MA35944B1 - Brayton cycle with environmental refrigeration close to the critical isotherm - Google Patents
Brayton cycle with environmental refrigeration close to the critical isothermInfo
- Publication number
- MA35944B1 MA35944B1 MA37373A MA37373A MA35944B1 MA 35944 B1 MA35944 B1 MA 35944B1 MA 37373 A MA37373 A MA 37373A MA 37373 A MA37373 A MA 37373A MA 35944 B1 MA35944 B1 MA 35944B1
- Authority
- MA
- Morocco
- Prior art keywords
- critical
- isobar
- close
- pressure
- brayton cycle
- Prior art date
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
- F02C1/00—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid
- F02C1/04—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid the working fluid being heated indirectly
- F02C1/10—Closed 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
- F02C1/00—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid
- F02C1/04—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid the working fluid being heated indirectly
- F02C1/10—Closed cycles
- F02C1/105—Closed cycles construction; details
-
- 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
- F02C7/08—Heating air supply before combustion, e.g. by exhaust gases
- F02C7/10—Heating air supply before combustion, e.g. by exhaust gases by means of regenerative heat-exchangers
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)
- Hybrid Cells (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Particle Accelerators (AREA)
Abstract
Cycle régénérateur fermé, dont la température minimale du fluide de travail est à son tour proche de la température critique, mais supérieure à celle-ci, et proche de la température ambiante utilisée pour réfrigérer un foyer froid; on sélectionne la valeur de l'isobare supérieur pour qu'il coïncide avec l'isobare dit suprême, qui présente la valeur maximale moyenne de chaleur spécifique à pression constante, dans la zone péri-critique, au-dessus de l'isotherme critique, et délimitée en pression entre un cinquième et cinq fois la pression critique, en fixant l'isobare inférieur pour fournir le maximum d'un facteur dans lequel le numérateur est le travail spécifique, et le dénominateur la somme des valeurs absolues de la variation d'enthalpie spécifique de chaque étape du cycle.Regenerative cycle closed, whose minimum temperature of the working fluid is in turn close to but above the critical temperature, and close to the ambient temperature used to cool a cold hearth; the value of the upper isobar is selected to coincide with the so-called supreme isobar, which has the mean maximum value of specific heat at constant pressure, in the peri-critical zone, above the critical isotherm, and delimited in pressure between one fifth and five times the critical pressure, fixing the lower isobar to provide the maximum of a factor in which the numerator is the specific work, and the denominator the sum of the absolute values of the variation of specific enthalpy of each stage of the cycle.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ES201200343A ES2427648B2 (en) | 2012-03-30 | 2012-03-30 | Brayton cycle with environmental refrigeration close to critical isotherm |
PCT/ES2013/000071 WO2013144391A1 (en) | 2012-03-30 | 2013-03-15 | Brayton cycle with ambient cooling close to the critical isotherm |
Publications (1)
Publication Number | Publication Date |
---|---|
MA35944B1 true MA35944B1 (en) | 2014-12-01 |
Family
ID=49258281
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
MA37373A MA35944B1 (en) | 2012-03-30 | 2014-09-24 | Brayton cycle with environmental refrigeration close to the critical isotherm |
Country Status (4)
Country | Link |
---|---|
CL (1) | CL2014002636A1 (en) |
ES (1) | ES2427648B2 (en) |
MA (1) | MA35944B1 (en) |
WO (1) | WO2013144391A1 (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ES2652522B2 (en) * | 2017-10-30 | 2019-01-16 | Univ Madrid Politecnica | THERMODYNAMIC CYCLING PROCESS WITHOUT FLUID CONDENSATION AND WITH REGULATED LIMITATIONS ON ITS POINTS OF MINIMUM AND MAXIMUM ENTHALPIA AND DEVICE FOR ITS REALIZATION |
ES2657072A1 (en) * | 2017-12-05 | 2018-03-01 | Universidad Politécnica de Madrid | THERMODYNAMIC CYCLIC PROCESS WITH TURBINE AND COMPRESSOR OF GAS, WITH CONTRIBUTION OF HEAT BY EXTERNAL SOURCE, AND DEVICE FOR ITS REALIZATION (Machine-translation by Google Translate, not legally binding) |
ES2713123B2 (en) * | 2019-02-19 | 2019-11-06 | Univ Madrid Politecnica | THERMAL SYSTEM WITH COMPRESSOR AND GAS EXPANSION TURBINE IN CLOSED CIRCUIT, WITH HEAT CONTRIBUTION FROM OUTDOOR SOURCE, AND INTERNAL RECOVERY OF HEAT AND MECHANICAL ENERGY, FOR GENERATION OF ELECTRICITY AND PROCEDURE |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS51143114A (en) * | 1975-06-04 | 1976-12-09 | Hitachi Ltd | Shaft sealing device of turbo machines |
US6666027B1 (en) * | 2002-07-15 | 2003-12-23 | General Electric Company | Turbine power generation systems and methods using off-gas fuels |
JP4179496B2 (en) * | 2002-10-08 | 2008-11-12 | 川崎重工業株式会社 | Atmospheric pressure combustion turbine system |
DE102009038322A1 (en) * | 2009-08-21 | 2011-02-24 | Krones Ag | Method and apparatus for converting thermal energy from biomass to mechanical work |
-
2012
- 2012-03-30 ES ES201200343A patent/ES2427648B2/en active Active
-
2013
- 2013-03-15 WO PCT/ES2013/000071 patent/WO2013144391A1/en active Application Filing
-
2014
- 2014-09-24 MA MA37373A patent/MA35944B1/en unknown
- 2014-09-30 CL CL2014002636A patent/CL2014002636A1/en unknown
Also Published As
Publication number | Publication date |
---|---|
ES2427648B2 (en) | 2014-04-01 |
WO2013144391A1 (en) | 2013-10-03 |
CL2014002636A1 (en) | 2015-01-30 |
ES2427648A1 (en) | 2013-10-31 |
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