FIELD: gas turbine engines of aircrafts.
SUBSTANCE: traction rod (40) with adjustable length for aircraft gas turbine engine has a common elongated shape and comprises two opposite longitudinal ends (42,50) for attachment to connected elements. First (42) of these longitudinal ends is connected to the first threaded axis (44) screwed into the first tubular section (46) of adjusting bushing (48). Second (50) of these longitudinal ends is connected to the second threaded axis (52) screwed into the second tubular section (54) of the adjusting bushing and additionally containing cavity (56), in which at least part of first axis can move by sliding.
EFFECT: higher engine thrust length variation range.
10 cl, 8 dwg
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