GB682952A - Improvements in or relating to gas turbine engine installations for vehicles - Google Patents
Improvements in or relating to gas turbine engine installations for vehiclesInfo
- Publication number
- GB682952A GB682952A GB797949A GB797949A GB682952A GB 682952 A GB682952 A GB 682952A GB 797949 A GB797949 A GB 797949A GB 797949 A GB797949 A GB 797949A GB 682952 A GB682952 A GB 682952A
- Authority
- GB
- United Kingdom
- Prior art keywords
- fuel
- valve
- burner
- supplied
- solenoid
- 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
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/54—Nozzles having means for reversing jet thrust
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/54—Nozzles having means for reversing jet thrust
- F02K1/56—Reversing jet main flow
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Output Control And Ontrol Of Special Type Engine (AREA)
Abstract
682,952. Liquid-fuel burners. BRISTOL AEROPLANE CO., Ltd. March 16, 1950 [March 23, 1949], No. 7979/49. Classes 75(i) and 75(iii) [Also in Groups XXVI and XXXIII] Air is tapped off from the compressor 6 of a gas turbine engine and supplied to a braking thrust producer 12 which comprises a combustion chamber 13 having a burner 14 supplied with fuel by an electrically driven pump 15. The fuel supplied to the burner 14 is ignited by a torch igniter 19 comprising an igniter plug 20 and a fuel jet controlled by a solenoid operated valve 22. The air supply through the duct 24 is controlled by a valve 25 operated by a lever 26. Movement of the lever 26 opens the valve 25 and at the same time completes the circuits of the fuel pump motor 16, ignition coil 21 and solenoid 23 so that valve 22 is opened and the fuel issuing from the jet ignited, which in turn ignites the fuel from the burner 14. The contact strips 28 associated with the coil 21 and solenoid 23 are shorter than that associated with the motor 16 so that the igniter 19 is only used for starting. The fuel pump 15 may be driven by the engine and may draw fuel from the engine fuel supply tank.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB797949A GB682952A (en) | 1949-03-23 | 1949-03-23 | Improvements in or relating to gas turbine engine installations for vehicles |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB797949A GB682952A (en) | 1949-03-23 | 1949-03-23 | Improvements in or relating to gas turbine engine installations for vehicles |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB682952A true GB682952A (en) | 1952-11-19 |
Family
ID=9843433
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB797949A Expired GB682952A (en) | 1949-03-23 | 1949-03-23 | Improvements in or relating to gas turbine engine installations for vehicles |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB682952A (en) |
-
1949
- 1949-03-23 GB GB797949A patent/GB682952A/en not_active Expired
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