FIELD: air and space craft.
SUBSTANCE: proposed reverser assembly of turbojet engine outer circuit contains fixed and movable housings and rotary doors hinge-connected with front fixed housing through two-link leverage. Rotary door and rear lever of leverage are provided with contact flats. Flat on rotary door is made in space open to side of outer circuit channels, and that on rear lever, on its side surface.
EFFECT: improved reliability of reverser assembly by provision of gas-dynamic locking of reverser assembly in case of failure of hydraulic system and fixing locks.
4 dwg
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