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US4037887A Expired / Lapsed US ⏱️ 0.0 years remaining

Universal-joint assemblies and self-aligning thrust bearings, especially for the shafts of rotating machines

Assignee: Safran Aircraft Engines SAS
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Filing: 1976-05-10
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Granted: 1977-07-26
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Expires: 1996-05-10
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Abstract

Abstract A thrust-bearing and guiding assembly which permits limited angular displment of a rotating shaft in any axial plane while preventing axial translation motion of the shaft comprises a bearing support articulated within a stator housing. The bearing support has two spherical sliding zones which form part of spheres having different centers, one zone being adapted to cooperate with a complementary surface of a ring which is endowed with freedom of sliding motion in the transverse direction with respect to the axis of the rotor within the stator housing.

Inventors

  • 👤 Roger Louis Elysee Germain

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-08 22:46
CPC Classifications
F; F16; F16C; F16C23/00; F16C23/06; F16C23/08; F16C23/082; F16C23/084; F16C19/00; F16C19/54; F16C19/541; F16C19/542; F16C19/543; F16C23/02; F16C23/04

Claims Analysis

Total Claims: 6
Claim 1
Independent Claim 96 words
A guiding unit for preventing axial translational motion of a rotor shaft of a rotating machine with respect to a stator by permitting limited angular displacement of said shaft in any axial plane comprising a housing, a bearing support articulated within said housing, said housing being within said stator, two partial spherical sliding zones on said support having different centers, a ring, a complementary surface on said ring cooperating with one of said zones and said ring being free in a transverse direction with respect to the axis of rotation of said rotor within said housing.
Claim 2
Dependent Claim 96 words
A guiding unit for preventing axial translational motion of a rotor shaft of a rotating machine with respect to a stator by permitting limited angular displacement of said shaft in any axial plane comprising a housing, a bearing support articulated within said housing, said housing being within said stator, two partial spherical sliding zones on said support having different centers, a ring, a complementary surface on said ring cooperating with one of said zones and said ring being free in a transverse direction with respect to the axis of rotation of said rotor within said housing.
Claim 3
Dependent Claim 35 words
A guiding unit according to claim 1, wherein said two partial spherical sliding zones of said bearing support are convex and a complementary concave surface on said housing cooperating respectively with one of said zones.
Claim 4
Dependent Claim 59 words
A guiding unit according to claim 1, wherein one of said spherical sliding zones of said bearing support is convex a complementary concave surface on said housing cooperating with said one zone and the other of said spherical sliding zones of said bearing support is concave and a complementary convex surface on said housing cooperating with said other zone.
Claim 5
Dependent Claim 39 words
A guiding unit according to claim 1, wherein said two spherical sliding zones of said bearing support are concave and two complementary convex surfaces on said housing each of said convex surfaces cooperating with one of said sliding zones.
Claim 6
Dependent Claim 24 words
A rotating machine having a vertical axis, wherein said machine comprises at least one unit for guiding a rotor shaft according to claim 1.

References Cited (Backward Citations)

US3260543A Cited
US3442561A Cited
US3290897A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1980-07-25 1981-01-24 1981-07-26 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1984-07-25 1985-01-24 1985-07-26 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1988-07-25 1989-01-24 1989-07-26 $7700.00 Window Closed / Lapsed

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