IT941123B - Generatore avviatore - Google Patents
Generatore avviatoreInfo
- Publication number
- IT941123B IT941123B IT3092271A IT3092271A IT941123B IT 941123 B IT941123 B IT 941123B IT 3092271 A IT3092271 A IT 3092271A IT 3092271 A IT3092271 A IT 3092271A IT 941123 B IT941123 B IT 941123B
- Authority
- IT
- Italy
- Prior art keywords
- starter generator
- starter
- generator
- Prior art date
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
- 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
- F02C7/32—Arrangement, mounting, or driving, of auxiliaries
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB5404470A GB1277853A (en) | 1970-11-13 | 1970-11-13 | Gas turbine engines |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| IT941123B true IT941123B (it) | 1973-03-01 |
Family
ID=10469756
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| IT3092271A IT941123B (it) | 1970-11-13 | 1971-11-10 | Generatore avviatore |
Country Status (4)
| Country | Link |
|---|---|
| DE (1) | DE2155882A1 (it) |
| FR (1) | FR2113941B1 (it) |
| GB (1) | GB1277853A (it) |
| IT (1) | IT941123B (it) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4068470A (en) * | 1974-11-08 | 1978-01-17 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Gas turbine engine with convertible accessories |
| GB0315894D0 (en) * | 2003-07-08 | 2003-08-13 | Rolls Royce Plc | Aircraft engine arrangement |
-
1970
- 1970-11-13 GB GB5404470A patent/GB1277853A/en not_active Expired
-
1971
- 1971-11-10 IT IT3092271A patent/IT941123B/it active
- 1971-11-10 DE DE19712155882 patent/DE2155882A1/de active Pending
- 1971-11-12 FR FR7140542A patent/FR2113941B1/fr not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| FR2113941B1 (it) | 1975-07-18 |
| FR2113941A1 (it) | 1972-06-30 |
| DE2155882A1 (de) | 1972-05-25 |
| GB1277853A (en) | 1972-06-14 |
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