FIELD: aviation.
SUBSTANCE: invention relates to a device for suspending a gas turbine engine of an aircraft. Ball joint device (10) for suspension of a gas turbine engine to a pylon or suspension of a device on the body of a gas turbine engine comprises first member (12) one end of which carries ball head (14), second member (18) having lugs (16, 17), pin (30) extending through the opening (28) of the ball head. Ends of pin (30) pass through openings (20, 22) of the lugs. Lugs comprise means for axial retention of the pin, including cover (52). Device further comprises elastic member (62) that is supported by the cover, support member (40) through which the pin extends and which is axially supported on ball head (14).
EFFECT: invention increases the reliability of the suspension device.
13 cl, 7 dwg
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