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US 4,914,906 AGranted
Turbine starter device
AssigneeAllied-Signal Inc.
InventorDarrel W. Burch
Life of this patent
Estimating the term…
Abstract
A double clutch mechanism is disclosed for use within a starter assembly for selectively coupling power to start a turbine engine. The invention includes a primary engagement assembly and a secondary engagement assembly, either of which may be of the pawl and ratchet type or the sprag type, for coupling power to the engine and preventing overrunning of the starter assembly.
Claims16
A starter for a gas turbine engine comprising:
- turbine means adapted to receive motive gas flow and for producing high speed low torque output;
- gear transmission means associated with said turbine means, for changing said high speed low torque output of said turbine means to a low speed high torque output;
- drive shaft means for transmitting rotational power from the starter to the gas turbine engine;
- gear assembly adapted to be supported on bearings and rotatably driven by said gear transmission means;
- a driven assembly attached to said drive shaft means;
- a double pawl and ratchet clutch assembly having primary pawls carried on said driven assembly, secondary pawls carried on said gear assembly, an external ratchet cylinder carried on said driven assembly, and an internal ratchet cylinder carried on said gear assembly, said driven assembly and said gear assembly configured to have said primary pawls operative with said external ratchet cylinder and said secondary pawls operative with said internal ratchet cylinder;
- and
- resilient biasing means associated with each of said primary and secondary pawls for biasing said primary and second pawls radially inward against centrifugal forces, and for allowing running engagements of said driven assembly while preventing said driving assembly from attaining a rotational speed in excess of said driven assembly.
5 more elements
A starter for a gas turbine engine comprising:
- turbine means adapted to receive motive gas flow and for producing high speed low torque output;
- gear transmission means associated with said turbine means, for changing said high speed low torque output of said turbine means to a low speed high torque output;
- drive shaft means for transmitting rotational power from the starter to the gas turbine engine;
- a gear assembly supported on bearings and rotatably driven by said gear transmission means;
- a driven assembly attached to said drive shaft means;
- a double sprag clutch assembly having a plurality of primary sprags contained within a frame attached to said driven assembly, and a plurality of secondary sprags contained within a secondary frame attached for rotation with said gear assembly, said gear assembly and said driven assembly configured to have said primary sprags operative to engage and transmit torque from a cylindrical driving race attached to said gear assembly, and said secondary sprags operative to engage and transmit torque to an internal race of said driven assembly;
- and
- resilient biasing means associated with each of said primary sprags and said secondary sprags for biasing said primary and said secondary sprags radially inward against centrifugal forces and for allowing running engagements of said driven assembly while preventing said driving assembly from attaining a rotational speed in excess of said driven assembly.
5 more elements
A starter for a gas turbine engine comprising:
- turbine means adapted to receive motive gas flow and for producing high speed low torque output;
- gear transmission means associated with said turbine means, for changing said high speed low torque output of said turbine means to a low speed high torque output;
- drive shaft means for transmitting rotational power form the starter to the gas turbine engine;
- a driving assembly attached to said gear transmission means;
- a driven assembly attached to said drive shaft means;
- primary engagement means resiliently biased and secured for rotation with said driven assembly, for transferring a torque load from said driving assembly at synchronous rotational speeds below a threshold rotational speed of said driven assembly, and for disengaging said driven assembly from said driving assembly when said torque load is removed;
- and
- secondary engagement means, resiliently biased and secured for rotation with said driving assembly, for response to centrifugal forces causing said secondary engagement means to contact said driven assembly at a speed below said threshold speed, and for allowing running engagements of said driven assembly while preventing said driving assembly from attaining a rotational speed in excess of said driven assembly.
5 more elements
An assembly for starting a turbine engine comprising:
- starter means for producing output rotational motion of a driving assembly;
- drive shaft means connected to said engine for receiving rotational motion from said starter means;
- a driven assembly attached to said drive shaft;
- primary engagement means resiliently biased and secured for rotation with said driven assembly, for transferring a torque load from said driving assembly to said driven assembly, said primary engagement means for initially engaging said driving assembly at synchronous rotational speeds below a threshold rotational speed of said driven assembly, and for disengaging said driven assembly from said driving assembly when said torque load is removed;
- and
- secondary engagement means, resiliently biased and secured for rotation with said driving assembly, for response to centrifugal forces causing said secondary engagement means to contact said driven assembly at a speed below said threshold speed, and for allowing running engagements of said driven assembly while preventing said driving assembly from attaining a rotational speed in excess of said driven assembly.
3 more elements
Dependencies are inferred from the claim text.