GB873146A - A fluid proportioner - Google Patents
A fluid proportionerInfo
- Publication number
- GB873146A GB873146A GB140157A GB140157A GB873146A GB 873146 A GB873146 A GB 873146A GB 140157 A GB140157 A GB 140157A GB 140157 A GB140157 A GB 140157A GB 873146 A GB873146 A GB 873146A
- Authority
- GB
- United Kingdom
- Prior art keywords
- flow
- fuel
- wheels
- ratios
- rates
- 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
- 239000012530 fluid Substances 0.000 title abstract 4
- 239000000446 fuel Substances 0.000 abstract 3
- 239000002828 fuel tank Substances 0.000 abstract 1
- 230000002463 transducing effect Effects 0.000 abstract 1
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D11/00—Control of flow ratio
- G05D11/02—Controlling ratio of two or more flows of fluid or fluent material
- G05D11/13—Controlling ratio of two or more flows of fluid or fluent material characterised by the use of electric means
- G05D11/131—Controlling ratio of two or more flows of fluid or fluent material characterised by the use of electric means by measuring the values related to the quantity of the individual components
- G05D11/132—Controlling ratio of two or more flows of fluid or fluent material characterised by the use of electric means by measuring the values related to the quantity of the individual components by controlling the flow of the individual components
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D37/00—Arrangements in connection with fuel supply for power plant
- B64D37/02—Tanks
- B64D37/14—Filling or emptying
- B64D37/20—Emptying systems
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Control Of Non-Positive-Displacement Pumps (AREA)
- Control Of Positive-Displacement Pumps (AREA)
Abstract
873,146. Automatic fluid flow control systems. SPE CO. Ltd. Jan. 14, 1958 [Jan. 14, 1957; July 29, 1957], Nos. 1401/57 and 24007/57. Class 38 (4). In a system for maintaining rates of fluid flow in a desired ratio, electrical pulses corresponding in frequency to the rates of flow operate step by step motors coupled through adjustable speed gearing to driven members which get out of step and operate means to control fluid flow and restore the desired ratio automatically, should it deviate. In Fig. 1 fuel is pumped from each of three aircraft fuel tanks 10, 11, 12 by pumps 13 through conduits 14 having electric motor-operated control valves 15, non-return valves 16, and flow measuring units 17. The flow transducing units are of the type in which a rotor driven by the fuel flow carries a vane which periodically interrupts light falling on a photo-transistor or operates an electromagnetic device so that electrical pulses are produced having a frequency corresponding to the rate of flow. These pulses, amplified, operate step-bystep motors 20 rotating ratchet wheels 22 to positions corresponding to integrated rate of flow in each conduit 14. Ratchet wheels 22 drive further wheels 25 through variable-speed gears 24 which are set so that when the flows are in such ratios that the three tanks empty together there is no relative movement between the three wheels 25. If relative movements do occur, indicating errors in the flow ratios, reversing switches 65 are operated to run the motors of control valves 15 in the appropriate direction to correct the ratios. Ratio correction by controlling by-pass valves returning fuel to the tanks or by varying pump speeds is referred to. Counters and speed-responsive devices operated by the pulses or by ratchet wheels 22 and by a shaft 32 indicate individual and total flows and rates of flow respectively. An emergency pump may be started to replace a main pump by a switch responsive to failure of pressure in one of the conduits.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB140157A GB873146A (en) | 1957-01-14 | 1957-01-14 | A fluid proportioner |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB140157A GB873146A (en) | 1957-01-14 | 1957-01-14 | A fluid proportioner |
Publications (1)
Publication Number | Publication Date |
---|---|
GB873146A true GB873146A (en) | 1961-07-19 |
Family
ID=9721360
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB140157A Expired GB873146A (en) | 1957-01-14 | 1957-01-14 | A fluid proportioner |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB873146A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3272217A (en) * | 1962-03-16 | 1966-09-13 | Sun Oil Co | Systems for proportioning fluids |
EP1731810B2 (en) † | 2005-06-10 | 2020-10-14 | The Boeing Company | Shrouded valve apparatus and related methods |
CN114746751A (en) * | 2019-11-27 | 2022-07-12 | 沃特世科技公司 | Passive damping gradient proportional valve |
-
1957
- 1957-01-14 GB GB140157A patent/GB873146A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3272217A (en) * | 1962-03-16 | 1966-09-13 | Sun Oil Co | Systems for proportioning fluids |
EP1731810B2 (en) † | 2005-06-10 | 2020-10-14 | The Boeing Company | Shrouded valve apparatus and related methods |
CN114746751A (en) * | 2019-11-27 | 2022-07-12 | 沃特世科技公司 | Passive damping gradient proportional valve |
US11940424B2 (en) | 2019-11-27 | 2024-03-26 | Waters Technologies Corporation | Gradient proportioning valve |
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