GB822645A - Improvements in or relating to devices for regulating the fuel flow delivered to supersonic ram jets - Google Patents
Improvements in or relating to devices for regulating the fuel flow delivered to supersonic ram jetsInfo
- Publication number
- GB822645A GB822645A GB30180/56A GB3018056A GB822645A GB 822645 A GB822645 A GB 822645A GB 30180/56 A GB30180/56 A GB 30180/56A GB 3018056 A GB3018056 A GB 3018056A GB 822645 A GB822645 A GB 822645A
- Authority
- GB
- United Kingdom
- Prior art keywords
- fuel
- supply
- missile
- aircraft
- oct
- 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
- F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
- F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
-
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/60—Steering arrangements
- F42B10/66—Steering by varying intensity or direction of thrust
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
- Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
Abstract
822,645. Jet propulsion plant. SUD-AVIATION SOC. NATIONALE DE CONSTRUCTIONS AERONAUTIQUES. Oct. 3, 1956 [Oct. 12, 1955], No. 30180/56. Class 110 (3). [Also in Groups XII and XXXV] In Fig. 1 the supply to a pilot fuel injection manifold 60 and main fuel injection manifolds 61, 62 of an aircraft or missile ram jet engine 1 is regulated by a rotary sleeve valve 9 driven by an electric servomotor 91 under the control (see Group XXXV) of Mach meters 14 and 17 responsive to internal and external airflow respectively. The aircraft or missile is launched by auxiliary means and the fuel supply is initiated soon after launching by raising fuel pressure to burst a diaphragm (not shown). Fuel is then supplied to manifolds 60, 61 and somewhat later to manifold 62. Regulation of by-pass fuel instead of the main fuel supply is referred to. Specification 810,843, [Group XII], is referred to.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR822645X | 1955-10-12 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB822645A true GB822645A (en) | 1959-10-28 |
Family
ID=9281006
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB30180/56A Expired GB822645A (en) | 1955-10-12 | 1956-10-03 | Improvements in or relating to devices for regulating the fuel flow delivered to supersonic ram jets |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB822645A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3067577A (en) * | 1960-01-25 | 1962-12-11 | North American Aviation Inc | Method and control system for sensing temperatured differentials of flowing gases |
-
1956
- 1956-10-03 GB GB30180/56A patent/GB822645A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3067577A (en) * | 1960-01-25 | 1962-12-11 | North American Aviation Inc | Method and control system for sensing temperatured differentials of flowing gases |
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