BE433598A - - Google Patents
Info
- Publication number
- BE433598A BE433598A BE433598DA BE433598A BE 433598 A BE433598 A BE 433598A BE 433598D A BE433598D A BE 433598DA BE 433598 A BE433598 A BE 433598A
- Authority
- BE
- Belgium
- Prior art keywords
- tube
- air
- accumulation
- ram
- aerodynamic
- Prior art date
Links
- 238000009825 accumulation Methods 0.000 claims description 36
- 238000002485 combustion reaction Methods 0.000 claims description 9
- 230000000694 effects Effects 0.000 claims description 7
- 239000007789 gas Substances 0.000 claims description 5
- 230000033001 locomotion Effects 0.000 claims description 5
- 238000000034 method Methods 0.000 claims description 3
- 238000010408 sweeping Methods 0.000 claims 1
- 230000006835 compression Effects 0.000 description 7
- 238000007906 compression Methods 0.000 description 7
- 239000012528 membrane Substances 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 230000001133 acceleration Effects 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 239000002826 coolant Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B27/00—Use of kinetic or wave energy of charge in induction systems, or of combustion residues in exhaust systems, for improving quantity of charge or for increasing removal of combustion residues
- F02B27/005—Oscillating pipes with charging achieved by arrangement, dimensions or shapes of intakes pipes or chambers; Ram air pipes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B27/00—Use of kinetic or wave energy of charge in induction systems, or of combustion residues in exhaust systems, for improving quantity of charge or for increasing removal of combustion residues
- F02B27/04—Use of kinetic or wave energy of charge in induction systems, or of combustion residues in exhaust systems, for improving quantity of charge or for increasing removal of combustion residues in exhaust systems only, e.g. for sucking-off combustion gases
-
- 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
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Jet Pumps And Other Pumps (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Publications (1)
Publication Number | Publication Date |
---|---|
BE433598A true BE433598A (enrdf_load_stackoverflow) |
Family
ID=92935
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BE433598D BE433598A (enrdf_load_stackoverflow) |
Country Status (1)
Country | Link |
---|---|
BE (1) | BE433598A (enrdf_load_stackoverflow) |
-
0
- BE BE433598D patent/BE433598A/fr unknown
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP3325346B1 (fr) | Aeronef comprenant un propulseur arriere carene avec stator d'entree a volets mobiles | |
EP1775441A1 (fr) | Dispositif de suralimentation pour moteur à combustion interne, et véhicule automobile équipé d'un tel dispositif | |
FR2692936A1 (fr) | Appareil et procédé pour la canalisation d'air dans un turbomoteur. | |
WO2017013363A1 (fr) | Aeronef avec un ensemble propulsif comprenant une soufflante a l'arriere du fuselage | |
FR2614072A1 (fr) | Moteur-turbopropulseur a turbine a gaz | |
EP3325778B1 (fr) | Aeronef comprenant un propulseur arriere carene avec stator d'entree comprenant une fonction soufflage | |
FR2910937A1 (fr) | Nacelle de reacteur d'aeronef et aeronef comportant une telle nacelle | |
FR3028888A1 (fr) | Dispositif de refroidissement pour une turbomachine alimente par un circuit de decharge | |
FR3050763A1 (fr) | Dispositif de circulation d'air pour une turbomachine comportant un systeme de derivation d'air chaud vers un echangeur de chaleur | |
FR3041933A1 (fr) | Aeronef avec un ensemble propulsif comprenant un doublet d'helices a l'arriere du fuselage | |
EP3325792B1 (fr) | Ensemble propulsif pour aéronef comportant un inverseur de poussée | |
EP3325771B1 (fr) | Aeronef comportant deux soufflantes contrarotatives a l'arriere d'un fuselage avec calage des aubes de la soufflante aval | |
WO2017013360A1 (fr) | Aeronef comportant une turbomachine integree au fuselage arriere a alimentation variable | |
CA2798679C (fr) | Dispositif pour attenuer le bruit emis par le jet d'un moteur de propulsion d'un aeronef | |
CA2835353C (fr) | Cone arriere de turboreacteur tournant a micro-jets | |
FR2596809A1 (fr) | Perfectionnements de tuyeres orientables pour aeronefs | |
CA2788903A1 (fr) | Tuyere de flux froid d'un turboreacteur a double flux a flux separes incorporant un inverseur de poussee a grilles | |
BE433598A (enrdf_load_stackoverflow) | ||
WO2013041818A1 (fr) | Capot primaire de turboréacteur double flux comportant une couronne tournante a micro-jets | |
FR3042820A1 (fr) | Dispositif de ventilation d'un compartiment de turbomachine | |
FR3083266A1 (fr) | Ensemble pour turbomachine d'aeronef comportant un systeme ameliore de lubrification d'un reducteur d'entrainement de soufflante en cas d'autorotation de la soufflante | |
BE537785A (enrdf_load_stackoverflow) | ||
FR2665485A1 (fr) | Moteur a turbine a gaz. | |
FR3039202A1 (fr) | Aeronef comportant une turbomachine integree au fuselage arriere a alimentation variable | |
FR2582054A1 (fr) | Moteur rotatif a gaz comprime et/ou a combustion interne |