FR1144879A - Exhaust manifold for gas turbine type airplane power plant - Google Patents
Exhaust manifold for gas turbine type airplane power plantInfo
- Publication number
- FR1144879A FR1144879A FR1144879DA FR1144879A FR 1144879 A FR1144879 A FR 1144879A FR 1144879D A FR1144879D A FR 1144879DA FR 1144879 A FR1144879 A FR 1144879A
- Authority
- FR
- France
- Prior art keywords
- gas turbine
- power plant
- exhaust manifold
- turbine type
- airplane power
- 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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/30—Exhaust heads, chambers, or the like
-
- 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
- F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1144879X | 1955-03-30 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1144879A true FR1144879A (en) | 1957-10-18 |
Family
ID=10877473
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1144879D Expired FR1144879A (en) | 1955-03-30 | 1956-03-28 | Exhaust manifold for gas turbine type airplane power plant |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR1144879A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3296804A (en) * | 1962-08-24 | 1967-01-10 | Rolls Royce | Gas turbine vertical lift engine |
FR2565293A1 (en) * | 1984-06-04 | 1985-12-06 | Aerospatiale | JET DILUATOR-DEVIATOR ASSEMBLY FOR AERODYNE TURBOMOTEUR |
-
1956
- 1956-03-28 FR FR1144879D patent/FR1144879A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3296804A (en) * | 1962-08-24 | 1967-01-10 | Rolls Royce | Gas turbine vertical lift engine |
FR2565293A1 (en) * | 1984-06-04 | 1985-12-06 | Aerospatiale | JET DILUATOR-DEVIATOR ASSEMBLY FOR AERODYNE TURBOMOTEUR |
EP0165167A1 (en) * | 1984-06-04 | 1985-12-18 | AEROSPATIALE Société Nationale Industrielle | Jet dilution and deviation device to suppress the infrared radiation of a turbo motor |
US4662174A (en) * | 1984-06-04 | 1987-05-05 | Societe Nationale Industrielle Et Aerospatiale | Plume diluter diverter assembly for a turbine engine of a heavier than air machine |
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