Length adjustable strut link with low aerodynamic drag

Power plants – Combustion products used as motive fluid – Combined with regulation of power output feature

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Details

60262, 60263, 248554, 244 54, F02C 720, B64D 2716

Patent

active

045719365

ABSTRACT:
A low aerodynamic drag structural link suitable for use within the housing of a turbofan jet engine; the link includes length adjustment capability, pivotal end mounting provision, maintained airstream orientation capability, low mass and jam nut length and orientation locking. Several variations in link construction including a single ball and socket arrangement, varying link cross-section along its longitudinal length and the use of fairing nose and tail inserts are disclosed.

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