GB924330A - Method of relighting in combustion chambers - Google Patents
Method of relighting in combustion chambersInfo
- Publication number
- GB924330A GB924330A GB933654A GB933654A GB924330A GB 924330 A GB924330 A GB 924330A GB 933654 A GB933654 A GB 933654A GB 933654 A GB933654 A GB 933654A GB 924330 A GB924330 A GB 924330A
- Authority
- GB
- United Kingdom
- Prior art keywords
- oxygen
- combustion chamber
- supply
- nozzle
- drillings
- 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
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Oxygen, Ozone, And Oxides In General (AREA)
Abstract
924,330. Generating combustion products under pressure. MINISTER OF SUPPLY. March 22, 1955 [March 30, 1954], No. 9336/54. Class 51 (1). [Also in Group XXVI] In the combustion chamber of an aircraft gas turbine or ram jet engine, the fuel injector is adapted to direct a supply of oxygen into the combustion chamber. As shown, Fig. 1, the flame tube 2 is supported inside the combustion chamber 1 by the arms 3b and 3c. The nozzle 4 is supplied with fuel through 3b and oxygen through 3c. The nozzle body 11 has a vortex chamber 11a with tangential inlets connected by drillings to 3b. Oxygen is led through drillings and slots 14, 15, 16 to the annular passage 17. Air from the main supply to the flame tube passes along the apertures 13 into 17 and is deflected across the face of the nozzle by the casing 12 tending to reduce the deposition of unburnt carbon.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB933654A GB924330A (en) | 1954-03-30 | 1954-03-30 | Method of relighting in combustion chambers |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB933654A GB924330A (en) | 1954-03-30 | 1954-03-30 | Method of relighting in combustion chambers |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB924330A true GB924330A (en) | 1963-04-24 |
Family
ID=9869997
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB933654A Expired GB924330A (en) | 1954-03-30 | 1954-03-30 | Method of relighting in combustion chambers |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB924330A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20160369700A1 (en) * | 2013-07-01 | 2016-12-22 | United Technologies Corporation | Enhanced apu operability |
-
1954
- 1954-03-30 GB GB933654A patent/GB924330A/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20160369700A1 (en) * | 2013-07-01 | 2016-12-22 | United Technologies Corporation | Enhanced apu operability |
| US10400676B2 (en) * | 2013-07-01 | 2019-09-03 | United Technologies Corporation | Enhanced APU operability |
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