216721A1 (en) * | 1985-07-03 | 1987-04-01 | United Technologies Corporation | Liner construction |
WO2007104587A2 (en) * | 2006-03-15 | 2007-09-20 | Siemens Aktiengesellschaft | Method for mounting a mixing housing in a gas turbine, and adjusting device therefor |
CN105605605A (en) * | 2016-01-25 | 2016-05-25 | 西北工业大学 | Anti-vibration cooling wall of ground gas turbine combustion chamber |
-
1950
- 1950-05-22 GB GB1273550A patent/GB701099A/en not_active Expired
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1084087B (en) * | 1948-11-30 | 1960-06-23 | Joseph Szydlowski | Combustion chamber arrangement |
FR2467980A1 (en) * | 1979-10-22 | 1981-04-30 | Gen Electric | HIGH TEMPERATURE RESISTANT CUSHION FOR LOW DUCTILITY PART |
GB2147405A (en) * | 1983-09-28 | 1985-05-09 | Rolls Royce | Gas turbine engine combustion chamber mounting |
EP0216721A1 (en) * | 1985-07-03 | 1987-04-01 | United Technologies Corporation | Liner construction |
WO2007104587A2 (en) * | 2006-03-15 | 2007-09-20 | Siemens Aktiengesellschaft | Method for mounting a mixing housing in a gas turbine, and adjusting device therefor |
WO2007104587A3 (en) * | 2006-03-15 | 2009-01-22 | Siemens Ag | Method for mounting a mixing housing in a gas turbine, and adjusting device therefor |
CN105605605A (en) * | 2016-01-25 | 2016-05-25 | 西北工业大学 | Anti-vibration cooling wall of ground gas turbine combustion chamber |
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