System for supporting a rotor in a conditions of accidental dynamic imbalance
AssigneeROLLS-ROYCE plc
InventorsDerek A. Roberts, John M. Treby
Life of this patent
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AssigneeROLLS-ROYCE plc
InventorsDerek A. Roberts, John M. Treby
Estimating the term…
The fan rotor (10) of a gas turbine engine is driven by a shaft (16) having a first part (16A) supported in a first radial bearing (17) for rotation about an axis (16C). The shaft (16) further has a second part (16B) secured to the rotor for transmitting torque thereto. The second part (16B) is flexible in bending to allow radial displacement of the rotor (10) relative to the bearing (17). Normally, the rotor (10) is supported against said displacement by a second radial bearing (23). If, due to damage, a given dynamic imbalance on the rotor (10) is exceeded, the resulting unbalanced force (F) transversely to the axis (16C) shears the pins (21C) of a coupling (21) provided between the rotor and the second bearing (23). This then permits the rotor (10) to move eccentrically with respect to the axis (16C) by virtue of the resilience of the shaft portion (16B) thereby cushioning the bearing (17) against the force (F).
System for supporting a rotor in conditions of dynamic imbalance;
System for supporting a rotor under conditions of dynamic imbalance comprising a shaft having a first part supported by a first radial bearing for concentric rotation relative to a support structure and a second part which is secured to the rotor for transmission of torque thereto and which is adapted to permit radial displacement of the rotor relative to the first bearing, a second radial bearing supporting the rotor against said displacement, and an overload-responsive means arranged between the rotor and the support structure in series with the second bearing and adapted to break or deform under radial forces acting on the rotor when a given dynamic imbalance thereof is exceeded, wherein the first part of the shaft is annular and contains the second bearing, the overload-responsive means is an annular structure comprising a first member secured to the rotor, a second member arranged interiorly of the annular first part of the shaft and supported thereon by the second bearing, and means connected between the first and second members and adpated to break or deform under a said radial force;
System for supporting a rotor in conditions of dynamic imbalance;
Dependencies are inferred from the claim text.