GB884061A - Gyroscopes, gyroscope stabilised systems and gas bearings for the same - Google Patents

Gyroscopes, gyroscope stabilised systems and gas bearings for the same

Info

Publication number
GB884061A
GB884061A GB17692/58A GB1769258A GB884061A GB 884061 A GB884061 A GB 884061A GB 17692/58 A GB17692/58 A GB 17692/58A GB 1769258 A GB1769258 A GB 1769258A GB 884061 A GB884061 A GB 884061A
Authority
GB
United Kingdom
Prior art keywords
rotor
intermediate frame
gas
bearings
axis
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB17692/58A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
STC PLC
Original Assignee
Standard Telephone and Cables PLC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Standard Telephone and Cables PLC filed Critical Standard Telephone and Cables PLC
Publication of GB884061A publication Critical patent/GB884061A/en
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C19/00Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C19/00Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
    • G01C19/02Rotary gyroscopes
    • G01C19/04Details
    • G01C19/16Suspensions; Bearings
    • G01C19/20Suspensions; Bearings in fluid
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2370/00Apparatus relating to physics, e.g. instruments
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C32/00Bearings not otherwise provided for
    • F16C32/06Bearings not otherwise provided for with moving member supported by a fluid cushion formed, at least to a large extent, otherwise than by movement of the shaft, e.g. hydrostatic air-cushion bearings
    • F16C32/0603Bearings not otherwise provided for with moving member supported by a fluid cushion formed, at least to a large extent, otherwise than by movement of the shaft, e.g. hydrostatic air-cushion bearings supported by a gas cushion, e.g. an air cushion

Landscapes

  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Magnetic Bearings And Hydrostatic Bearings (AREA)

Abstract

884,061. Fluid bearings. STANDARD TELEPHONES & CABLES Ltd. June 3, 1958 [June 3, 1957], No. 17692/58. Class 12 (1). [Also in Group XX] A gyroscope comprises a rotor 1, Fig. 1, adapted to rotate about an axis 2, an intermediate frame 4, and gas bearings for the rotor 1, so that it has two degrees of freedom of tilting of its axis, and means for steadily rotating both the rotor 1 and the intermediate frame 4 with respect to a main frame, which is intended to remain approximately rotationally fixed in space, so that processional drifts resulting from static torques of the gas bearings are continually neutralized. As shown, the rotor 1 is supported by six bearing pads 3, gas being supplied through the manifolding 5 to the reservoirs 6 within the pads 3, and fed through the almost microscopic feed holes 7 to the bearing surfaces. The rotor 1, which is hollow, has two cylindrical cavities 2 which define the axis of rotation and are used with the pick-off system which may be capacitive or photoelectric. The intermediate frame 4 is mounted in mechanical bearings and spun by some external driving mechanism such as an electric motor or gas turbine system, and the rotor 1 may be secured by a caging mechanism, not shown, to the intermediate frame 4 during both the spin-period and also the slow-down period. When the operating speed is reached, the caging mechanism releases the rotor 1 which is then supported solely by the gas bearings. The signals obtained from the pick-off arrangement, are used to maintain the intermediate frame 4 in line with the rotor 1 about all axes except the axis of rotation, and the rotor may be spun at a speed different from that of the intermediate frame 4, for example at a higher speed. In a modification, Fig. 5, in which the rotor and intermediate frame rotate at the same speed, the six bearing pads 27, support a sphere 39 which is connected by spokes 40 to an external rotor 38, and high pressure gas is supplied through manifolding 29 into feed tubes 30 and high pressure chambers 31. The gas passes to the bearing surface through the very minute feed holes 32 and leaves through a ring 28 and vacuum chamber 34. A still higher vacuum is maintained in the case 36. In another embodiment in which there are eight bearing pads, each has three chambers 51, 52, 53, Fig. 12. High pressure gas from chamber 51 passes through holes 89 and is mostly received by the inner ring 91, to which a moderate suction is applied through chamber 52. Chamber 53 applies a considerably higher suction to the second ring 93 through the connecting holes 94. A still higher degree of vacuum is applied to the casing in which the bearing pads and rotor are mounted. In a modification, the casing instead of being spherical may be flattened at the top and bottom and the rotor may have a corresponding configuration.
GB17692/58A 1957-06-03 1958-06-03 Gyroscopes, gyroscope stabilised systems and gas bearings for the same Expired GB884061A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US884061XA 1957-06-03 1957-06-03

