BE525244A - - Google Patents
Info
- Publication number
- BE525244A BE525244A BE525244DA BE525244A BE 525244 A BE525244 A BE 525244A BE 525244D A BE525244D A BE 525244DA BE 525244 A BE525244 A BE 525244A
- Authority
- BE
- Belgium
- Prior art keywords
- cooling fluid
- turbine
- established
- stream
- installation
- Prior art date
Links
- 239000012530 fluid Substances 0.000 claims description 48
- 238000001816 cooling Methods 0.000 claims description 34
- 238000007906 compression Methods 0.000 claims description 23
- 238000009434 installation Methods 0.000 claims description 21
- 238000002347 injection Methods 0.000 claims description 14
- 239000007924 injection Substances 0.000 claims description 14
- 238000002485 combustion reaction Methods 0.000 claims description 13
- 239000003380 propellant Substances 0.000 claims description 11
- 238000011144 upstream manufacturing Methods 0.000 claims description 7
- 239000000446 fuel Substances 0.000 claims description 5
- 239000000203 mixture Substances 0.000 claims description 5
- 230000015572 biosynthetic process Effects 0.000 claims description 4
- 238000006243 chemical reaction Methods 0.000 claims description 4
- 238000005755 formation reaction Methods 0.000 claims description 4
- GBMDVOWEEQVZKZ-UHFFFAOYSA-N methanol;hydrate Chemical compound O.OC GBMDVOWEEQVZKZ-UHFFFAOYSA-N 0.000 claims description 3
- 238000005070 sampling Methods 0.000 claims 1
- 239000000126 substance Substances 0.000 claims 1
- 239000002826 coolant Substances 0.000 description 20
- 239000007789 gas Substances 0.000 description 20
- 230000000694 effects Effects 0.000 description 3
- 239000007788 liquid Substances 0.000 description 2
- 238000009834 vaporization Methods 0.000 description 2
- 229920002456 HOTAIR Polymers 0.000 description 1
- QGZKDVFQNNGYKY-UHFFFAOYSA-N ammonia Chemical compound N QGZKDVFQNNGYKY-UHFFFAOYSA-N 0.000 description 1
- 238000009835 boiling Methods 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 230000000875 corresponding Effects 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 238000001704 evaporation Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 230000001141 propulsive Effects 0.000 description 1
Classifications
-
- 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
- F02K1/06—Varying effective area of jet pipe or nozzle
- F02K1/08—Varying effective area of jet pipe or nozzle by axially moving or transversely deforming an internal member, e.g. the exhaust cone
-
- 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
- F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
- F02C3/30—Adding water, steam or other fluids for influencing combustion, e.g. to obtain cleaner exhaust gases
- F02C3/305—Increasing the power, speed, torque or efficiency of a gas turbine or the thrust of a turbojet engine by injecting or adding water, steam or other fluids
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/212—Heat transfer, e.g. cooling by water injection
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE525244A true BE525244A (de) |
Family
ID=159598
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE525244D BE525244A (de) |
Country Status (1)
| Country | Link |
|---|---|
| BE (1) | BE525244A (de) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2669680A1 (fr) * | 1986-06-21 | 1992-05-29 | British Aerospace | Prefectionnements apportes a des moteurs a turbine a gaz ou les concernants. |
| WO1997043530A1 (en) * | 1996-05-14 | 1997-11-20 | The Dow Chemical Company | Process and apparatus for achieving power augmentation in gas turbines via wet compression |
| EP1344928A2 (de) | 2002-03-12 | 2003-09-17 | ROLLS-ROYCE plc | Düse mit veränderlichem Querschnitt |
| WO2007093760A1 (en) * | 2006-02-18 | 2007-08-23 | Rolls-Royce Plc | A gas turbine engine |
