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US3132480A Expired / Lapsed US ⏱️ 0.0 years remaining

Gas turbine engine control using plural servomotors

Assignee: Rolls Royce PLC
•
Filing: 1961-06-27
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Granted: 1964-05-12
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Expires: 1981-06-27
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Abstract

No abstract record available.

Inventors

  • 👤 Johnson Christopher Linley
  • 👤 Jubb Albert

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-01 20:28
CPC Classifications
F; F02; F02K; F02K1/00; F02K1/06; F02K1/15; F02K1/16; F15; F15B; F15B11/00; F15B11/08; F15B11/12

Claims Analysis

Total Claims: 3
Claim 1
Independent Claim 377 words
A FLUID-OPERATED SERVOMECHANISM COMPRISING A CASING HAVING SEPARATE COAXIAL MASTER AND SLAVE CYLINDERS, MASTER AND SLAVE PISTONS AXIALLY SLIDABLY MOUNTED IN SAID MASTER AND SLAVE CYLINDERS RESPECTIVELY, EACH PISTON BEING CONNECTED TO A RESPECTIVE SHAFT AND DIVIDING ITS RESPECTIVE CYLINDER INTO TWO CHAMBERS, THE SHAFT OF THE SLAVE PISTON HAVING A BORE IN WHICH THE SHAFT OF THE MASTER PISTON IS SLIDABLY LOCATED, MEANS FOR ROTATING THE SHAFT OF THE MASTER PISTON, A SLAVE MOTIVE FLUID SOURCE AND FIRST AND SECOND CONTROL PRESSURE FLUID SOURCES, FIRST AND SECOND RESTRICTED ORIFICES MEANS PROVIDING IN SAID CASING, SAID SLAVE PISTON MOTIVE FLUID SOURCE BEING CONNECTED TO EACH OF THE TWO CHAMBERS SEPARATED BY THE SLAVE PISTON VIA SAID FIRST RESTRICTED ORIFICE MEANS, AND SAID FIRST CONTROL PRESSURE FLUID SOURCE BEING CONNECTED TO ONE OF THE TWO CHAMBERS SEPARATED BY THE MASTER PISTON VIA SAID SECOND RESTRICTED ORIFICE MEANS, SAID CASING FURTHER HAVING APERTURE MEANS WHEREBY SAID SECOND CONTROL PRESSURE FLUID SOURCE IS CONNECTED TO THE OTHER OF THE TWO CHAMBERS SEPARATED BY THE MASTER PISTON, SAID ONE CHAMBER HAVING BLEED VALVE MEANS CONTROLLED BY THE RELATIVE POSITION OF THE MASTER PISTON IN ITS CYLINDER FOR BLEEDING FROM SAID ONE CHAMBER PRESSURE FLUID ORIGINATING FROM SAID FIRST CONTROL PRESSURE FLUID SOURCE, WHEREBY THE PRESSURE IN SAID ONE CHAMBER IS REDUCED BELOW THE PRESSURE OF SAID FIRST CONTROL PRESSURE FLUID SOURCE, AND THE MASTER PISTON IS ADJUSTED IN ITS CYLINDER TO A RELATIVE POSITION DEPENDING UNIQUELY ON THE RELATIVE PRESSURES OF SAID FIRST AND SECOND CONTROL PRESSURE FLUID SOURCES, THE MASTER AND SLAVE CYLINDERS BEING AXIALLY SEPARATED BY AN EXHAUST CHAMBER CONNECTED TO EXHAUST, SAID SLAVE PISTON AND SHAFT THEREOF HAVING PASSAGEWAYS CONNECTED EACH CHAMBER SEPARATED BY THE SLAVE PISTON TO THE BORE OF THAT SHAFT, THE SHAFT OF THE MASTER PISTON LOCATED IN SAID BORE HAVING MEANS FOR SELECTIVELY CONNECTING ONE OF SAID PASSAGEWAYS TO THE EXHAUST CHAMBER, DEPENDING ON THE DIRECTION IN WHICH THE MASTER PISTON IS ADJUSTED IN ITS CYLINDER, SUCH THAT THE SLAVE PISTON IS ADJUSTED IN THE SAME DIRECTION AS THE MASTER PISTON AS A RESULT OF THE PRESSURES ON OPPOSITE SIDES OF THE SLAVE PISTON BECOMING UNEQUAL DUE TO THE DISCHARGE OF SLAVE PISTON MOTIVE FLUID TO EXHAUST VIA THE SELECTED ONE OF SAID PASSAGEWAYS.
Claim 2
Dependent Claim 377 words
