NL62040C - - Google Patents
Info
- Publication number
- NL62040C NL62040C NL62040DA NL62040C NL 62040 C NL62040 C NL 62040C NL 62040D A NL62040D A NL 62040DA NL 62040 C NL62040 C NL 62040C
- Authority
- NL
- Netherlands
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
- 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
- F02K1/04—Mounting of an exhaust cone in the jet pipe
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Control Of Turbines (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB257833X | 1942-02-02 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| NL62040C true NL62040C (US06818201-20041116-C00086.png) |
Family
ID=10233221
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| NL62040D NL62040C (US06818201-20041116-C00086.png) | 1942-02-02 |
Country Status (6)
Families Citing this family (21)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2828603A (en) * | 1948-04-09 | 1958-04-01 | Westinghouse Electric Corp | Afterburner for turbo jet engines and the like |
| US2714287A (en) * | 1950-01-03 | 1955-08-02 | Westinghouse Electric Corp | Flameholder device for turbojet afterburner |
| GB685939A (en) * | 1950-05-17 | 1953-01-14 | Rolls Royce | Improvements in or relating to gas-turbine engine structures |
| US2813396A (en) * | 1952-02-20 | 1957-11-19 | Solar Aircraft Co | Tail cone and resilient mounting therefor |
| GB761444A (en) * | 1953-06-26 | 1956-11-14 | Glover Webb Liversidge Ltd | Improvements in or relating to tipping vehicles |
| US2938336A (en) * | 1956-12-06 | 1960-05-31 | United Aircraft Corp | Gas flow straightening vanes |
| US2919888A (en) * | 1957-04-17 | 1960-01-05 | United Aircraft Corp | Turbine bearing support |
| US3024969A (en) * | 1957-12-26 | 1962-03-13 | Gen Electric | Compressor rear frame |
| CA623385A (en) * | 1959-03-13 | 1961-07-04 | R. Reese Homer | Elastic fluid branch conduit structure |
| US3778185A (en) * | 1972-08-28 | 1973-12-11 | United Aircraft Corp | Composite strut joint construction |
| FR2534222A1 (fr) * | 1982-10-06 | 1984-04-13 | Aerospatiale | Agencement de rotor de queue a poussee accrue pour aeronef a voilure tournante et dispositif pour accroitre la poussee d'un tel agencement |
| US4989406A (en) * | 1988-12-29 | 1991-02-05 | General Electric Company | Turbine engine assembly with aft mounted outlet guide vanes |
| DE4329623A1 (de) * | 1993-09-02 | 1995-03-09 | Abb Management Ag | Abgasdiffusor |
| DE19729433C1 (de) * | 1997-07-09 | 1998-08-13 | Siemens Ag | Stützvorrichtung für einen temperaturbeaufschlagten Kanal |
| US6584766B1 (en) * | 2000-03-24 | 2003-07-01 | General Electric Co. | Methods and apparatus for minimizing thermal stresses in a centerbody |
| US6807803B2 (en) * | 2002-12-06 | 2004-10-26 | General Electric Company | Gas turbine exhaust diffuser |
| FR2988434B1 (fr) * | 2012-03-20 | 2016-02-05 | Aircelle Sa | Cone d'ejection des gaz pour turboreacteurs d'aeronefs |
| WO2014186018A2 (en) | 2013-03-13 | 2014-11-20 | United Technologies Corporation | Nosecone support |
| WO2014158283A1 (en) * | 2013-03-14 | 2014-10-02 | Bronwyn Power | A subsonic shock strut |
| US9644497B2 (en) * | 2013-11-22 | 2017-05-09 | Siemens Energy, Inc. | Industrial gas turbine exhaust system with splined profile tail cone |
| DE102017130563A1 (de) * | 2017-12-19 | 2019-06-19 | Rolls-Royce Deutschland Ltd & Co Kg | Schubdüse für ein Turbofan-Triebwerk eines Überschallflugzeugs |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE319776C (de) * | 1920-04-03 | Hannoversche Waggonfabrik Akt | Bekleidung fuer zwei oder mehr Flugzeugverspannungsorgane | |
| FR15364E (fr) * | 1911-07-03 | 1912-06-25 | Societe R Bourbeau Et H Devaux | Aéroplane à coque directrice |
| US1065118A (en) * | 1912-05-23 | 1913-06-17 | Albert B Doering | Flame and spark arrester. |
| GB126707A (en) * | 1917-02-21 | 1919-05-22 | William John Dickinson | An Improvement in the Means for Utilising the Kinitic Energy of Air Currents. |
| US2207522A (en) * | 1938-03-24 | 1940-07-09 | Bell Telephone Labor Inc | Concentric conductor transmission line |
| US2393808A (en) * | 1943-12-29 | 1946-01-29 | Westinghouse Electric Corp | Blower apparatus |
-
0
- BE BE462020D patent/BE462020A/xx unknown
- NL NL62040D patent/NL62040C/xx active
-
1942
- 1942-02-02 GB GB1396/42A patent/GB582978A/en not_active Expired
-
1945
- 1945-08-24 US US612467A patent/US2516819A/en not_active Expired - Lifetime
- 1945-11-29 CH CH257833D patent/CH257833A/de unknown
- 1945-11-30 FR FR918158D patent/FR918158A/fr not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| US2516819A (en) | 1950-07-25 |
| FR918158A (fr) | 1947-01-31 |
| BE462020A (US06818201-20041116-C00086.png) | |
| CH257833A (de) | 1948-10-31 |
| GB582978A (en) | 1946-12-04 |
