BE463884A - - Google Patents
Info
- Publication number
- BE463884A BE463884A BE463884DA BE463884A BE 463884 A BE463884 A BE 463884A BE 463884D A BE463884D A BE 463884DA BE 463884 A BE463884 A BE 463884A
- Authority
- BE
- Belgium
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
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
- F02C6/20—Adaptations of gas-turbine plants for driving vehicles
- F02C6/206—Adaptations of gas-turbine plants for driving vehicles the vehicles being airscrew driven
-
- 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
- F02C3/10—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with another turbine driving an output shaft but not driving the compressor
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB257003X | 1944-03-29 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE463884A true BE463884A (xx) |
Family
ID=10231879
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE463884D BE463884A (xx) | 1944-03-29 |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US2589078A (xx) |
| BE (1) | BE463884A (xx) |
| CH (1) | CH257003A (xx) |
| FR (1) | FR923473A (xx) |
| GB (1) | GB602584A (xx) |
Families Citing this family (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2756561A (en) * | 1952-01-18 | 1956-07-31 | Rolls Royce | Gas turbine engine with axial-flow compressor and bearing means for supporting the compressor rotor |
| US2914918A (en) * | 1955-12-28 | 1959-12-01 | Poly Ind Inc | Gas turbine jet engine starter with serially-connected concentrically-arranged combustion chambers |
| US3412849A (en) * | 1964-10-01 | 1968-11-26 | M. Dominique Delerue | Yarn package |
| US9869240B2 (en) | 2015-02-20 | 2018-01-16 | Pratt & Whitney Canada Corp. | Compound engine assembly with cantilevered compressor and turbine |
| US10428734B2 (en) | 2015-02-20 | 2019-10-01 | Pratt & Whitney Canada Corp. | Compound engine assembly with inlet lip anti-icing |
| US10408123B2 (en) | 2015-02-20 | 2019-09-10 | Pratt & Whitney Canada Corp. | Engine assembly with modular compressor and turbine |
| US20160245162A1 (en) | 2015-02-20 | 2016-08-25 | Pratt & Whitney Canada Corp. | Compound engine assembly with offset turbine shaft, engine shaft and inlet duct |
| US10371060B2 (en) | 2015-02-20 | 2019-08-06 | Pratt & Whitney Canada Corp. | Compound engine assembly with confined fire zone |
| US10533492B2 (en) * | 2015-02-20 | 2020-01-14 | Pratt & Whitney Canada Corp. | Compound engine assembly with mount cage |
| US10533500B2 (en) | 2015-02-20 | 2020-01-14 | Pratt & Whitney Canada Corp. | Compound engine assembly with mount cage |
Family Cites Families (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1959795A (en) * | 1931-10-24 | 1934-05-22 | Aktienbolaget Milo | Gas turbine system for varying load |
| US2050349A (en) * | 1931-11-23 | 1936-08-11 | Milo Ab | Gas turbine system for aerial propulsion |
| US2243467A (en) * | 1937-02-13 | 1941-05-27 | Jendrassik George | Process and equipment for gas turbines |
| US2292288A (en) * | 1937-06-02 | 1942-08-04 | Soc Es Energie Sa | Means for driving the propelling system of aircraft |
| US2326072A (en) * | 1939-06-28 | 1943-08-03 | Bbc Brown Boveri & Cie | Gas turbine plant |
| US2409446A (en) * | 1941-11-10 | 1946-10-15 | Northrop Aircraft Inc | Airplane power plant |
| US2411227A (en) * | 1941-11-17 | 1946-11-19 | Andre P E Planiol | Power plant for airplanes |
| US2504414A (en) * | 1943-10-11 | 1950-04-18 | Power Jets Res & Dev Ltd | Gas turbine propulsion unit |
| US2454738A (en) * | 1944-01-31 | 1948-11-23 | Power Jets Res And Development | Internal-combustion turbine power plant |
-
0
- BE BE463884D patent/BE463884A/xx unknown
-
1944
- 1944-03-29 GB GB5847/44A patent/GB602584A/en not_active Expired
-
1945
- 1945-03-27 US US585167A patent/US2589078A/en not_active Expired - Lifetime
-
1946
- 1946-01-19 CH CH257003D patent/CH257003A/de unknown
- 1946-03-07 FR FR923473D patent/FR923473A/fr not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| CH257003A (de) | 1948-09-15 |
| US2589078A (en) | 1952-03-11 |
| GB602584A (en) | 1948-05-31 |
| FR923473A (fr) | 1947-07-08 |