GB610973A - Improvements in or relating to internal combination engines and their application - Google Patents
Improvements in or relating to internal combination engines and their applicationInfo
- Publication number
- GB610973A GB610973A GB1193846A GB1193846A GB610973A GB 610973 A GB610973 A GB 610973A GB 1193846 A GB1193846 A GB 1193846A GB 1193846 A GB1193846 A GB 1193846A GB 610973 A GB610973 A GB 610973A
- Authority
- GB
- United Kingdom
- Prior art keywords
- turbine
- combustion chamber
- compressor
- relating
- application
- 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
- 238000002485 combustion reaction Methods 0.000 abstract 5
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 abstract 2
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 abstract 1
- 229910002092 carbon dioxide Inorganic materials 0.000 abstract 1
- 239000001569 carbon dioxide Substances 0.000 abstract 1
- 229910002091 carbon monoxide Inorganic materials 0.000 abstract 1
- 230000006835 compression Effects 0.000 abstract 1
- 238000007906 compression Methods 0.000 abstract 1
- 239000000446 fuel Substances 0.000 abstract 1
- 230000001105 regulatory effect Effects 0.000 abstract 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Supercharger (AREA)
Abstract
610,973. Gas turbines. ADAMS, T. HAMILTON-. April 18, 1946, No. 11938. [Class 110 (iii)] A gas turbine plant comprises an axial flow turbine and an air compressor driven thereby, the air and fuel supplies being so regulated that carbon monoxide is formed in a first combustion chamber located between the compressor and turbine and carbon dioxide is formed in a further combustion chamber located after the turbine. The turbine and compressor may be mounted on a common shaft. Ignition is by compression in the first combustion chamber and by hot wire or sparking-plug in the second combustion chamber. The exhaust from the turbine may be used for jet propulsion, in which case water may be injected into or after the second combustion chamber. According to the Provisional Specification, the compressor is of the axial flow type. Specification 567,560, [Group XXVII], is referred to.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1193846A GB610973A (en) | 1946-04-18 | 1946-04-18 | Improvements in or relating to internal combination engines and their application |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1193846A GB610973A (en) | 1946-04-18 | 1946-04-18 | Improvements in or relating to internal combination engines and their application |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB610973A true GB610973A (en) | 1948-10-22 |
Family
ID=9995403
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1193846A Expired GB610973A (en) | 1946-04-18 | 1946-04-18 | Improvements in or relating to internal combination engines and their application |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB610973A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE953929C (en) * | 1952-07-20 | 1956-12-06 | Maschf Augsburg Nuernberg Ag | Gas turbine plant with an auxiliary or afterburning chamber |
-
1946
- 1946-04-18 GB GB1193846A patent/GB610973A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE953929C (en) * | 1952-07-20 | 1956-12-06 | Maschf Augsburg Nuernberg Ag | Gas turbine plant with an auxiliary or afterburning chamber |
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