Gear drive for gas turbine engine
AssigneeGeneral Motors Corporation
InventorDouglas A. Wagner
Life of this patent
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AssigneeGeneral Motors Corporation
InventorDouglas A. Wagner
Estimating the term…
A drive system for a multiple gas turbine engine system includes power output shafts from first and second gas turbine engines, each power shaft connected to drive a load and each engine including a load sharing cross-over shaft for power transfer from one of the engines to the other engine; a right angle gear box assembly connects each of the power output shafts to the cross-over shaft and each of the right angle gear box assemblies includes first and second load sharing gear paths including tooth geometry in an input bevel gear configured to produce a thrust reversal so that for normal direction torque transfer the input bevel gear thrust is in a direction to load mesh points in both gear paths and for a reversal of torque direction from input to output gears the input gear thrust is reversed so that the input gear will be directed into a tighter mesh to take out normal backlash in the system so that reverse meshed torque paths will be maintained in each of the first and second gear paths to maintain a sharing of torque in both forward and reverse directions of drive within the gear box assembly thereby to reduce weight and size of gear components of aircraft or other lightweight drive systems with reverse driving modes.
In a multiple engine drive system having first and second engines with an output shaft connected to drive a load and including a load sharing cross-over drive between each of the engine output shafts to maintain power transfer to each of the loads when one of the engines is disconnected from the system, the improvement comprising:
A multiple gas turbine engine drive system having first and second core engines with a power turbine output shaft connected to drive a fan and including a load sharing cross-over drive between each of the engine output shafts to maintain power transfer to each of the fans when one of the engines is disconnected from the system, an overrunning clutch assembly which responds to a negative torque produced by a freewheeling fan,
Dependencies are inferred from the claim text.