Thrust balancing

Claim 2

A rotor thrust compensator assembly for association with a gas turbine engine comprising: a rotor extension having a fore and aft segment and being axially movable in response to variable gas loads on a rotor element of a gas turbine engine, a thrust bearing having inner and outer races with anti-friction means therebetween, one of said races fixed to said rotor extension for axial movement therewith, bearing support means for the other of said races, variable axial load integrating means including a pair of relatively rotating pistons with a cavity therebetween, a pressurizable fluid system, flow regulator means including a movable carriage engageable with the other of said races and including means thereon for directing fluid into said fluid system and for directing a quantity of fluid into said cavity in accordance with rotor thrust loads acting on the one of said races, the movement of said movable carriage controlling a throttling gap for said fluid, a preload spring biased between said carriage and said bearing support and operative to compensate axial bearing loads when a first predetermined rotor thrust load is imposed on said bearing, one of said relatively rotating pistons being connected to said rotor extension, said one of said relatively rotating pistons rotating fluid within said cavity so as to produce a dynamic, rotor speed responsive centrifugal fluid head on said rotor extension to compensate second predetermined rotor thrust loadings on said bearing.

Claim 3

A rotor thrust compensator assembly for association with a gas turbine engine comprising: a rotor extension having a fore and aft segment and being axially movable in response to variable gas loads on a rotor element of a gas turbine engine, a thrust bearing having inner and outer races with anti-friction means therebetween, one of said races fixed to said rotor extension for axial movement therewith, bearing support means for the other of said races, variable axial load integrating means including a pair of relatively rotating pistons with a liquid cavity therebetween, a pressurizable oil system for receiving engine oil, flow regulator means including a movable carriage engageable with the other of said races and including means thereon for directing engine oil into said oil system and for directing a quantity of oil into said liquid cavity in accordance with rotor thrust loads acting on the one of said races, the movement of said movable carriage controlling a throttling gap for said oil, a preload spring biased between said carriage and said bearing support and operative to compensate axial bearing loads when a first predetermined rotor thrust load is imposed on said bearing, one of said relatively rotating pistons being connected to said rotor extension, said one of said relatively rotating pistons rotating oil within said cavity so as to produce a dynamic, rotor speed responsive centrifugal fluid head on said rotor extension to compensate second predetermined rotor thrust loadings on said bearing.

Claim 4

A rotor thrust compensator assembly for association with a gas turbine engine comprising: a rotor extension having a fore and aft segment and being axially movable in response to variable gas loads on a rotor element of a gas turbine engine, a thrust bearing having inner and outer races with anti-friction means therebetween, one of said races fixed to said rotor extension for axial movement therewith, bearing support means for the other of said races, variable axial load integrating means including a pair of relatively rotating pistons with a liquid cavity therebetween, a pressurizable oil system for receiving engine oil, flow regulator means including a movable carriage engageable with the other of said races and including means thereon for directing engine oil into said oil system and for directing a quantity of oil into said liquid cavity in accordance with rotor thrust loads acting on the one of said races, the movement of said movable carriage controlling a throttling gap for said oil, a preload spring biased between said carriage and said bearing support and operative to compensate axial bearing loads when a first predetermined rotor thrust load is imposed on said bearing, one of said relatively rotating pistons being connected to said rotor extension, said one of said relatively rotating pistons rotating oil within said cavity so as to produce a dynamic, rotor speed responsive centrifugal fluid head on said rotor extension to compensate second predetermined rotor thrust loadings on said bearing.

Claim 5

A rotor thrust compensator assembly for association with a gas turbine engine comprising: a rotor extension having a fore and aft segment and being axially movable in response to variable gas loads on a rotor element of a gas turbine engine, a thrust bearing having inner and outer races with anti-friction means therebetween, one of said races fixed to said rotor extension for axial movement therewith, bearing support means for the other of said races, variable axial load integrating means including a pair of relatively rotating pistons with a liquid cavity therebetween, a pressurizable oil system for receiving engine oil, flow regulator means including a movable carriage engageable with the other of said races and including means thereon for directing engine oil into said oil system and for directing a quantity of oil into said liquid cavity in accordance with rotor thrust loads acting on the one of said races, the movement of said movable carriage controlling a throttling gap for said oil, a preload spring biased between said carriage and said bearing support and operative to compensate axial bearing loads when a first predetermined rotor thrust load is imposed on said bearing, means including said spring causing said carriage to be positioned to open said flow regulator means thereby to cause pressurization of said oil system when the first predetermined rotor thrust load is imposed on said bearing, one of said relatively rotating pistons being connected to said rotor extension, said one of said relatively rotating pistons rotating oil received within said cavity to produce a dynamic, rotor speed responsive centrifugal fluid head on said rotor extension to compensate second predetermined rotor thrust loadings on said bearing.

