Patent US2565965A successfully refreshed from Google Patents.
Patent US4268220A successfully refreshed from Google Patents.
US4268220A
Expired / Lapsed
US
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Thrust balancing
Assignee: Rolls Royce Corp
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Filing: 1979-03-05
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Granted: 1981-05-19
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Expires: 1999-03-05
Abstract
Abstract A gas turbine engine having variable geometry flow controllers therein for controlling mass flow in accordance with engine operation includes a rotor with a wide variation in thrust forces thereon during different phases of engine operation countered by a variable axial load integrating device having a rotating hydraulic thrust compensating piston mounted forwardly of the rotor in association with a rotor thrust bearing and further including means for generating a centrifugal head in accordance with engine speed and wherein improved oil distribution panels are included to evenly distribute oil between the rotating piston and a nonrotating counterpiston to form a uniform depth of rotating oil automatically regulated by an integral, flow regulator having flow area therethrough varied in accordance with axial position of a thrust bearing carriage that has the variable rotor thrust loading imposed thereon.
Inventors
- 👤 Richard C. Malott
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-09 01:41
CPC Classifications
F; F01; F01D; F01D25/00; F01D25/16; F01D3/00; F01D3/04
Claims Analysis
Total Claims: 4
Claim 1
Independent Claim
214 words
A rotor thrust compensating assembly for association with a gas turbine engine comprising: a rotor 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 being fixed to said rotor for both axial and rotary movement therewith, bearing support means for the other of said races, variable axial load integrating means including a pair of relatively rotating pistons having a cavity therebetween, oil supply means for directing oil into said load integrating means in accordance with rotor thrust loads acting on the said one of said races, means on one of said relatively rotating pistons to define a plurality of separate circumferentially spaced pockets thereon, the other of said pair of relatively rotating pistons having an inboard surface, a cover on said one of said pistons with an open end thereon for directing oil from said oil supply means into each of said pockets, said cover having pores therethrough rotated with respect to said inboard surface for distributing liquid from said pockets to uniformly fill said cavity between said surface and said cover for producing a uniformly distributed resultant dynamic hydraulic force on said rotor to compensate variable gas loadings thereon.
Claim 2
Dependent Claim
214 words
A rotor thrust compensating assembly for association with a gas turbine engine comprising: a rotor 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 being fixed to said rotor for both axial and rotary movement therewith, bearing support means for the other of said races, variable axial load integrating means including a pair of relatively rotating pistons having a cavity therebetween, oil supply means for directing oil into said load integrating means in accordance with rotor thrust loads acting on the said one of said races, means on one of said relatively rotating pistons to define a plurality of separate circumferentially spaced pockets thereon, the other of said pair of relatively rotating pistons having an inboard surface, a cover on said one of said pistons with an open end thereon for directing oil from said oil supply means into each of said pockets, said cover having pores therethrough rotated with respect to said inboard surface for distributing liquid from said pockets to uniformly fill said cavity between said surface and said cover for producing a uniformly distributed resultant dynamic hydraulic force on said rotor to compensate variable gas loadings thereon.
Claim 3
Dependent Claim
241 words
A rotor thrust compensating assembly for association with a gas turbine engine comprising: a rotor extension having a fore segment and an 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 being fixed to said rotor extension for both axial and rotary movement therewith, bearing support means for the other of said races, variable axial load integrating means including a pair of relatively rotating pistons having a cavity therebetween, flow regulator means including said bearing support means to direct oil into said load integrating means in accordance with rotor thrust loads acting on the said one of said races, one of said relatively rotating pistons having a plurality of circumferentially spaced pockets thereon separated from one another by a plurality of reinforcing ribs to maintain a surface of said piston in spaced parallel relationship to an inboard surface of said other of said relatively rotating pistons, a cover for said pockets having an open end for directing oil into each of said pockets, said cover having pores therethrough rotated with respect to said inboard surface for distributing oil from each of said pockets to uniformly fill said cavity between said surface and said cover for producing a uniformly distributed resultant dynamic hydraulic force on said rotor extension to compensate variable gas loadings thereon.
Claim 4
Dependent Claim
241 words
A rotor thrust compensating assembly for association with a gas turbine engine comprising: a rotor extension having a fore segment and an 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 being fixed to said rotor extension for both axial and rotary movement therewith, bearing support means for the other of said races, variable axial load integrating means including a pair of relatively rotating pistons having a cavity therebetween, flow regulator means including said bearing support means to direct oil into said load integrating means in accordance with rotor thrust loads acting on the said one of said races, one of said relatively rotating pistons having a plurality of circumferentially spaced pockets thereon separated from one another by a plurality of reinforcing ribs to maintain a surface of said piston in spaced parallel relationship to an inboard surface of said other of said relatively rotating pistons, a cover for said pockets having an open end for directing oil into each of said pockets, said cover having pores therethrough rotated with respect to said inboard surface for distributing oil from each of said pockets to uniformly fill said cavity between said surface and said cover for producing a uniformly distributed resultant dynamic hydraulic force on said rotor extension to compensate variable gas loadings thereon.
References Cited (Backward Citations)
FR851065A
Cited
US2779531A
Cited
US3485541A
Cited
US3468259A
Cited
US3491536A
Cited
US3505813A
Cited
US3671137A
Cited
US3746461A
Cited
US4183713A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1984-05-18 | 1984-11-17 | 1985-05-19 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1988-05-18 | 1988-11-17 | 1989-05-19 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1992-05-18 | 1992-11-17 | 1993-05-19 | $7700.00 | Window Closed / Lapsed |