CA2516700C - Ensemble moteur combine compact - Google Patents
Ensemble moteur combine compact Download PDFInfo
- Publication number
- CA2516700C CA2516700C CA2516700A CA2516700A CA2516700C CA 2516700 C CA2516700 C CA 2516700C CA 2516700 A CA2516700 A CA 2516700A CA 2516700 A CA2516700 A CA 2516700A CA 2516700 C CA2516700 C CA 2516700C
- Authority
- CA
- Canada
- Prior art keywords
- engine
- turbine
- rotary
- cycle
- casing
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 150000001875 compounds Chemical class 0.000 title claims abstract description 29
- 238000001816 cooling Methods 0.000 claims description 31
- 238000002485 combustion reaction Methods 0.000 claims description 18
- 239000000446 fuel Substances 0.000 claims description 11
- 239000007858 starting material Substances 0.000 claims description 4
- 239000002826 coolant Substances 0.000 claims description 3
- 239000003570 air Substances 0.000 description 41
- 239000007789 gas Substances 0.000 description 14
- 238000009434 installation Methods 0.000 description 4
- 230000010354 integration Effects 0.000 description 4
- 230000032683 aging Effects 0.000 description 3
- 239000000567 combustion gas Substances 0.000 description 3
- 239000000203 mixture Substances 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 230000033001 locomotion Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000004806 packaging method and process Methods 0.000 description 2
- 235000001270 Allium sibiricum Nutrition 0.000 description 1
- 239000012080 ambient air Substances 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 239000003990 capacitor Substances 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 238000013021 overheating Methods 0.000 description 1
- 230000001141 propulsive effect Effects 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 1
- 239000002699 waste material Substances 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
- F02K5/00—Plants including an engine, other than a gas turbine, driving a compressor or a ducted fan
-
- 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
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
-
- 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
- F02C7/32—Arrangement, mounting, or driving, of auxiliaries
-
- 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
- F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
-
- 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)
- Supercharger (AREA)
Abstract
L'invention concerne un moteur à cycle combiné (10) qui comprend un compresseur (19) et une section turbine (16 & 20) et au moins un dispositif (12) de développement à cycle coopérant avec la section turbine (16 & 20) pour produire de la puissance. Ledit dispositif (12) possède un arbre de sortie (26) formant un angle avec l'arbre de la turbine (28). Le train d'engrenages (34) en angle permet de connecter l'arbre de la turbine (28) à gaz et le dispositif (12) de développement à cycle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CA2516700A CA2516700C (fr) | 2003-02-24 | 2004-02-24 | Ensemble moteur combine compact |
Applications Claiming Priority (6)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CA2419692 | 2003-02-24 | ||
| CA2419691 | 2003-02-24 | ||
| CA2,419,692 | 2003-02-24 | ||
| CA2,419,691 | 2003-02-24 | ||
| CA2516700A CA2516700C (fr) | 2003-02-24 | 2004-02-24 | Ensemble moteur combine compact |
| PCT/CA2004/000259 WO2004074653A1 (fr) | 2003-02-24 | 2004-02-24 | Ensemble moteur combine compact |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CA2516700A1 CA2516700A1 (fr) | 2004-09-02 |
| CA2516700C true CA2516700C (fr) | 2011-11-29 |
Family
ID=35276930
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA2516700A Expired - Lifetime CA2516700C (fr) | 2003-02-24 | 2004-02-24 | Ensemble moteur combine compact |
Country Status (1)
| Country | Link |
|---|---|
| CA (1) | CA2516700C (fr) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2014195632A1 (fr) * | 2013-06-06 | 2014-12-11 | Snecma | Boîtier d'entraînement des accessoires pour un turbopropulseur |
| CN110905659A (zh) * | 2016-02-18 | 2020-03-24 | Apgn公司 | 燃气涡轮鼓风机/泵 |
-
2004
- 2004-02-24 CA CA2516700A patent/CA2516700C/fr not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| CA2516700A1 (fr) | 2004-09-02 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| EEER | Examination request | ||
| MKEX | Expiry |
Effective date: 20240226 |