US5282719A — Quad mode fan pitch actuation system for a gas tu…

Claim 1

Independent Claim 169 words

Apparatus for controlling variable blade pitch of a turbine engine including a turbine shaft and a plurality of fan blades, said apparatus comprising: a first member relatively rotatable with respect to said shaft; a second member relatively rotatable with respect to said shaft; differential gear means for interengaging with said first and second members and for providing a translational output in response to rotation of said first and second members relative to said shaft; linkage means for receiving said translational output of said differential gear means and for converting and transmitting said translational output to said fan blades to affect a pitch change of said fan blades; first actuator means for selectively causing rotation of said first member relative to said shaft and thereby effecting a pitch change of said fan blades in a first direction; and second actuator means for selectively causing rotation of said second member relative to said shaft and thereby effecting a pitch change of said fan blades in a direction opposite said first direction.

Claim 2

Dependent Claim 169 words

Apparatus for controlling variable blade pitch of a turbine engine including a turbine shaft and a plurality of fan blades, said apparatus comprising: a first member relatively rotatable with respect to said shaft; a second member relatively rotatable with respect to said shaft; differential gear means for interengaging with said first and second members and for providing a translational output in response to rotation of said first and second members relative to said shaft; linkage means for receiving said translational output of said differential gear means and for converting and transmitting said translational output to said fan blades to affect a pitch change of said fan blades; first actuator means for selectively causing rotation of said first member relative to said shaft and thereby effecting a pitch change of said fan blades in a first direction; and second actuator means for selectively causing rotation of said second member relative to said shaft and thereby effecting a pitch change of said fan blades in a direction opposite said first direction.

Claim 3

Dependent Claim 35 words

The apparatus of claim 1 wherein each said actuator means includes brake means for applying a braking force to its associated member to thereby slow rotation of its associated member with respect to said shaft.

Claim 4

Dependent Claim 46 words

The apparatus of claim 2 wherein each said brake means comprises a brake rotor secured for rotation with its associated member and a stator affixed to a housing of said engine, whereby a stator receives a DC excitation to retard rotation of its associated brake rotor.

Claim 5

Dependent Claim 23 words

The apparatus of claim 3 wherein each said brake rotor includes a squirrel cage rotor, and wherein each said stator includes multiphase windings.

Claim 6

Dependent Claim 28 words

The apparatus of claim 3 further including control means for selectively effecting a pitch change while said engine is running by exciting a selected one of said stators.

Claim 7

Dependent Claim 63 words

The apparatus of claim 3 further including control means for selectively effecting a pitch change while said engine is not running by exciting at least one of said stators with AC power; and for selectively rotating said shaft while said engine is not running by application of alternating current of like phase to both said stators to accelerate said engine toward starting speed.

Claim 8

Dependent Claim 102 words

The apparatus of claim 1 wherein said differential gear means includes: gear means, coupled to said shaft and responsive to said first and second members, for providing a rotational output in one direction when said first member is rotated faster than said second member and for providing a rotational output in an opposite direction when said second member is rotated faster than said first member; and translational means, responsive to said rotational output of said gear means, for converting said rotational output to linear motion; wherein said linkage means rotates said blades in response to said linear motion of said translational means.

Claim 9

Dependent Claim 49 words

The apparatus of claim 7 wherein said translational means comprises a ball screw assembly including an annular ball screw and an associated pair of oppositely disposed axially traveling annular ball nuts, said annular ball nuts driving said linkage means when said ball screw is rotated by said gear means.

Claim 10

Dependent Claim 15 words

The apparatus of claim 8 wherein said ball screw assembly is a double acting type.

Claim 11

Dependent Claim 57 words

The apparatus of claim 8 wherein said linkage means includes, for each blade: a yoke secured for rotation with its associated blade; first linking means for linking a first end of said yoke to one of said nuts; and second linking means for linking a second end of said yoke to the other one of said nuts.

Claim 12

Dependent Claim 19 words

The apparatus of claim 10 wherein said linkage means further includes counterweight means for balancing each said linking means.

