BE710710A - - Google Patents
Info
- Publication number
- BE710710A BE710710A BE710710DA BE710710A BE 710710 A BE710710 A BE 710710A BE 710710D A BE710710D A BE 710710DA BE 710710 A BE710710 A BE 710710A
- Authority
- BE
- Belgium
- Prior art keywords
- wall
- annular
- separator
- channel
- vortex
- Prior art date
Links
- 230000033001 locomotion Effects 0.000 claims description 33
- 239000012530 fluid Substances 0.000 claims description 21
- 238000000605 extraction Methods 0.000 claims description 12
- 238000011144 upstream manufacturing Methods 0.000 claims description 9
- 239000000463 material Substances 0.000 claims description 7
- 238000004519 manufacturing process Methods 0.000 claims description 6
- 238000004891 communication Methods 0.000 claims description 5
- 230000001629 suppression Effects 0.000 claims description 2
- 239000002245 particle Substances 0.000 description 44
- 238000000926 separation method Methods 0.000 description 7
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 6
- 239000000428 dust Substances 0.000 description 5
- 230000008859 change Effects 0.000 description 3
- 230000002829 reductive effect Effects 0.000 description 3
- 239000004576 sand Substances 0.000 description 3
- 230000008901 benefit Effects 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000003628 erosive effect Effects 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 230000009467 reduction Effects 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 230000001154 acute effect Effects 0.000 description 1
- 230000004323 axial length Effects 0.000 description 1
- 239000003638 chemical reducing agent Substances 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 239000012141 concentrate Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000001066 destructive effect Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 230000003670 easy-to-clean Effects 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 238000001914 filtration Methods 0.000 description 1
- 239000006260 foam Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000013021 overheating Methods 0.000 description 1
- 230000036961 partial effect Effects 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
- 230000008439 repair process Effects 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 150000003839 salts Chemical class 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
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
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/05—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for obviating the penetration of damaging objects or particles
-
- 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)
- Separating Particles In Gases By Inertia (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| BE710710 | 1968-02-13 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE710710A true BE710710A (enrdf_load_stackoverflow) | 1968-06-17 |
Family
ID=3852343
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE710710D BE710710A (enrdf_load_stackoverflow) | 1968-02-13 | 1968-02-13 |
Country Status (1)
| Country | Link |
|---|---|
| BE (1) | BE710710A (enrdf_load_stackoverflow) |
-
1968
- 1968-02-13 BE BE710710D patent/BE710710A/fr unknown
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| EP2488739B1 (fr) | Entrée d'air de moteur à turbine à gaz dans une nacelle | |
| EP3155234B1 (fr) | Turbomachine comprenant un systeme d'entrainement d'un equipement tel qu'un boitier d'accessoires | |
| FR2536789A1 (fr) | Moteur a turbine a gaz comportant un separateur de particules | |
| EP3377732B1 (fr) | Partie avant de turbomachine d'aéronef | |
| FR2538452A1 (fr) | Separateur de particules de flux d'air d'entree pour moteur a turbine a gaz | |
| EP2417359A1 (fr) | Prelevement d ' air avec filtre inertiel dans le rotor tandem d ' un compresseur | |
| FR3070448B1 (fr) | Aube de redresseur de soufflante de turbomachine, ensemble de turbomachine comprenant une telle aube et turbomachine equipee de ladite aube ou dudit ensemble | |
| BE1024684B1 (fr) | Bec degivrant de compresseur de turbomachine axiale | |
| FR2906569A1 (fr) | Entree d'air radiale polyvalente d'un turbomoteur. | |
| WO2009133308A2 (fr) | Prelevement d'air centripete dans un rotor de compresseur d'une turbomachine | |
| EP3325771B1 (fr) | Aeronef comportant deux soufflantes contrarotatives a l'arriere d'un fuselage avec calage des aubes de la soufflante aval | |
| FR2982842A1 (fr) | Avion | |
| FR3075867A1 (fr) | Dispositif de deshuilage d'une enceinte de lubrification de turbomachine | |
| FR3036144A1 (fr) | Helice de turbomachine | |
| BE710710A (enrdf_load_stackoverflow) | ||
| WO2013132190A1 (fr) | Générateurs de vortex placés dans le canal inter-aubes d'un redresseur de compresseur | |
| FR3090035A1 (fr) | Dispositif de deshuilage et d’etancheite d’une enceinte de lubrification de turbomachine | |
| FR2987876A1 (fr) | Reduction du bruit de prelevement | |
| BE710709A (enrdf_load_stackoverflow) | ||
| FR2951504A1 (fr) | Entree d'air de moteur a turbine a gaz dans une nacelle | |
| BE1024760B1 (fr) | Dispositif de degivrage pour turbomachine axiale | |
| EP4165287B1 (fr) | Dispositif de filtration d'un air de refroidissement d'une turbine de turbomachine | |
| EP3938626B1 (fr) | Redresseur de flux secondaire à tuyère integrêe | |
| FR2971553A1 (fr) | Procede pour reduire la signature acoustique d'un reacteur de propulsion et reacteur a signature acoustique reduite | |
| EP3174637A1 (fr) | Dispositif de séparation cyclonique comprenant deux cyclones reliés par une unité de canalisation optimisée |