GB855469A - Gas turbine engine afterburner - Google Patents
Gas turbine engine afterburnerInfo
- Publication number
- GB855469A GB855469A GB12102/59A GB1210259A GB855469A GB 855469 A GB855469 A GB 855469A GB 12102/59 A GB12102/59 A GB 12102/59A GB 1210259 A GB1210259 A GB 1210259A GB 855469 A GB855469 A GB 855469A
- Authority
- GB
- United Kingdom
- Prior art keywords
- sleeves
- fuel
- gas turbine
- turbine engine
- april
- 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
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
-
- 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
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/26—Control of fuel supply
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)
Abstract
855,469. Supplying liquid fuel to burners. GENERAL MOTORS CORPORATION. April 9, 1959 [April 9, 1958], No. 12102/59. Class 75(1). Fuel is delivered to a gas turbine reheater by perforated radial bars 23 with internal valve sleeves 46. The sleeves have slots 50 of varying length so that when the sleeves are rotated both the rate of flow and the distribution of fuel in the combustion chamber change. Fuel is fed from a manifold 24 to the interiors of the sleeves ; drains 54 are provided to remove fuel leaking through the valve bearings. The sleeves are rotated together by linkages on a ring 72.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US855469XA | 1958-04-09 | 1958-04-09 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB855469A true GB855469A (en) | 1960-11-30 |
Family
ID=22192332
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB12102/59A Expired GB855469A (en) | 1958-04-09 | 1959-04-09 | Gas turbine engine afterburner |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB855469A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2172392A (en) * | 1985-03-14 | 1986-09-17 | Kuesters Eduard | Gas burner |
FR2629136A1 (en) * | 1985-09-17 | 1989-09-29 | Aerospatiale | STATOREACTOR PROVIDED WITH A PLURALITY OF CARBIDE AND MISSILE AIR SUPPLY SLEEVES PROVIDED WITH SUCH A STATOREACTOR |
-
1959
- 1959-04-09 GB GB12102/59A patent/GB855469A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2172392A (en) * | 1985-03-14 | 1986-09-17 | Kuesters Eduard | Gas burner |
US4774747A (en) * | 1985-03-14 | 1988-10-04 | Eduard Kusters | Gas burner for the interior heating of hollow rolls |
FR2629136A1 (en) * | 1985-09-17 | 1989-09-29 | Aerospatiale | STATOREACTOR PROVIDED WITH A PLURALITY OF CARBIDE AND MISSILE AIR SUPPLY SLEEVES PROVIDED WITH SUCH A STATOREACTOR |
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