Publications (1)

Publication Number Publication Date
GB884061A true GB884061A (en) 1961-12-06

Family

ID=22211191

Family Applications (1)

Application Number Title Priority Date Filing Date
GB17692/58A Expired GB884061A (en) 1957-06-03 1958-06-03 Gyroscopes, gyroscope stabilised systems and gas bearings for the same

Country Status (1)

Country Link
GB (1) GB884061A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2005068988A2 (en) * 2004-01-16 2005-07-28 Forschungszentrum Jülich GmbH Rotor
EP2017575A2 (en) * 2007-07-17 2009-01-21 Honeywell International Inc. Inertial measurement unit with gas plenums
US8919213B2 (en) 2012-05-21 2014-12-30 Honeywell International Inc. Control moment gyroscopes including rotors having radially-compliant spokes and methods for the manufacture thereof
US9354079B2 (en) 2012-05-21 2016-05-31 Honeywell International Inc. Control moment gyroscopes including torsionally-stiff spoked rotors and methods for the manufacture thereof
CN107131874A (en) * 2017-06-23 2017-09-05 桂林电子科技大学 The spherical omnidirectional's gyro mechanism of totally enclosed type and its operation method

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2005068988A2 (en) * 2004-01-16 2005-07-28 Forschungszentrum Jülich GmbH Rotor
WO2005068988A3 (en) * 2004-01-16 2005-10-06 Forschungszentrum Juelich Gmbh Rotor
EP2017575A2 (en) * 2007-07-17 2009-01-21 Honeywell International Inc. Inertial measurement unit with gas plenums
EP2017575A3 (en) * 2007-07-17 2015-02-25 Honeywell International Inc. Inertial measurement unit with gas plenums
US8919213B2 (en) 2012-05-21 2014-12-30 Honeywell International Inc. Control moment gyroscopes including rotors having radially-compliant spokes and methods for the manufacture thereof
US9354079B2 (en) 2012-05-21 2016-05-31 Honeywell International Inc. Control moment gyroscopes including torsionally-stiff spoked rotors and methods for the manufacture thereof
CN107131874A (en) * 2017-06-23 2017-09-05 桂林电子科技大学 The spherical omnidirectional's gyro mechanism of totally enclosed type and its operation method

Similar Documents

Publication Publication Date Title
US2729106A (en) Air-supported gyroscope
EP0600851B1 (en) Robot apparatus
US2940318A (en) Gyroscopes, gyroscope stabilized systems and gas bearings for the same
GB1352981A (en) Gyroscopic devices
GB884061A (en) Gyroscopes, gyroscope stabilised systems and gas bearings for the same
GB937444A (en) Free rotor gas bearing gyro
GB890264A (en) Rotatable antenna assembly
US2474072A (en) Air bearing gyroscope
US3813788A (en) Dynamic pendulum north-seeking gyro apparatus
US3747418A (en) Fluidic inertial platform
US3762226A (en) Control moment gyroscope with integral torque control
US2129586A (en) Gyroscopic instrument
US2969680A (en) Gyroscope utilizing inverted hydrodynamic bearings
US3501966A (en) Photodynamic pickoff means having a pulse duration modulated output
US3604277A (en) Single jet pneumatic pulse duration modulation gyro
US2380932A (en) Gyro magnetic compass
US4000660A (en) Drift-compensated free-rotor gyro
US3335614A (en) Stable platforms
US3320816A (en) Pneumatic pickoff for two degree of freedom gyro
GB1364757A (en) Gyroscopic devices
US3354727A (en) Gyroscopic apparatus
US3877317A (en) Dynamic gas-liquid gyroscope bearing
US2512279A (en) Gyroscopically-controlled instrument
GB191513280A (en) Improvements in Gyrostatic Apparatus.
US2382967A (en) Gyro rotor and mounting structure