Variable stiffness positioning link for a gearbox
AssigneeUnited Technologies Corporation
InventorKeven G. Van Duyn
Life of this patent
Estimating the term…
Loading patent…
AssigneeUnited Technologies Corporation
InventorKeven G. Van Duyn
Estimating the term…
A gearbox mounting arrangement for a gas turbine engine includes a plurality of variable stiffness positioning links that attach the gearbox housing to the engine case. The links include a first portion that is connected to the engine case, a second portion connected to the gearbox and the first and second portion releasably connected by an isolation mechanism having a lower stiffness than the first and second portions. During a high rotor imbalance condition such as a fan blade loss condition, the links yield to a lower stiffness level than during normal operation as the isolation mechanism becomes operational in response to the application of high axial loads and the first and second portions partially disengage. The partial disengagement of the portions of the links of the present invention results in partially isolating the gearbox from the deflections experienced by the engine case. Thus, only a percentage of engine case imbalance loads are transmitted through the links to the gearbox. Alternate embodiments for the isolation mechanism are disclosed.
A variable stiffness positioning link for securing a gearbox to a gas turbine engine case, said link characterized by having a first spring rate in a first direction during normal operation, said link comprising:
Dependencies are inferred from the claim text.