CH310034A - Combustion device for gas turbine installation. - Google Patents
Combustion device for gas turbine installation.Info
- Publication number
- CH310034A CH310034A CH310034DA CH310034A CH 310034 A CH310034 A CH 310034A CH 310034D A CH310034D A CH 310034DA CH 310034 A CH310034 A CH 310034A
- Authority
- CH
- Switzerland
- Prior art keywords
- gas turbine
- combustion device
- turbine installation
- installation
- combustion
- Prior art date
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
- F23R3/46—Combustion chambers comprising an annular arrangement of several essentially tubular flame tubes within a common annular casing or within individual casings
- F23R3/48—Flame tube interconnectors, e.g. cross-over tubes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/26—Starting; Ignition
- F02C7/264—Ignition
- F02C7/266—Electric
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)
- Ignition Installations For Internal Combustion Engines (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB310034X | 1950-03-06 |
Publications (1)
Publication Number | Publication Date |
---|---|
CH310034A true CH310034A (en) | 1955-09-30 |
Family
ID=10316462
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH310034D CH310034A (en) | 1950-03-06 | 1951-03-06 | Combustion device for gas turbine installation. |
Country Status (4)
Country | Link |
---|---|
CH (1) | CH310034A (en) |
DE (1) | DE882775C (en) |
FR (1) | FR1033404A (en) |
GB (1) | GB691366A (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2952126A (en) * | 1955-05-10 | 1960-09-13 | Midland Ross Corp | Combustion unit for supplying hot gas for jet aircraft |
-
1950
- 1950-03-06 GB GB5582/50A patent/GB691366A/en not_active Expired
-
1951
- 1951-03-05 FR FR1033404D patent/FR1033404A/en not_active Expired
- 1951-03-06 CH CH310034D patent/CH310034A/en unknown
- 1951-03-07 DE DEC3895A patent/DE882775C/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
FR1033404A (en) | 1953-07-10 |
GB691366A (en) | 1953-05-13 |
DE882775C (en) | 1953-07-13 |
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