Claim 6

A rotor thrust compensator assembly for association with a gas turbine engine comprising: a rotor extension having a fore and aft segment and being axially movable in response to variable gas loads on a rotor element of a gas turbine engine, a thrust bearing having inner and outer races with anti-friction means therebetween, one of said races fixed to said rotor extension for axial movement therewith, bearing support means for the other of said races, variable axial load integrating means including a pair of relatively rotating pistons with a liquid cavity therebetween, a pressurizable oil system for receiving engine oil, flow regulator means including a movable carriage engageable with the other of said races and including means thereon for directing engine oil into said oil system and for directing a quantity of oil into said liquid cavity in accordance with rotor thrust loads acting on the one of said races, the movement of said movable carriage controlling a throttling gap for said oil, a preload spring biased between said carriage and said bearing support and operative to compensate axial bearing loads when a first predetermined rotor thrust load is imposed on said bearing, means including said spring causing said carriage to be positioned to open said flow regulator means thereby to cause pressurization of said oil system when the first predetermined rotor thrust load is imposed on said bearing, one of said relatively rotating pistons being connected to said rotor extension, said one of said relatively rotating pistons rotating oil received within said cavity to produce a dynamic, rotor speed responsive centrifugal fluid head on said rotor extension to compensate second predetermined rotor thrust loadings on said bearing.

Claim 7

A rotor thrust compensator assembly for association with a gas turbine engine comprising: a rotor extension having a fore and aft segment and being axially movable in response to variable gas loads on a rotor element of a gas turbine engine, a thrust bearing having inner and outer races with anti-friction means therebetween, one of said races fixed to said rotor extension for axial movement therewith, fixed bearing support means for the other of said races, variable axial load integrating means including first and second relatively rotating pistons with a means on said first and second pistons forming a liquid cavity therebetween, said first piston being connected to said rotor extension, said second piston being fixed to said bearing support means, a pressurizable oil system for receiving engine oil, flow regulator means including a movable carriage engageable with the other of said races and including means thereon for directing engine oil into said oil system and for directing a quantity of oil into said liquid cavity in accordance with rotor thrust loads acting on the one of said races, the movement of said movable carriage controlling a throttling gap for said oil, a preload spring biased between said carriage and said bearing support and operative to compensate axial bearing loads when a first predetermined rotor thrust load is imposed on said bearing, means including said spring for causing said carriage to be positioned to open said flow regulator means thereby to cause pressurization of said oil system when the first predetermined rotor thrust load is imposed on said bearing, means on said first piston to pick up oil received within said cavity and to rotate it so as to produce a dynamic, rotor speed responsive centrifugal fluid head on said rotor extension to compensate second predetermined rotor thrust loadings on said bearing.

Claim 8

A rotor thrust compensator assembly for association with a gas turbine engine comprising: a rotor extension having a fore and aft segment and being axially movable in response to variable gas loads on a rotor element of a gas turbine engine, a thrust bearing having inner and outer races with anti-friction means therebetween, one of said races fixed to said rotor extension for axial movement therewith, fixed bearing support means for the other of said races, variable axial load integrating means including first and second relatively rotating pistons with a means on said first and second pistons forming a liquid cavity therebetween, said first piston being connected to said rotor extension, said second piston being fixed to said bearing support means, a pressurizable oil system for receiving engine oil, flow regulator means including a movable carriage engageable with the other of said races and including means thereon for directing engine oil into said oil system and for directing a quantity of oil into said liquid cavity in accordance with rotor thrust loads acting on the one of said races, the movement of said movable carriage controlling a throttling gap for said oil, a preload spring biased between said carriage and said bearing support and operative to compensate axial bearing loads when a first predetermined rotor thrust load is imposed on said bearing, means including said spring for causing said carriage to be positioned to open said flow regulator means thereby to cause pressurization of said oil system when the first predetermined rotor thrust load is imposed on said bearing, means on said first piston to pick up oil received within said cavity and to rotate it so as to produce a dynamic, rotor speed responsive centrifugal fluid head on said rotor extension to compensate second predetermined rotor thrust loadings on said bearing.