| EP3263849A1 (de) * | 2016-06-28 | 2018-01-03 | Safran Aero Boosters SA | Luftfahrzeug mit einem antriebssystem |
-
0
- BE BE525244D patent/BE525244A/fr unknown
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2669680A1 (fr) * | 1986-06-21 | 1992-05-29 | British Aerospace | Prefectionnements apportes a des moteurs a turbine a gaz ou les concernants. |
| WO1997043530A1 (en) * | 1996-05-14 | 1997-11-20 | The Dow Chemical Company | Process and apparatus for achieving power augmentation in gas turbines via wet compression |
| EP1108870A3 (de) * | 1996-05-14 | 2003-12-17 | The Dow Chemical Company | Methode und Einrichtung um die Leistung von Gasturbinen durch Verdunstungskühlung zu steigern |
| EP1344928A2 (de) | 2002-03-12 | 2003-09-17 | ROLLS-ROYCE plc | Düse mit veränderlichem Querschnitt |
| EP1344928A3 (de) * | 2002-03-12 | 2005-03-23 | ROLLS-ROYCE plc | Düse mit veränderlichem Querschnitt |
| WO2007093760A1 (en) * | 2006-02-18 | 2007-08-23 | Rolls-Royce Plc | A gas turbine engine |
| US8453458B2 (en) | 2006-02-18 | 2013-06-04 | Rolls-Royce Plc | Gas turbine engine variable exhaust nozzle |
| EP3263849A1 (de) * | 2016-06-28 | 2018-01-03 | Safran Aero Boosters SA | Luftfahrzeug mit einem antriebssystem |
| BE1024315B1 (fr) * | 2016-06-28 | 2018-01-30 | Safran Aero Boosters Sa | Système de propulsion pour aéronef |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| EP0333585B1 (de) | Kombinationstriebwerk, Rakete mit luftatmendem Turbinenstrahltriebwerk | |
| EP2643579B1 (de) | Kombination aus einem turboluftstrahltriebwerk und staustrahltriebwerk | |
| FR2599428A1 (fr) | Dispositif de propulsion combine pour aeronefs, en particulier pour avions spatiaux. | |
| FR2692936A1 (fr) | Appareil et procédé pour la canalisation d'air dans un turbomoteur. | |
| FR2859500A1 (fr) | Procede d'assemblage d'un moteur a turbines prevenant l'accumulation de glace dans le moteur et systeme de protection contre le gel | |
| EP0403372B1 (de) | Turbostrahl- und Raketenkombinationstriebwerk | |
| FR2889251A1 (fr) | Turbine a gaz et procede pour faire fonctionner celle-ci | |
| FR2870293A1 (fr) | Procedes et dispositifs pour assembler des turbomoteurs | |
| FR2686654A1 (fr) | Ameliorations dans la propulsion aerospatiale. | |
| FR2669680A1 (fr) | Prefectionnements apportes a des moteurs a turbine a gaz ou les concernants. | |
| FR3028888A1 (fr) | Dispositif de refroidissement pour une turbomachine alimente par un circuit de decharge | |
| FR2875269A1 (fr) | Systeme de refroidissement pour moteur a turbine a gaz ayant un systeme central ameliore | |
| EP2766591B1 (de) | Strahlantriebsvorrichtung und brennstoffzufuhrverfahren | |
| FR2687433A1 (fr) | Propulseur a composants inverses, a alimentation modulee. | |
| BE525244A (de) | ||
| EP0362052B1 (de) | Düsenkonstruktion für einen Kombinationsantrieb (Turbo-Staustrahl-Rakete) | |
| FR2487913A1 (fr) | Procede pour ameliorer le fonctionnement d'un turbo-compresseur de suralimentation d'un moteur thermique et turbo-compresseur pour la mise en oeuvre de ce procede | |
| EP2078822B1 (de) | Gasturbinenmotor mit Ventil für die Verbindung von zwei Behältern | |
| WO2021191528A1 (fr) | Turbomachine à double flux comprenant un dispositif de régulation du débit de fluide de refroidissement | |
| EP0473494B1 (de) | Brennstoffversorgungssystem für einen Turbomotor | |
| EP0362053B1 (de) | Konstruktion eines Kombinationsantriebs für zwei Funktionstypen | |
| FR3039220A1 (fr) | Dipositif de postcombustion pour turboreacteur | |
| EP0362054B1 (de) | Gaseinspritzrohre für ein Turbinenstrahl- und Raketentriebwerk | |
| CH277880A (fr) | Installation de propulsion par réaction. | |
| FR2777943A1 (fr) | Moteur thermique a capsulismes differencies et apport de chaleur continu |