GB627896A - Improvements in or relating to gas turbine plants - Google Patents
Improvements in or relating to gas turbine plantsInfo
- Publication number
- GB627896A GB627896A GB967147A GB967147A GB627896A GB 627896 A GB627896 A GB 627896A GB 967147 A GB967147 A GB 967147A GB 967147 A GB967147 A GB 967147A GB 627896 A GB627896 A GB 627896A
- Authority
- GB
- United Kingdom
- Prior art keywords
- air
- exchanger
- heat
- tubes
- exchangers
- 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
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
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Treating Waste Gases (AREA)
Abstract
627,896. Heating and cooling gases. HEAT EXCHANGERS, Ltd., and TOOGOOD, G. D. April 11, 1947, No. 9671. [Class 64(iii)] [Also in Groups XXVI and XXVIII] A gas-cleaning heat exchanger 14 is placed between the combustion chamber 5 and the gas turbine 1, and the combustion gases flow around the tubes of the exchanger giving up heat to a stream of air in the tubes. The temperature, pressure or rate of flow of the air is regulated to maintain constant the temperature of the gases reaching the turbine. The air passes through a second heat-exchanger 15 where it gives up its heat to the air flowing in the pipe 9 to the combustion chamber. The air passing through the exchangers 14, 15 is circulated in a closed circuit by a pump 18 and the pressure in that circuit is variable by means of a bleed 21 to the compressor inlet 7 and a bleed 19 from the compressor delivery 8. In an alternative form, the air passing through the exchangers 14, 15 is a part of the compressor delivery and is finally passed to the combustion chamber 5. The air may be passed through a cooler before the exchanger 14. The bundles of tubes in the exchanger 14 are arranged to act as interceptors of ash and other matter carried by the combustion gases and may be removed for cleaning. As shown in Fig. 3, two exchangers 14, 114 are arranged in parallel and one may be in use whilst the tubes of the other are being cleaned.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB967147A GB627896A (en) | 1947-04-11 | 1947-04-11 | Improvements in or relating to gas turbine plants |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB967147A GB627896A (en) | 1947-04-11 | 1947-04-11 | Improvements in or relating to gas turbine plants |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB627896A true GB627896A (en) | 1949-08-18 |
Family
ID=9876502
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB967147A Expired GB627896A (en) | 1947-04-11 | 1947-04-11 | Improvements in or relating to gas turbine plants |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB627896A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE930356C (en) * | 1952-10-07 | 1955-07-14 | Max Adolf Dipl-Ing Mueller | Process for the operation of gas turbine plants |
| US2743163A (en) * | 1952-02-18 | 1956-04-24 | Ryan Aeronautical Co | Inert gas generator |
| FR2552163A1 (en) * | 1983-09-21 | 1985-03-22 | Onera (Off Nat Aerospatiale) | Improvements made to gas turbine installations in which the air coming from the compressor is reheated |
-
1947
- 1947-04-11 GB GB967147A patent/GB627896A/en not_active Expired
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2743163A (en) * | 1952-02-18 | 1956-04-24 | Ryan Aeronautical Co | Inert gas generator |
| DE930356C (en) * | 1952-10-07 | 1955-07-14 | Max Adolf Dipl-Ing Mueller | Process for the operation of gas turbine plants |
| FR2552163A1 (en) * | 1983-09-21 | 1985-03-22 | Onera (Off Nat Aerospatiale) | Improvements made to gas turbine installations in which the air coming from the compressor is reheated |
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