GB615915A - Improvements in or relating to jet-propulsion and gas-turbine power-units - Google Patents
Improvements in or relating to jet-propulsion and gas-turbine power-unitsInfo
- Publication number
- GB615915A GB615915A GB9201/46A GB920146A GB615915A GB 615915 A GB615915 A GB 615915A GB 9201/46 A GB9201/46 A GB 9201/46A GB 920146 A GB920146 A GB 920146A GB 615915 A GB615915 A GB 615915A
- Authority
- GB
- United Kingdom
- Prior art keywords
- joint
- combustion chamber
- ring
- power unit
- gas
- 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
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
-
- 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)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Joints Allowing Movement (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
615,915. Gas-turbine plant. OULIANOFF, G. March 25, 1946, Nos. 9201 and 20677. [Class 110 (iii)] [Also in Group XXVIII] In a jet propulsion or gas turbine power unit in which the combustion chamber is supported at one end by a joint connecting it to the compressor casing or to a member rigidly connected to the compressor casing and at its other end by a joint connecting it to a member of the power unit, the joint at one of the ends of the combustion chamber locates the combustion chamber axially and allows a limited range of universal angular setting of the combustion chamber relative to the member of the power unit to which it is connected. The joint, Fig. 2, connecting the combustion chamber to the outlet 8 from the compressor comprises a ring 11 which is spigotted in the outlet 8 and which has a spherical joint face 10 which co-operates with a similar face on the inlet to the combustion chamber. The joint is held together by bolts 9. The joint, Fig. 4, connecting the combustion chamber to the nozzle box 18 comprises a ring-member 16 which has, on one side, a spherical surface 20 engaged by a corresponding surface of a ring nut 19 and which is separated on the other side, from the flange of the nozzle box 18 by a packing ring 21 of flexible material. The ring 21 may be a steel-and-asbestos washer. The joint of Fig. 4 may be replaced by one according to Specification 584,820.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB270343X | 1946-03-25 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB615915A true GB615915A (en) | 1949-01-13 |
Family
ID=10253082
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB9201/46A Expired GB615915A (en) | 1946-03-25 | 1946-03-25 | Improvements in or relating to jet-propulsion and gas-turbine power-units |
Country Status (2)
| Country | Link |
|---|---|
| CH (1) | CH270343A (en) |
| GB (1) | GB615915A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2608057A (en) * | 1949-12-24 | 1952-08-26 | A V Roe Canada Ltd | Gas turbine nozzle box |
| US2637163A (en) * | 1951-04-26 | 1953-05-05 | Westinghouse Electric Corp | Jet engine variable area exhaust nozzle |
| DE2756963A1 (en) * | 1976-12-23 | 1978-06-29 | Gen Electric | DOSING DEVICE FOR COOLANT FLOW |
| FR2467980A1 (en) * | 1979-10-22 | 1981-04-30 | Gen Electric | HIGH TEMPERATURE RESISTANT CUSHION FOR LOW DUCTILITY PART |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE952669C (en) * | 1951-12-20 | 1956-11-22 | Ruston & Hornsby Ltd | Gas turbine plant |
| US4686823A (en) * | 1986-04-28 | 1987-08-18 | United Technologies Corporation | Sliding joint for an annular combustor |
| DE4232385A1 (en) * | 1992-09-26 | 1994-03-31 | Asea Brown Boveri | Gas turbine with flanged exhaust housing |
-
1946
- 1946-03-25 GB GB9201/46A patent/GB615915A/en not_active Expired
-
1947
- 1947-03-24 CH CH270343D patent/CH270343A/en unknown
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2608057A (en) * | 1949-12-24 | 1952-08-26 | A V Roe Canada Ltd | Gas turbine nozzle box |
| US2637163A (en) * | 1951-04-26 | 1953-05-05 | Westinghouse Electric Corp | Jet engine variable area exhaust nozzle |
| DE2756963A1 (en) * | 1976-12-23 | 1978-06-29 | Gen Electric | DOSING DEVICE FOR COOLANT FLOW |
| FR2467980A1 (en) * | 1979-10-22 | 1981-04-30 | Gen Electric | HIGH TEMPERATURE RESISTANT CUSHION FOR LOW DUCTILITY PART |
Also Published As
| Publication number | Publication date |
|---|---|
| CH270343A (en) | 1950-08-31 |
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