Aircraft generator starter-drive

Claim 2

A hydraulic control system for an aircraft starter-drive mechanism that includes a generator/motor drivingly connected through a differential, which is mutually connected to first and second hydraulic units and to an engine driveshaft during a start mode, said hydraulic control comprising: a control valve operatively coupled to said first and second hydraulic units and operative in said starting mode to control flow between said hydraulic units to thereby divide the delivery of rotary power from the generator/motor to said engine driveshaft through said differential and said hydraulic units.

Claim 3

The combination of claim 1, wherein said control valve is operative to dissipate the energy of hydraulic flow between said first and second hydraulic units, while simultaneously operative in said starting mode to cause said first hydraulic unit to maintain maximum displacement, thereby initiating an engine starting torque to said second shaft through said hydraulic units and said differential.

Claim 4

The combination of claim 2, wherein the cooperation of the control valve and the hydraulic units is such that when the flow capacity of said second hydraulic unit matches the maximum displacement flow capacity of said first hydraulic unit, said control valve causes said first hydraulic unit displacement to be reduced to zero and thereafter, to a maximum value in an opposite direction, thereby increasing the speed of said second shaft while simultaneously reducing torque.

Claim 5

The combination of claim 1, wherein said first hydraulic unit is of a variable displacement type.

Claim 6

The combination of claim 4, wherein said second hydraulic unit is of a fixed displacement type.

Claim 7

The combination of claim 5, wherein said control valve includes means to control the amount of said first hydraulic unit displacement.

Claim 8

The combination of claim 4, wherein said second hydraulic unit is of the variable displacement type.

Claim 9

The combination of claim 7, wherein said control valve includes means to independently control the amount of both hydraulic units displacement.

Claim 10

The combination of claim 1, wherein said control valve is operative in said starting mode to cause said second hydraulic unit displacement to be increased while simultaneously maintaining said first hydraulic unit at maximum displacement, thereby initiating an engine starting torque on said second shaft exclusively from said first hydraulic unit through said first element of said differential, thereafter said second hydraulic unit increased displacement results in a contribution to engine starting torque acting through said second element of said differential, thereby increasing the starting torque to a maximum value achieved when said second hydraulic unit displacement matches the displacement of said first hydraulic unit.

Claim 11

The combination of claim 8, wherein the cooperation of the control valve and the hydraulic units is such that when the flow of said second hydraulic unit matches the displacement of said first hydraulic unit, said control valve causes said first hydraulic unit displacement to be reduced to zero and thereafter, to a maximum value in an opposite direction, thereby increasing the speed of said second shaft while simultaneously reducing torque.

Claim 12

A starter-drive for use between an aircraft engine and a generator/motor to transmit in either direction, comprising: a first shaft connectible with said generator/motor, a second shaft connectible with said engine, a differential including first, second and third elements, said first element rotatable with said second shaft and said third element rotatable on said second shaft, a first hydraulic unit drivingly connected to said first element, a second hydraulic unit drivingly connected to said second element, said first and second hydraulic units hydraulically interconnected through and controlled by a control valve, said third element drivingly connected through a first clutch to said first shaft for driving said generator/motor in a generating mode, and through a second clutch to said first shaft for driving said engine from said generator/motor in a starting mode, said control valve operative in said starting mode to control flow between said hydraulic units to thereby divide the delivery of rotary power from the generator/motor to said second shaft and said engine through said differential and said hydraulic units.

Claim 13

A starter-drive for use between an aircraft engine and a generator/motor to transmit in either direction, comprising: a first shaft connectible with said generator/motor, a second shaft connectible with said engine, a differential including first, second and third elements, said first element rotatable with said second shaft and said third element rotatable on said second shaft, a first hydraulic unit drivingly connected to said first element, a second hydraulic unit drivingly connected to said second element, said first and second hydraulic units hydraulically interconnected through and controlled by a control valve, said third element drivingly connected through a first clutch to said first shaft for driving said generator/motor in a generating mode, and through a second clutch to said first shaft for driving said engine from said generator/motor in a starting mode, said control valve operative in said starting mode to control flow between said hydraulic units to thereby divide the delivery of rotary power from the generator/motor to said second shaft and said engine through said differential and said hydraulic units.

Claim 14

The combination of claim 11, wherein said first clutch is a one-way clutch.

Claim 15

The combination of claim 11, wherein said second clutch is a one-way clutch.

Claim 16

The combination of claim 11, wherein said first and second clutches are one-way clutches.

Claim 17

The combination of claim 11, wherein said control valve is operative to dissipate the energy of hydraulic flow between said first and second hydraulic units, while simultaneously operative in said starting mode to cause said first hydraulic unit to maintain maximum displacement, thereby initiating an engine starting torque to said second shaft through said hydraulic units and said differential.

Claim 18

The combination of claim 15, wherein the cooperation of the control valve and the hydraulic units is such that when the flow capacity of said second hydraulic unit matches the maximum displacement flow capacity of said first hydraulic unit, said control valve causes said first hydraulic unit displacement to be reduced to zero and thereafter, to a maxiumum value in an opposite direction, thereby increasing the speed of said second shaft while simultaneously reducing torque.

Claim 19

The combinaton of claim 11, wherein said first hydraulic unit is of the variable displacement type.

Claim 20

The combination of claim 14, wherein said second hydraulic unit is of the fixed displacement type.

Claim 21

The combination of claim 15, wherein said control valve includes means to control the amount of said first hydraulic unit displacement.

Claim 22

The combination of claim 14, wherein said second hydraulic unit is of the variable displacement type.

Claim 23

The combination of claim 16, wherein said control valve includes means to independently control the amount of both hydraulic units displacement.

Claim 24

The combination of claim 11, wherein said control valve is operative in said starting mode to cause said second hydraulic unit displacement to be increased while simultaneously maintaining said first hydraulic unit at maximum displacement, thereby initiating an engine starting torque on said second shaft exclusively from said first hydraulic unit through said first element of said differential, thereafter said second hydraulic unit increased displacement results in a contribution to engine starting torque acting through said second element of said differential, thereby increasing the starting torque to a maximum value achieved when said second hydraulic unit displacement matches the displacement of said first hydraulic unit.

Claim 25

The combination of claim 18, wherein the cooperation of the control valve and the hydraulic units is such that when the flow of said second hydraulic unit matches the displacement of said first hydraulic unit, said control valve causes said first hydraulic unit displacement to be reduced to zero and thereafter, to a maximum value in an opposite direction, thereby increasing the speed of said second shaft while simultaneously reducing torque.