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US3677098A Expired / Lapsed US ⏱️ 0.0 years remaining

Gyroscope uncaging device

Assignee: Plessey Telecommunications Research Ltd
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Filing: 1970-09-30
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Granted: 1972-07-18
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Expires: 1990-09-30
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Abstract

Abstract In order to minimize uncaging kicks on the rotor of a gyroscope device, the caging member acts on the rotor through air buffer means which, in air-bearing fashion, produce, during caging, aligning forces as a result of differences in the thickness of the air cushion. These forces rapidly decrease in size during uncaging by withdrawal of the caging member.

Inventors

  • 👤 John Christopher Hammond Davis

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-27 21:32
CPC Classifications
G; G01; G01C; G01C19/00; G01C19/02; G01C19/04; G01C19/26; Y; Y10; Y10T; Y10T74/00; Y10T74/12; Y10T74/1204; Y10T74/1207; Y10T74/1229; Y10T74/1232; Y10T74/1239; Y10T74/1282

Claims Analysis

Total Claims: 6
Claim 1
Independent Claim 320 words
A gyroscope device comprising a supporting structure, a stator, a rotor constructed symmetrically to a rotor axis, and means for caging the rotor on the stator relative enveloping a caging axis intersecting said rotor axis, wherein the stator incluDes a spherical bearing member, a stem connecting said spherical bearing member to the supporting structure and having a cylinder surface coaxial with said caging axis, and gas bearing means supporting the rotor on said spherical bearing member for rotation about said rotor axis and for universal movement about the point of intersection of said rotor axis with said caging axis, said stem and bearing member being provided with passages for the supply of gas to the surface of said bearing member, the rotor including a spherical shell portion enveloping said spherical bearing member at a small distance therefrom so as to form therewith a gas bearing when gas is supplied through said passages, and the rotor being formed to include a surface of revolution which is coaxial with said rotor axis and which has a profile extending approximately radially from the said point of intersection of the rotor axis with the caging axis, said caging means including a caging member guided on said cylinder surface for movement in the direction of said caging axis between a caging position and a free position, said caging member having bearing-surface portions which are spaced round said caging axis at equal distances from said axis and which are so arranged that when said caging member is in said caging position, said bearing surface portions face said surface of revolution of the stator at small and equal distances, the gyroscope device also including means for producing between each said bearing surface portion and said surface of revolution a flow of gas operative, when the rotor axis forms an angle with the caging axis, to exert upon the rotor a couple tending to reduce the said angle.
Claim 2
Dependent Claim 320 words
A gyroscope device comprising a supporting structure, a stator, a rotor constructed symmetrically to a rotor axis, and means for caging the rotor on the stator relative enveloping a caging axis intersecting said rotor axis, wherein the stator incluDes a spherical bearing member, a stem connecting said spherical bearing member to the supporting structure and having a cylinder surface coaxial with said caging axis, and gas bearing means supporting the rotor on said spherical bearing member for rotation about said rotor axis and for universal movement about the point of intersection of said rotor axis with said caging axis, said stem and bearing member being provided with passages for the supply of gas to the surface of said bearing member, the rotor including a spherical shell portion enveloping said spherical bearing member at a small distance therefrom so as to form therewith a gas bearing when gas is supplied through said passages, and the rotor being formed to include a surface of revolution which is coaxial with said rotor axis and which has a profile extending approximately radially from the said point of intersection of the rotor axis with the caging axis, said caging means including a caging member guided on said cylinder surface for movement in the direction of said caging axis between a caging position and a free position, said caging member having bearing-surface portions which are spaced round said caging axis at equal distances from said axis and which are so arranged that when said caging member is in said caging position, said bearing surface portions face said surface of revolution of the stator at small and equal distances, the gyroscope device also including means for producing between each said bearing surface portion and said surface of revolution a flow of gas operative, when the rotor axis forms an angle with the caging axis, to exert upon the rotor a couple tending to reduce the said angle.
Claim 3
Dependent Claim 46 words
A gyroscope device as claimed in claim 1, wherein the caging member is provided with a plurality of jet nozzles whose axes are approximately parallel to the caging axis, and which respectively penetrate said surface portions to face an approximately plane end face of the rotor.
Claim 4
Dependent Claim 22 words
A gyroscope device as claimed in claim 2, which includes means f axially adjusting the individual jet nozzles in the caging member.
Claim 5
Dependent Claim 31 words
A gyroscope device claimed in claim 1, wherein the spherical bearing member is provided, at a point diametrically opposite to the stem, with a stem extension which includes said cylinder surface.
Claim 6
Dependent Claim 63 words
A gyroscope device as claimed in claim 1, wherein the said surface of revolution is an inwardly facing cone surface penetrating said spherical shell portion, and wherein the bearing-surface portions of the caging member jointly form on the caging member an outwardly facing cone surface which forms with said surface of revolution an annular gap through which gas passes from the gas bearing.

References Cited (Backward Citations)

US3115784A Cited
US3416378A Cited
US3438269A Cited
US3457793A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1975-07-18 1976-01-17 1976-07-18 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1979-07-18 1980-01-17 1980-07-18 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1983-07-18 1984-01-17 1984-07-18 $7700.00 Window Closed / Lapsed

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