FR2028599A5 - - Google Patents
Info
- Publication number
- FR2028599A5 FR2028599A5 FR6900021A FR6900021A FR2028599A5 FR 2028599 A5 FR2028599 A5 FR 2028599A5 FR 6900021 A FR6900021 A FR 6900021A FR 6900021 A FR6900021 A FR 6900021A FR 2028599 A5 FR2028599 A5 FR 2028599A5
- Authority
- FR
- France
- 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
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/26—Controlling the air flow
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2250/00—Geometry
- F05B2250/40—Movement of component
- F05B2250/41—Movement of component with one degree of freedom
- F05B2250/411—Movement of component with one degree of freedom in rotation
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2260/00—Function
- F05B2260/70—Adjusting of angle of incidence or attack of rotating blades
-
- 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
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/00001—Arrangements using bellows, e.g. to adjust volumes or reduce thermal stresses
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Gas Burners (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Control Of Turbines (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB5129367 | 1967-11-10 | ||
| GB2809268A GB1256066A (en) | 1967-11-10 | 1967-11-10 | Flame tubes for gas turbine engines |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| FR2028599A5 true FR2028599A5 (enExample) | 1970-10-09 |
Family
ID=26259181
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR6900021A Expired FR2028599A5 (enExample) | 1967-11-10 | 1969-01-03 |
Country Status (3)
| Country | Link |
|---|---|
| AU (1) | AU4793068A (enExample) |
| FR (1) | FR2028599A5 (enExample) |
| GB (1) | GB1256066A (enExample) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2133832A1 (enExample) * | 1971-04-15 | 1972-12-01 | United Aircraft Canada | |
| EP0806611A1 (fr) * | 1996-05-09 | 1997-11-12 | SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION -Snecma | Systéme d'injection à geometrie variable adoptant un debit d'air en fonction du regime moteur |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS4873607A (enExample) * | 1972-01-10 | 1973-10-04 | ||
| US8966877B2 (en) * | 2010-01-29 | 2015-03-03 | United Technologies Corporation | Gas turbine combustor with variable airflow |
| DE102014204482A1 (de) | 2014-03-11 | 2015-09-17 | Rolls-Royce Deutschland Ltd & Co Kg | Brennkammer einer Gasturbine |
| CN114076324B (zh) * | 2022-01-19 | 2022-07-08 | 中国航发四川燃气涡轮研究院 | 能够自动调节掺混进气的燃烧室 |
-
1967
- 1967-11-10 GB GB2809268A patent/GB1256066A/en not_active Expired
-
1968
- 1968-12-17 AU AU47930/68A patent/AU4793068A/en not_active Expired
-
1969
- 1969-01-03 FR FR6900021A patent/FR2028599A5/fr not_active Expired
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2133832A1 (enExample) * | 1971-04-15 | 1972-12-01 | United Aircraft Canada | |
| EP0806611A1 (fr) * | 1996-05-09 | 1997-11-12 | SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION -Snecma | Systéme d'injection à geometrie variable adoptant un debit d'air en fonction du regime moteur |
| FR2748553A1 (fr) * | 1996-05-09 | 1997-11-14 | Snecma | Systeme d'injection a geometrie variable adoptant un debit d'air en fonction du regime moteur |
Also Published As
| Publication number | Publication date |
|---|---|
| DE1815695B2 (de) | 1976-07-15 |
| DE1815695A1 (de) | 1970-08-13 |
| GB1256066A (en) | 1971-12-08 |
| AU4793068A (en) | 1970-06-18 |
Similar Documents
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| ST | Notification of lapse |