GB268861A - Improvements in systems of gas turbine aggregates - Google Patents
Improvements in systems of gas turbine aggregatesInfo
- Publication number
- GB268861A GB268861A GB296/26A GB29626A GB268861A GB 268861 A GB268861 A GB 268861A GB 296/26 A GB296/26 A GB 296/26A GB 29626 A GB29626 A GB 29626A GB 268861 A GB268861 A GB 268861A
- Authority
- GB
- United Kingdom
- Prior art keywords
- turbine
- gas turbine
- turbo
- systems
- working
- 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
Links
- 239000007789 gas Substances 0.000 abstract 4
- 238000002485 combustion reaction Methods 0.000 abstract 2
- 239000012530 fluid Substances 0.000 abstract 2
- 239000007788 liquid Substances 0.000 abstract 2
- 239000007921 spray Substances 0.000 abstract 2
- 238000001816 cooling Methods 0.000 abstract 1
- 239000000446 fuel Substances 0.000 abstract 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
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
- F02C6/003—Gas-turbine plants with heaters between turbine stages
-
- 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
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/211—Heat transfer, e.g. cooling by intercooling, e.g. during a compression cycle
-
- 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)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
NO1766886X | 1923-12-13 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB268861A true GB268861A (en) | 1927-04-05 |
Family
ID=19910422
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB296/26A Expired GB268861A (en) | 1923-12-13 | 1926-01-05 | Improvements in systems of gas turbine aggregates |
Country Status (7)
Country | Link |
---|---|
US (1) | US1766886A (xx) |
BE (1) | BE331656A (xx) |
CH (1) | CH120074A (xx) |
DE (1) | DE529745C (xx) |
FR (1) | FR609387A (xx) |
GB (1) | GB268861A (xx) |
NL (1) | NL19660C (xx) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2428830A (en) * | 1942-04-18 | 1947-10-14 | Turbo Engineering Corp | Regulation of combustion gas turbines arranged in series |
US2608822A (en) * | 1944-10-07 | 1952-09-02 | Turbolectric Corp | Method of operation and regulation of thermal power plants |
US2526409A (en) * | 1945-01-09 | 1950-10-17 | Lockheed Aircraft Corp | Turbo-propeller type power plant having radial flow exhaust turbine means |
US5347806A (en) * | 1993-04-23 | 1994-09-20 | Cascaded Advanced Turbine Limited Partnership | Cascaded advanced high efficiency multi-shaft reheat turbine with intercooling and recuperation |
-
0
- NL NL19660D patent/NL19660C/xx active
- BE BE331656D patent/BE331656A/xx unknown
- DE DEE31642D patent/DE529745C/de not_active Expired
-
1924
- 1924-12-02 US US753530A patent/US1766886A/en not_active Expired - Lifetime
-
1926
- 1926-01-05 GB GB296/26A patent/GB268861A/en not_active Expired
- 1926-01-05 CH CH120074D patent/CH120074A/de unknown
- 1926-01-13 FR FR609387D patent/FR609387A/fr not_active Expired
Also Published As
Publication number | Publication date |
---|---|
FR609387A (fr) | 1926-08-13 |
NL19660C (xx) | |
DE529745C (de) | 1931-07-16 |
CH120074A (de) | 1927-05-02 |
BE331656A (xx) | |
US1766886A (en) | 1930-06-24 |
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