GB617911A - Improvements relating to apparatus for controlling the distribution of fuel in aircraft - Google Patents
Improvements relating to apparatus for controlling the distribution of fuel in aircraftInfo
- Publication number
- GB617911A GB617911A GB1477846A GB1477846A GB617911A GB 617911 A GB617911 A GB 617911A GB 1477846 A GB1477846 A GB 1477846A GB 1477846 A GB1477846 A GB 1477846A GB 617911 A GB617911 A GB 617911A
- Authority
- GB
- United Kingdom
- Prior art keywords
- tanks
- tank
- volume
- fuel
- ratio
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D37/00—Arrangements in connection with fuel supply for power plant
- B64D37/02—Tanks
- B64D37/06—Constructional adaptations thereof
- B64D37/08—Internal partitioning
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Control Of Non-Electrical Variables (AREA)
- Control Of Positive-Displacement Pumps (AREA)
Abstract
617,911. Automatic control systems. SMITH, S. J. May 16, 1946, No. 14778. [Class 38 (iv)] A system for controlling the volume of liquid in each of two tanks, particularly the distribution of fuel in the tanks of an aircraft, comprises a condenser, whose capacity is proportional to the volume of liquid in the tank, situated inside each tank, and means responsive to the ratio of these capacities for controlling means for varying the volume of liquid in the tanks in such a way as to maintain the ratio of these volumes at a desired value. As shown, the tanks A and B have condensers 1a, 1b respectively, both of these, together with reference condensers 5a, 5b, being energized from a common A.C. supply 8. The measuring system employed is the same for each tank and is described in Specification 560,872, [Group XXXVI]. The condenser currents are passed through the primary windings of transformers 3a, 6a and 3b, 6b, the secondaries of which feed rectifiers 4a, 7a and 4b, 7b, the output being applied to ratiometer instruments 2a, 2b, which are calibrated to indicate the volume of fuel in each tank. The secondary windings of the transformers are connected to the grids 9a, 9b of a twin diode amplifying valve 10, the anodes of which feed the grids of push-pull connected rectifying valves 14a, 14b, feeding the two opposing field windings 15 of a control motor 16. If the capacities of the tank condensers are -not in the correct ratio, the field balance is disturbed and the control motor, the armature of which is continuously energized, rotates and operates a slide 19 on a potential divider 20 which governs the relative speeds of a pair of motors 21a, 21b. These motors drive pumps 24a, 24b, withdrawing fuel from the tanks A, B, respectively and restore the desired volume ratio. The arrangement is made self-balancing by connecting the control motor to a slider 22 on a further potential divider which alters the screen grid potential of valves 14a, 14b, in such a sense as to offset the changes due to the valve 10. An over-riding manual control acting on the valve circuits may be provided.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1477846A GB617911A (en) | 1946-05-16 | 1946-05-16 | Improvements relating to apparatus for controlling the distribution of fuel in aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1477846A GB617911A (en) | 1946-05-16 | 1946-05-16 | Improvements relating to apparatus for controlling the distribution of fuel in aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB617911A true GB617911A (en) | 1949-02-14 |
Family
ID=10047316
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1477846A Expired GB617911A (en) | 1946-05-16 | 1946-05-16 | Improvements relating to apparatus for controlling the distribution of fuel in aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB617911A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3159076A (en) * | 1958-12-20 | 1964-12-01 | Meissner J | Process and device for the filling of shells with an explosive agent containing phosphorus |
US3217368A (en) * | 1961-08-22 | 1965-11-16 | Alusuisse | Metal flow regulation |
-
1946
- 1946-05-16 GB GB1477846A patent/GB617911A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3159076A (en) * | 1958-12-20 | 1964-12-01 | Meissner J | Process and device for the filling of shells with an explosive agent containing phosphorus |
US3217368A (en) * | 1961-08-22 | 1965-11-16 | Alusuisse | Metal flow regulation |
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