CA2516720C - Moteur rotatif turbo-combine integre a faible taux de compression volumetrique - Google Patents
Moteur rotatif turbo-combine integre a faible taux de compression volumetrique Download PDFInfo
- Publication number
- CA2516720C CA2516720C CA2516720A CA2516720A CA2516720C CA 2516720 C CA2516720 C CA 2516720C CA 2516720 A CA2516720 A CA 2516720A CA 2516720 A CA2516720 A CA 2516720A CA 2516720 C CA2516720 C CA 2516720C
- Authority
- CA
- Canada
- Prior art keywords
- engine
- section
- rotary
- turbine
- air
- 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
- 230000006835 compression Effects 0.000 title claims abstract description 37
- 238000007906 compression Methods 0.000 title claims abstract description 37
- 150000001875 compounds Chemical class 0.000 claims abstract description 40
- 239000007789 gas Substances 0.000 claims description 49
- 239000000446 fuel Substances 0.000 claims description 42
- 239000000203 mixture Substances 0.000 claims description 25
- 238000000034 method Methods 0.000 claims description 22
- 230000009467 reduction Effects 0.000 claims description 8
- 238000011144 upstream manufacturing Methods 0.000 claims description 4
- 239000003570 air Substances 0.000 description 34
- 238000002485 combustion reaction Methods 0.000 description 12
- 238000001816 cooling Methods 0.000 description 6
- 238000010586 diagram Methods 0.000 description 5
- 239000007788 liquid Substances 0.000 description 5
- 230000008901 benefit Effects 0.000 description 4
- 238000013461 design Methods 0.000 description 3
- UHZZMRAGKVHANO-UHFFFAOYSA-M chlormequat chloride Chemical compound [Cl-].C[N+](C)(C)CCCl UHZZMRAGKVHANO-UHFFFAOYSA-M 0.000 description 2
- 239000000110 cooling liquid Substances 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000035945 sensitivity Effects 0.000 description 2
- 241000543375 Sideroxylon Species 0.000 description 1
- 239000012080 ambient air Substances 0.000 description 1
- 230000005540 biological transmission Effects 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
- 238000011038 discontinuous diafiltration by volume reduction Methods 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 239000003350 kerosene Substances 0.000 description 1
- 238000012552 review Methods 0.000 description 1
- 239000007858 starting material Substances 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
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
- F02C3/08—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising at least one radial stage
-
- 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
- F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
- F02C3/045—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor having compressor and turbine passages in a single rotor-module
- F02C3/05—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor having compressor and turbine passages in a single rotor-module the compressor and the turbine being of the radial flow type
-
- 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
- F02C5/00—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
- F02C5/06—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the working fluid being generated in an internal-combustion gas generated of the positive-displacement type having essentially no mechanical power output
-
- 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
-
- 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)
- Supercharger (AREA)
Abstract
L'invention concerne un moteur combiné cyclique (10) comprenant une section de compresseur et une section de turbine (14, 18), ainsi qu'au moins un dispositif de flux non dérivé (16) fournissant une entrée d'énergie dans la section de turbine (18). La section de compresseur (14) comprime l'air selon un taux de compression PR¿gt?. Le dispositif de flux dérivé (16) comprime également l'air selon un taux de compression volumétrique R¿vc?, PR¿gt? x R¿vc? étant sélectionné, selon un mode de réalisation de l'invention, pour fournir un cycle permettant d'obtenir un moteur combiné cyclique plus compact et léger.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CA2516720A CA2516720C (fr) | 2003-02-24 | 2004-02-24 | Moteur rotatif turbo-combine integre a faible taux de compression volumetrique |
Applications Claiming Priority (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CA2419690 | 2003-02-24 | ||
| CA2,419,690 | 2003-02-24 | ||
| CA2516720A CA2516720C (fr) | 2003-02-24 | 2004-02-24 | Moteur rotatif turbo-combine integre a faible taux de compression volumetrique |
| PCT/CA2004/000258 WO2004074655A1 (fr) | 2003-02-24 | 2004-02-24 | Moteur rotatif turbo-combine integre a faible taux de compression volumetrique |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CA2516720A1 CA2516720A1 (fr) | 2004-09-02 |
| CA2516720C true CA2516720C (fr) | 2012-04-24 |
Family
ID=35276932
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA2516720A Expired - Lifetime CA2516720C (fr) | 2003-02-24 | 2004-02-24 | Moteur rotatif turbo-combine integre a faible taux de compression volumetrique |
Country Status (1)
| Country | Link |
|---|---|
| CA (1) | CA2516720C (fr) |
Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10107195B2 (en) | 2012-07-20 | 2018-10-23 | Pratt & Whitney Canada Corp. | Compound cycle engine |
| US9926843B2 (en) | 2012-07-20 | 2018-03-27 | Pratt & Whitney Canada Corp. | Compound cycle engine |
| US9512721B2 (en) | 2012-07-20 | 2016-12-06 | Pratt & Whitney Canada Corp. | Compound cycle engine |
| US9194232B2 (en) | 2012-07-20 | 2015-11-24 | Pratt & Whitney Canada Corp. | Compound cycle engine |
| CA2933113C (fr) * | 2015-06-16 | 2023-09-26 | Pratt & Whitney Canada Corp. | Moteur a cycle combine |
| CA2933112C (fr) * | 2015-06-16 | 2023-09-26 | Pratt & Whitney Canada Corp. | Moteur a cycle combine |
-
2004
- 2004-02-24 CA CA2516720A patent/CA2516720C/fr not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| CA2516720A1 (fr) | 2004-09-02 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| EEER | Examination request | ||
| MKEX | Expiry |
Effective date: 20240226 |