A FLUID-OPERATED SERVOMECHANISM COMPRISING A CASING HAVING SEPARATE COAXIAL MASTER AND SLAVE CYLINDERS, MASTER AND SLAVE PISTONS AXIALLY SLIDABLY MOUNTED IN SAID MASTER AND SLAVE CYLINDERS RESPECTIVELY, EACH PISTON BEING CONNECTED TO A RESPECTIVE SHAFT AND DIVIDING ITS RESPECTIVE CYLINDER INTO TWO CHAMBERS, THE SHAFT OF THE SLAVE PISTON HAVING A BORE IN WHICH THE SHAFT OF THE MASTER PISTON IS SLIDABLY LOCATED, MEANS FOR ROTATING THE SHAFT OF THE MASTER PISTON, A SLAVE MOTIVE FLUID SOURCE AND FIRST AND SECOND CONTROL PRESSURE FLUID SOURCES, FIRST AND SECOND RESTRICTED ORIFICES MEANS PROVIDING IN SAID CASING, SAID SLAVE PISTON MOTIVE FLUID SOURCE BEING CONNECTED TO EACH OF THE TWO CHAMBERS SEPARATED BY THE SLAVE PISTON VIA SAID FIRST RESTRICTED ORIFICE MEANS, AND SAID FIRST CONTROL PRESSURE FLUID SOURCE BEING CONNECTED TO ONE OF THE TWO CHAMBERS SEPARATED BY THE MASTER PISTON VIA SAID SECOND RESTRICTED ORIFICE MEANS, SAID CASING FURTHER HAVING APERTURE MEANS WHEREBY SAID SECOND CONTROL PRESSURE FLUID SOURCE IS CONNECTED TO THE OTHER OF THE TWO CHAMBERS SEPARATED BY THE MASTER PISTON, SAID ONE CHAMBER HAVING BLEED VALVE MEANS CONTROLLED BY THE RELATIVE POSITION OF THE MASTER PISTON IN ITS CYLINDER FOR BLEEDING FROM SAID ONE CHAMBER PRESSURE FLUID ORIGINATING FROM SAID FIRST CONTROL PRESSURE FLUID SOURCE, WHEREBY THE PRESSURE IN SAID ONE CHAMBER IS REDUCED BELOW THE PRESSURE OF SAID FIRST CONTROL PRESSURE FLUID SOURCE, AND THE MASTER PISTON IS ADJUSTED IN ITS CYLINDER TO A RELATIVE POSITION DEPENDING UNIQUELY ON THE RELATIVE PRESSURES OF SAID FIRST AND SECOND CONTROL PRESSURE FLUID SOURCES, THE MASTER AND SLAVE CYLINDERS BEING AXIALLY SEPARATED BY AN EXHAUST CHAMBER CONNECTED TO EXHAUST, SAID SLAVE PISTON AND SHAFT THEREOF HAVING PASSAGEWAYS CONNECTED EACH CHAMBER SEPARATED BY THE SLAVE PISTON TO THE BORE OF THAT SHAFT, THE SHAFT OF THE MASTER PISTON LOCATED IN SAID BORE HAVING MEANS FOR SELECTIVELY CONNECTING ONE OF SAID PASSAGEWAYS TO THE EXHAUST CHAMBER, DEPENDING ON THE DIRECTION IN WHICH THE MASTER PISTON IS ADJUSTED IN ITS CYLINDER, SUCH THAT THE SLAVE PISTON IS ADJUSTED IN THE SAME DIRECTION AS THE MASTER PISTON AS A RESULT OF THE PRESSURES ON OPPOSITE SIDES OF THE SLAVE PISTON BECOMING UNEQUAL DUE TO THE DISCHARGE OF SLAVE PISTON MOTIVE FLUID TO EXHAUST VIA THE SELECTED ONE OF SAID PASSAGEWAYS.
Claim 3
Dependent Claim 89 words
IN A GAS TURBINE ENGINE INCLUDING A COMPRESSOR, A PRESSURE FUEL SOURCE, AND A PLURALITY OF ADJUSTABLE CONTROL MEMBERS FOR CONTROLLING OPERATION OF THE ENGINE, A FLUIDOPERATED SERVOMECHANISM AS CLAIMED IN CLAIM 1, SAID PRESSURE FUEL SOURCE BEING SAID SLAVE PISTON MOTIVE FLUID SOURCE, SAID COMPRESSOR HAVING TWO DIFFERENT STAGE TAPPINGS SERVING AS SAID FIRST AND SECOND CONTROL PRESSURE FLUIDS SOURCES RESPECTIVELY, AND SAID CONTROL MEMBERS HAVING A COMMON ROTATABLE OPERATING SHAFT, WHICH SHAFT IS CONNECTED TO THE SHAFT OF THE SLAVE PISTON OF THE SERVOMECHANISM FOR ROTATION THEREBY.

References Cited (Backward Citations)

US2613029A Cited
US2746242A Cited
US2705940A Cited
GB736003A Cited
US3085397A Cited
US2941354A Cited
US3007446A Cited
US2971583A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1967-05-12 1967-11-11 1968-05-12 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1971-05-12 1971-11-11 1972-05-12 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1975-05-12 1975-11-11 1976-05-12 $7700.00 Window Closed / Lapsed

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