FIELD: transport.
SUBSTANCE: invention relates to aircraft fuel systems. Fuel tank valve consists of the body with channel to communicate fuel tank with atmosphere, lower and upper shut-off members arranged coaxially and in succession. Every said shut-off member consists of pressure bush and shut-off element to be fitted on appropriate body seat and coupled with pressure bush to provided clearance in lengthwise and crosswise directions. Pressure bush top parts have wrench seats. Pressure bush of lower shut-off member is screwed to the body, while that of upper shut-off member is screwed to detachable plug bayonet-jointed to the body. Lower part of shut-off member has multi-face seat corresponding to that for aforesaid wrench.
EFFECT: higher valve tightness.
3 cl, 2 dwg
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Authors
Dates
2010-03-27—Published
2008-12-11—Filed