Multi-range starter-generator drive
AssigneeSundstrand Corporation
InventorMichael A. Cordner
Life of this patent
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AssigneeSundstrand Corporation
InventorMichael A. Cordner
Estimating the term…
A starter-generator drive usable in an aircraft must be of the smallest possible size and the lowest possible weight and have maximum reliability. A drive having a multi-speed transmission and a controllable hydro-viscous dissipative clutch can be interposed between an engine and a starter-generator to achieve maximum efficiency in the drive and meets the foregoing objectives. The starter-generator drive has a multi-speed transmission for stepping the input speed from an engine to a hydro-viscous dissipative clutch to provide plural speed ranges of operation and thus limit the amount of slip that occurs within the clutch in each range to provide the constant speed drive of the generator. The dissipative clutch operates in a hydro-viscous manner whereby sudden changes of speed, as the multi-speed transmission shifts, do not vary the torque transmitted to the generator and therefore the speed of the generator. This avoids transients in the output power frequency of the generator during ratio changing of the multi-speed transmission. The starter-generator drive also provides for dissipative engine start utilizing the generator as an electric motor.
A multi-range starter-generator drive connected between a variable speed engine and a generator, comprising:
A multi-range starter-generator drive comprising:
A multi-range aircraft starter-generator drive in combination with a variable speed engine and a generator for alterntively driving the generator from the variable speed engine or utilizing the generator as a motor to start the engine, comprising:
A constant speed drive for driving a generator at constant speed from a variable speed engine comprising, a first shaft for operative connection to an engine, planetary gear means having plural relatively movable planetary elements with a first planetary element connected to said first shaft, and also having second, third and fourth planetary elements, a selectively operable brake connected to said second planetary element, first and second drive trains with the first drive train connected to the third planetary element for movement therewith and the second drive train connected to the fourth planetary element, hydroviscous means for transmitting torque and having a pair of shafts with one of said pair of shafts drivingly coupled to the generator, said first and second drive trains being both connected to the other of said pair of shafts, and each of said first and second drive trains having a selectively operable clutch whereby there can be different drive ratios between the engine and the constant torque-transmitting means depending upon which of said selectively operable clutches is operable as well as selective operation of the brake.
A multi-range aircraft starter-generator drive for alternatively driving the generator from a variable speed engine or utilizing the generator as a motor to start the engine, comprising:
Dependencies are inferred from the claim text.