WO2008087685A3 - Open-cycle gas turbine engine system having power and modulation sections - Google Patents
Open-cycle gas turbine engine system having power and modulation sections Download PDFInfo
- Publication number
- WO2008087685A3 WO2008087685A3 PCT/IT2008/000023 IT2008000023W WO2008087685A3 WO 2008087685 A3 WO2008087685 A3 WO 2008087685A3 IT 2008000023 W IT2008000023 W IT 2008000023W WO 2008087685 A3 WO2008087685 A3 WO 2008087685A3
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- power
- section
- modulation
- gas turbine
- open
- 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.)
- Ceased
Links
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
- F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
- F02C3/30—Adding water, steam or other fluids for influencing combustion, e.g. to obtain cleaner exhaust gases
- F02C3/305—Increasing the power, speed, torque or efficiency of a gas turbine or the thrust of a turbojet engine by injecting or adding water, steam or other fluids
-
- 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
- F02C3/36—Open cycles
-
- 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
- F02C6/006—Open cycle gas-turbine in which the working fluid is expanded to a pressure below the atmospheric pressure and then compressed to atmospheric pressure
-
- 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
- F02C6/18—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use using the waste heat of gas-turbine plants outside the plants themselves, e.g. gas-turbine power heat plants
-
- 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
- F02C6/20—Adaptations of gas-turbine plants for driving vehicles
-
- 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
- F02C7/12—Cooling of plants
- F02C7/14—Cooling of plants of fluids in the plant, e.g. lubricant or fuel
- F02C7/141—Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid
- F02C7/143—Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid before or between the compressor stages
-
- 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)
- Engine Equipment That Uses Special Cycles (AREA)
- Control Of Eletrric Generators (AREA)
Abstract
An open-cycle gas turbine system comprising a power section (5, 6, 7, 8, 9), a modulation section (1, 2, 3, 4), and a regeneration section (10, 11) for recovering heat from the exhaust gases. The turbines (6, 7) of the power section operate at a substantially constant maximum temperature, also in the regulation mode (partial load), up to the time a burner (3) of the modulation section is switched off. During the continuous modulation of the delivered power, which is mainly performed by modulating the amount of fuel injected into the burner (3), the efficiency constantly remains at high levels. The system can be sized in such a way to attain a maximum of the efficiency in the regulation mode. The system has rapid response times since the power modulation obtained through the variation of the density of the working fluid maintains unaltered the rpm value and the temperature of the power section, until reduced power values are reached.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| ITRM2007A000023 | 2007-01-18 | ||
| IT000023A ITRM20070023A1 (en) | 2007-01-18 | 2007-01-18 | SYSTEM OF GAS TURBINES OPERATING IN OPEN CIRCUIT |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| WO2008087685A2 WO2008087685A2 (en) | 2008-07-24 |
| WO2008087685A3 true WO2008087685A3 (en) | 2008-09-25 |
Family
ID=39628775
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/IT2008/000023 Ceased WO2008087685A2 (en) | 2007-01-18 | 2008-01-16 | Open-cycle gas turbine engine system having power and modulation sections |
Country Status (2)
| Country | Link |
|---|---|
| IT (1) | ITRM20070023A1 (en) |
| WO (1) | WO2008087685A2 (en) |
Families Citing this family (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2466081B (en) * | 2008-12-15 | 2010-11-17 | Etv Motors Ltd | Cooling for hybrid electric vehicle |
| FR2993926A1 (en) * | 2012-07-24 | 2014-01-31 | Vianney Rabhi | INTERNAL AND / OR EXTERNAL COMBUSTION LOW PRESSURE TURBOMOTOR |
| ITMO20130083A1 (en) * | 2013-03-29 | 2014-09-30 | Konner S R L | HYBRID AERONAUTICAL ENGINE |
| MX2017013353A (en) | 2015-04-17 | 2018-01-25 | Nostrum Energy Pte Ltd | Novel multiloop gas turbine and method of operation thereof. |
| FR3101378B1 (en) * | 2019-09-30 | 2021-10-15 | Psa Automobiles Sa | THERMODYNAMIC ELECTRIC ENERGY PRODUCTION SYSTEM INCLUDING A TURBOMACHINE AND A MACHINE IMPLEMENTING WATER VAPOR |
| FR3120251B1 (en) * | 2021-02-26 | 2025-02-28 | Psa Automobiles Sa | TURBOMACHINE DEVICE WITH GENERATOR POWER SYSTEM AND VEHICLE COMPRISING SUCH A DEVICE |
| FR3120571B1 (en) * | 2021-03-09 | 2024-03-01 | Psa Automobiles Sa | TRITHERMAL TURBOMACHINE DEVICE AND VEHICLE COMPRISING SUCH A DEVICE |
| DE102021122631A1 (en) * | 2021-09-01 | 2023-03-02 | Obrist Technologies Gmbh | Drive system for a vehicle |
| FR3141723B1 (en) * | 2022-11-07 | 2024-09-20 | Psa Automobiles Sa | MOTOR VEHICLE COMPRISING MULTIAXIAL TURBOCHARGERS COUPLED TO AN ELECTRIC GENERATOR, METHOD BASED ON SUCH A VEHICLE |
| FR3156166A1 (en) * | 2023-12-01 | 2025-06-06 | Stellantis Auto Sas | ELECTRICITY PRODUCTION DEVICE COMPRISING AN IRRegT CYCLE TURBOGENERATOR |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB492831A (en) * | 1937-05-14 | 1938-09-28 | Milo Ab | Improvements in gas turbine plants of the continuous combustion type |
| US2418911A (en) * | 1944-04-28 | 1947-04-15 | Elliott Co | Gas turbine cycle |
| US6606864B2 (en) * | 2001-02-13 | 2003-08-19 | Robin Mackay | Advanced multi pressure mode gas turbine |
| GB2398606A (en) * | 2003-02-21 | 2004-08-25 | Alstom Technology Ltd | Method and system for operating a partially closed cycle turbocharged gas turbine engine |
| US20050056021A1 (en) * | 2003-09-12 | 2005-03-17 | Mes International, Inc. | Multi-spool turbogenerator system and control method |
-
2007
- 2007-01-18 IT IT000023A patent/ITRM20070023A1/en unknown
-
2008
- 2008-01-16 WO PCT/IT2008/000023 patent/WO2008087685A2/en not_active Ceased
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB492831A (en) * | 1937-05-14 | 1938-09-28 | Milo Ab | Improvements in gas turbine plants of the continuous combustion type |
| US2418911A (en) * | 1944-04-28 | 1947-04-15 | Elliott Co | Gas turbine cycle |
| US6606864B2 (en) * | 2001-02-13 | 2003-08-19 | Robin Mackay | Advanced multi pressure mode gas turbine |
| GB2398606A (en) * | 2003-02-21 | 2004-08-25 | Alstom Technology Ltd | Method and system for operating a partially closed cycle turbocharged gas turbine engine |
| US20050056021A1 (en) * | 2003-09-12 | 2005-03-17 | Mes International, Inc. | Multi-spool turbogenerator system and control method |
Also Published As
| Publication number | Publication date |
|---|---|
| ITRM20070023A1 (en) | 2008-07-19 |
| WO2008087685A2 (en) | 2008-07-24 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| NENP | Non-entry into the national phase |
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| 122 | Ep: pct application non-entry in european phase |
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