GB657083A - Improvements in fuel supply systems for aircraft - Google Patents
Improvements in fuel supply systems for aircraftInfo
- Publication number
- GB657083A GB657083A GB1502/49A GB150249A GB657083A GB 657083 A GB657083 A GB 657083A GB 1502/49 A GB1502/49 A GB 1502/49A GB 150249 A GB150249 A GB 150249A GB 657083 A GB657083 A GB 657083A
- Authority
- GB
- United Kingdom
- Prior art keywords
- valve
- fuel
- aircraft
- casing
- tanks
- 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
- 239000000446 fuel Substances 0.000 title abstract 6
- 239000002828 fuel tank Substances 0.000 abstract 2
Classifications
-
- 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
- B64D37/04—Arrangement thereof in or on aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Multiple-Way Valves (AREA)
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
Abstract
657,083. Emptying tanks. SAUNDERS-ROE, Ltd., and WHITTING, L. K. Jan. 19, 1949, No. 1502. [Class 21] [Also in Group XXIX] A gravity-operated valve 15 for emptying the wing fuel tanks of an aircraft comprises a tubular casing 23 having two fuel inlets and a fuel outlet 31, a valve member with valve heads 28 thereon being slidable between alternative end positions when the casing 23 is tilted due to change of attitude of the aircraft so that the inlet at the higher level is sealed to prevent the entry of air whilst the lower inlet is open to allow the passage of fuel from the tank. As shown, the valve 15 is supported on the base of a wing tank 12 in the fore and aft direction. The tubular casing 23 has end casings 24 fitted with filters 25. The valve member comprises an inner tube 26 containing loose balls 32 and connected to bars 27 on each of which a valve head 28 is universally mounted. The valve member is guided in the casing 23 by pairs of rollers 29 arranged in slots 30 and having their axes at right-angles to one another. The outlet to the fuel pump is through an aperture 31. The Specification shows the application of the valve to the inboard and outboard fuel tanks which are connected to the fuel pump through a valve as described in Specification 657,082.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1502/49A GB657083A (en) | 1949-01-19 | 1949-01-19 | Improvements in fuel supply systems for aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1502/49A GB657083A (en) | 1949-01-19 | 1949-01-19 | Improvements in fuel supply systems for aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB657083A true GB657083A (en) | 1951-09-12 |
Family
ID=9723106
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1502/49A Expired GB657083A (en) | 1949-01-19 | 1949-01-19 | Improvements in fuel supply systems for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB657083A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3275061A (en) * | 1964-01-02 | 1966-09-27 | Boeing Co | Fuel feeding systems |
-
1949
- 1949-01-19 GB GB1502/49A patent/GB657083A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3275061A (en) * | 1964-01-02 | 1966-09-27 | Boeing Co | Fuel feeding systems |
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