FIELD: flight vehicles, fuselages.
SUBSTANCE: the door control mechanism has two control posts and two lines connected to the door control cylinder. The door control mechanism has also a pneumatic distributor with three chambers in its body. The first of them is connected to the high-pressure regulator and has connections closed by valves to the two other chambers, each of them is connected to the line and has a hollow spring-loaded rod with two holes, one of which is located inside with the control posts, a deflection of any of them results in closing of the second hole of the rod and opening of the mentioned valve by the rod. The bell-cranks and two platforms are so installed that a deflection of any bell-crank results in a deflection of one of the platforms and displacement of the rod. For fixation of the bell-cranks in the extreme position provision is made for a spring-loaded lever, whose termination and one of the edges of each bell-crank are made for their engagement. For control of the flight vehicle canopy provision is made for a cylinder connected to the canopy sealing tube and acting on the lever.
EFFECT: provided opening and closing of the door from two posts without interlocking of any post and without use of electric-fed elements.
4 cl, 1 dwg
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Authors
Dates
2004-11-27—Published
2003-06-10—Filed