GB899681A - Improvements relating to the control of the ratio of the flow rates of fuel and oxidant to a combustion chamber - Google Patents
Improvements relating to the control of the ratio of the flow rates of fuel and oxidant to a combustion chamberInfo
- Publication number
- GB899681A GB899681A GB1488359A GB1488359A GB899681A GB 899681 A GB899681 A GB 899681A GB 1488359 A GB1488359 A GB 1488359A GB 1488359 A GB1488359 A GB 1488359A GB 899681 A GB899681 A GB 899681A
- Authority
- GB
- United Kingdom
- Prior art keywords
- venturi
- flow
- valve
- pipe
- meter
- 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
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/44—Feeding propellants
- F02K9/56—Control
- F02K9/58—Propellant feed valves
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D11/00—Control of flow ratio
- G05D11/006—Control of flow ratio involving a first fluid acting on the feeding of a second fluid
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Testing Of Engines (AREA)
Abstract
899,681. Rocket propulsion. BRISTOL SIDDELEY ENGINES Ltd. April 28, 1960 [May 1, 1959], No. 14883/59. Class 110 (3). [Also in Group XXIX] Apparatus for controlling the flow ratio of oxidant and of fuel to a combustion chamber, such as in a rocket motor, comprises flow pipes 3, 4 for leading oxidant and a fuel respectively to the combustion chamber, means 1, 2 in each pipe capable of producing a pressure difference in response to flow therethrough, separate pressure tappings leading from each of the flow paths at a position upstream of the means therein and at a position of reduced pressure produced by the means, a valve-actuating device 9 responsive differentially to the pressure difference for use by each of the means and a valve 7 operable by the valve-actuating device to vary the rate of flow through one of the pipes with respect to the flow through the other pipe, whereby the flow ratio can be maintained substantially constant, the valve-actuating device comprising a housing 12 defining a pair of separate compartments in which pistons 10, 11 are mounted, and a rod 8 connecting at least one of the pistons with the valve. The means 1, 2 as shown in Fig. 1, are in the form of Venturi meters, the opposite sides of the piston 10 being connected by pipes 15, 19 into the Venturi-meter 1, and opposite sides of the piston 11, being connected to the Venturi-meter 2 by a pipe 20 and a connection upstream of the latter meter. The pistons are connected by a common rod 8 which is coupled to a valve 7 located in the fuel pipe 4. In operation, if a variation in flow occurs in the oxidant pipe 3, the pressure difference thereby produced across the Venturi-meter 1 moves the piston 10 and thus adjusts the position of the valve in order to permit more or less fuel through the pipe 4. The flow through the Venturi 1 is initially set by a by-pass 5, 6; alternatively, Venturi-meter 2 may be provided with the by-pass. In a modification, the Venturi-meters, which have fixed throats, may be provided with a spring- loaded throttling device which produces a varying flow characteristic through the Venturi.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1488359A GB899681A (en) | 1959-05-01 | 1959-05-01 | Improvements relating to the control of the ratio of the flow rates of fuel and oxidant to a combustion chamber |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1488359A GB899681A (en) | 1959-05-01 | 1959-05-01 | Improvements relating to the control of the ratio of the flow rates of fuel and oxidant to a combustion chamber |
Publications (1)
Publication Number | Publication Date |
---|---|
GB899681A true GB899681A (en) | 1962-06-27 |
Family
ID=10049215
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1488359A Expired GB899681A (en) | 1959-05-01 | 1959-05-01 | Improvements relating to the control of the ratio of the flow rates of fuel and oxidant to a combustion chamber |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB899681A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1256482B (en) * | 1963-08-16 | 1967-12-14 | Bristol Siddeley Engines Ltd | Control valve for a rocket engine |
US3690340A (en) * | 1970-03-05 | 1972-09-12 | Anatole J Sipin | Fluid proportioning system |
GB2128728A (en) * | 1982-10-19 | 1984-05-02 | Stordy Combustion Eng | Burner control |
GB2225091A (en) * | 1988-11-18 | 1990-05-23 | Pro Aqua Systems Ltd | Flow modulator system for pressure reducing valves |
-
1959
- 1959-05-01 GB GB1488359A patent/GB899681A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1256482B (en) * | 1963-08-16 | 1967-12-14 | Bristol Siddeley Engines Ltd | Control valve for a rocket engine |
US3690340A (en) * | 1970-03-05 | 1972-09-12 | Anatole J Sipin | Fluid proportioning system |
GB2128728A (en) * | 1982-10-19 | 1984-05-02 | Stordy Combustion Eng | Burner control |
GB2225091A (en) * | 1988-11-18 | 1990-05-23 | Pro Aqua Systems Ltd | Flow modulator system for pressure reducing valves |
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