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Standard fuel bladder tanks sizes range from 100-US-gallon (380 L) to 200,000-US-gallon (760,000 L) capacities and larger. Custom fuel storage bladders and cells are available, although at sizes exceeding 50,000 US gallons (190,000 L) there is an increased spill risk.
A bladder tank is a large, flexible container used to store many types of liquids. [1] When maximum capacity is reached, the bladder tank takes the form of a large pillow , hence it is also called a pillow tank .
These tanks can be either supported or unsupported. The supported tanks have a steel or aluminum frame and range in size from 600 to 5,000 US gallons (500 to 4,160 imp gal; 2,300 to 18,900 L) or larger by custom design. Portable water tanks are also unsupported such as self-supporting tanks (onion tanks), blivets and pillow or bladder tanks and ...
Bladder tanks, bag tanks or fuel cells, are reinforced rubberised bags installed in a section of aircraft structure designed to accommodate fuel. The bladder is rolled up and installed into the compartment through the fuel filler neck or access panel, and is secured by means of snap fasteners or cord and loops inside the compartment.
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English Electric Lightning [17] Conformal ventral store was used for a small or large belly fuel tank which bulges out from the underbody. Gloster Javelin fitted with dual flush-mounted belly tanks with a capacity of 1,137 liters (300 US gallons). They were known as "bosom tanks" or "Sabrinas". [18] [19] Gloster Meteor. [20] Shenyang J-6.
The diaphragm or bladder may itself exert a pressure on the water, but it is usually small and will be neglected in the following discussion. Case 1 is an empty tank at the charging pressure P c (gauge). The total volume of the tank is V t. Case 2 is a tank in use, with the air pressure at pressure P (gauge) and a water volume of V
Fuel is housed internally within both the integral wing tank and a bladder cell within the fuselage, accommodating a combined 955 L (210 U.S. gal). For greater range, a maximum of two drop tanks can be installed upon the inner hard points of the wing, each having a capacity of 323 L (71 U.S. gal). [8]
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