CH251279A - Antriebsanlage an Flugzeugen. - Google Patents
Antriebsanlage an Flugzeugen.Info
- Publication number
- CH251279A CH251279A CH251279DA CH251279A CH 251279 A CH251279 A CH 251279A CH 251279D A CH251279D A CH 251279DA CH 251279 A CH251279 A CH 251279A
- Authority
- CH
- Switzerland
- Prior art keywords
- aircraft
- propulsion system
- propulsion
- 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
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/02—Gas-turbine plants characterised by the use of combustion products as the working fluid using exhaust-gas pressure in a pressure exchanger to compress combustion-air
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
- F02K7/02—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the jet being intermittent, i.e. pulse-jet
- F02K7/06—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the jet being intermittent, i.e. pulse-jet with combustion chambers having valves
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
- Supercharger (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CH606544X | 1945-12-29 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CH251279A true CH251279A (de) | 1947-10-15 |
Family
ID=4523115
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CH251279D CH251279A (de) | 1945-12-29 | 1945-12-29 | Antriebsanlage an Flugzeugen. |
Country Status (3)
| Country | Link |
|---|---|
| CH (1) | CH251279A (de) |
| FR (1) | FR937689A (de) |
| GB (1) | GB606544A (de) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1987006976A1 (fr) * | 1986-05-14 | 1987-11-19 | Daniel Buchser | Statoreacteur |
| EP0503277A1 (de) * | 1991-03-12 | 1992-09-16 | Asea Brown Boveri Ag | Gasturbogruppe |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0468083B1 (de) * | 1990-07-27 | 1995-11-15 | Asea Brown Boveri Ag | Verfahren zur Aufbereitung des Arbeitsgases in einer Gasturbinenanlage |
-
1945
- 1945-12-29 CH CH251279D patent/CH251279A/de unknown
-
1946
- 1946-02-25 GB GB5879/46A patent/GB606544A/en not_active Expired
- 1946-12-28 FR FR937689D patent/FR937689A/fr not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1987006976A1 (fr) * | 1986-05-14 | 1987-11-19 | Daniel Buchser | Statoreacteur |
| EP0503277A1 (de) * | 1991-03-12 | 1992-09-16 | Asea Brown Boveri Ag | Gasturbogruppe |
Also Published As
| Publication number | Publication date |
|---|---|
| FR937689A (fr) | 1948-08-24 |
| GB606544A (en) | 1948-08-16 |
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