BE462490A - - Google Patents
Info
- Publication number
- BE462490A BE462490A BE462490DA BE462490A BE 462490 A BE462490 A BE 462490A BE 462490D A BE462490D A BE 462490DA BE 462490 A BE462490 A BE 462490A
- Authority
- BE
- Belgium
- Prior art keywords
- fan
- turbine
- compressor
- rotor
- caged
- Prior art date
Links
- 239000000446 fuel Substances 0.000 claims description 7
- 150000001875 compounds Chemical class 0.000 claims description 6
- 239000003380 propellant Substances 0.000 claims description 5
- 230000005540 biological transmission Effects 0.000 claims description 3
- 239000000126 substance Substances 0.000 claims 1
- 238000002485 combustion reaction Methods 0.000 description 11
- 239000007789 gas Substances 0.000 description 7
- 210000000188 Diaphragm Anatomy 0.000 description 6
- 238000011144 upstream manufacturing Methods 0.000 description 5
- 210000001331 Nose Anatomy 0.000 description 2
- 238000002347 injection Methods 0.000 description 2
- 239000007924 injection Substances 0.000 description 2
- 229920002892 amber Polymers 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 150000002500 ions Chemical class 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 210000000056 organs Anatomy 0.000 description 1
- 230000001141 propulsive Effects 0.000 description 1
- 238000003303 reheating Methods 0.000 description 1
- 230000002441 reversible Effects 0.000 description 1
- 230000037303 wrinkles 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
- 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
- F02K3/06—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 with front fan
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 |
|---|---|
| BE462490A true BE462490A (de) |
Family
ID=114886
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE462490D BE462490A (de) |
Country Status (1)
| Country | Link |
|---|---|
| BE (1) | BE462490A (de) |
-
0
- BE BE462490D patent/BE462490A/fr unknown
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US2504181A (en) | Double compound independent rotor | |
| EP2478198B1 (de) | Turbomotor mit parallelen wellen | |
| EP3111077B1 (de) | Lüfterrad für eine turbomaschine wie etwa ein mehrstrom-turbostrahltriebwerk mit untersetzungsgetriebe | |
| US2430399A (en) | Jet augmenter for combustion turbine propulsion plants | |
| FR2581423A1 (fr) | Turbine de travail a contre-rotation | |
| FR2929338A1 (fr) | Chambre de post-combustion pour moteur a turbine a gaz | |
| CN108518289A (zh) | 一种叶尖喷气自驱动轮式风扇发动机 | |
| US2589078A (en) | Aircraft propulsion power plant | |
| FR3036140A1 (fr) | Turbomachine d'aeronef a effet coanda | |
| BE462490A (de) | ||
| CA2839248C (fr) | Architecture double corps de turbomoteur avec compresseur haute pression lie a la turbine basse pression | |
| FR3131755A1 (fr) | Turbomoteur a cycle récupéré | |
| FR2961857A1 (fr) | Tube d'alimentation en air de refroidissement d'une turbine d'un turbomoteur, et turbomoteur equipe d'un tel tube | |
| FR3107308A1 (fr) | Système de soufflage pour système propulsif d’aéronef | |
| FR3080652A1 (fr) | Turbomachine a architecture inversee, optionnellement pourvue d'un recuperateur de chaleur en sortie de turbine basse pression | |
| FR2576358A1 (fr) | Module haute-pression et haute-temperature pour turboreacteurs | |
| FR3092621A1 (fr) | Turbomachine pourvue d’un récupérateur de chaleur en sortie de turbine | |
| FR3041932A3 (fr) | Ensemble de propulsion d'un aeronef comportant au moins deux soufflantes deportees | |
| EP1359309B1 (de) | Gasturbine mit einer Loben- und Röhren-Mischvorrichtung | |
| FR3131939A1 (fr) | Bec de séparation de turbomachine axiale comprenant un passage de débit d’air de dégivrage s’étandant jusqu’au redresseur | |
| RU2840U1 (ru) | Роторно-реактивный двигатель | |
| FR3131756A1 (fr) | Turbomoteur a cycle récupéré | |
| BE463885A (de) | ||
| FR2951503A1 (fr) | Entree d air de moteur a turbine a gaz dans une nacelle | |
| BE462714A (de) |