Claim 13

Independent Claim 148 words

A method of operating a differential electromagnetic induction fan blade pitch system having two induction motors, each said induction motor including a rotor and a stator, said method comprising the steps of; selectively energizing either one of the stators to alter fan blade pitch in opposite senses when the fan is rotating and a first mode of operation is selected; selectively energizing both of the stators simultaneously such that both rotors transmit torque to rotate the fan for assisting in starting fan rotation when a second mode of operation is selected; selectively energizing at least one of the stators to drive the fan to a reverse pitch position when a third mode of operation is selected whereby the rotating fan creates a reverse thrust; and driving both rotors by the engine during normal fan operation to generate auxiliary electrical power when a fourth mode of operation is selected.

Claim 14

Independent Claim 148 words

A method of operating a differential electromagnetic induction fan blade pitch system having two induction motors, each said induction motor including a rotor and a stator, said method comprising the steps of; selectively energizing either one of the stators to alter fan blade pitch in opposite senses when the fan is rotating and a first mode of operation is selected; selectively energizing both of the stators simultaneously such that both rotors transmit torque to rotate the fan for assisting in starting fan rotation when a second mode of operation is selected; selectively energizing at least one of the stators to drive the fan to a reverse pitch position when a third mode of operation is selected whereby the rotating fan creates a reverse thrust; and driving both rotors by the engine during normal fan operation to generate auxiliary electrical power when a fourth mode of operation is selected.

Claim 15

Dependent Claim 143 words

Apparatus for rotating at least one output member in response to relative rotation between first and second input members, comprising; a planetary gear train having first and second input gears coupled to said first and second input members and having an output driven in response to relative rotation between said first and second input members; a drive plate member engaging said output of said planetary gear train; ball screw means, including a ball screw secured to said drive plate member and ball nuts threadedly engaging said ball screw and moving axially on said ball screw in response to rotation of said ball screw by said drive plate member; and a yoke member corresponding to each output member, each said yoke member being coupled to said ball nuts for rotating said corresponding output member when said ball nuts move axially on said ball screw.

Claim 16

Dependent Claim 143 words

Apparatus for rotating at least one output member in response to relative rotation between first and second input members, comprising; a planetary gear train having first and second input gears coupled to said first and second input members and having an output driven in response to relative rotation between said first and second input members; a drive plate member engaging said output of said planetary gear train; ball screw means, including a ball screw secured to said drive plate member and ball nuts threadedly engaging said ball screw and moving axially on said ball screw in response to rotation of said ball screw by said drive plate member; and a yoke member corresponding to each output member, each said yoke member being coupled to said ball nuts for rotating said corresponding output member when said ball nuts move axially on said ball screw.

Claim 17

Dependent Claim 33 words

The apparatus of claim 13, wherein said first and second input members are sleeves which terminate in said first and second input gears, respectively, one sleeve being disposed coaxially about the other sleeve.

Claim 18

Dependent Claim 16 words

The apparatus of claim 14, further comprising locking means for interlocking said first and second sleeves.

Claim 19

Dependent Claim 71 words

The apparatus of claim 15, wherein said locking means includes: a first set of disks secured for axial movement on said first sleeve; a second set of disks secured for axial movement on said second sleeve, said first and second disks being interleaved; and actuatable urging means for urging said first set of disks against said second set of disks when said first and second sleeves are to be locked together.

Claim 20

Dependent Claim 98 words

The apparatus of claim 16, wherein said actuatable means includes: a solenoid having an armature which slides from a first position towards a second position when said solenoid is actuated; an arm extending from said armature, towards said disks; and spring means for pressing said arm against said disks when said armature is at said first position, whereby said first and second sleeves are interlocked, said solenoid being actuated to remove pressure on said disks, allowing said first set of disks to rotate relative to said second set of disks, whereby said first and second sleeves are unlocked.

Annuity Stage	Window Opens	Payment Deadline	Surcharge Period Until	Estimated Fee	Status
3.5 Years (Year 4)	1997-01-31	1997-08-02	1998-02-01	$2000.00	Window Closed / Lapsed
7.5 Years (Year 8)	2001-01-31	2001-08-02	2002-02-01	$3760.00	Window Closed / Lapsed
11.5 Years (Year 12)	2005-01-31	2005-08-02	2006-02-01	$7700.00	Window Closed / Lapsed

Quad mode fan pitch actuation system for a gas turbine engine

Abstract

Inventors

Bibliographic Details

Claims Analysis

References Cited (Backward Citations)

USPTO Annuity & Maintenance Windows

Assigned Categories & Tags

Assign Category Tag