FR973589A - - Google Patents
Info
- Publication number
- FR973589A FR973589A FR973589DA FR973589A FR 973589 A FR973589 A FR 973589A FR 973589D A FR973589D A FR 973589DA FR 973589 A FR973589 A FR 973589A
- 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
- 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
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
Publications (1)
| Publication Number | Publication Date |
|---|---|
| FR973589A true FR973589A (nl) | 1951-02-12 |
Family
ID=1566814
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR973589D Expired FR973589A (nl) |
Country Status (1)
| Country | Link |
|---|---|
| FR (1) | FR973589A (nl) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3012962A (en) * | 1954-08-23 | 1961-12-12 | Shell Oil Co | Method of bringing a fluidized catalytic cracker-regenerator system on stream |
| US5201796A (en) * | 1991-10-15 | 1993-04-13 | United Technologies Corporation | Gas turbine engine arrangement |
-
0
- FR FR973589D patent/FR973589A/fr not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3012962A (en) * | 1954-08-23 | 1961-12-12 | Shell Oil Co | Method of bringing a fluidized catalytic cracker-regenerator system on stream |
| US5201796A (en) * | 1991-10-15 | 1993-04-13 | United Technologies Corporation | Gas turbine engine arrangement |