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US3917432A Expired / Lapsed US ⏱️ 0.0 years remaining

Borescope support apparatus

Assignee: General Electric Co
•
Filing: 1974-11-13
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Granted: 1975-11-04
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Expires: 1994-11-13
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Abstract

Abstract An apparatus for supporting a borescope probe in a gas turbine includes a housing, spaced swivel or washer bearings which receive the stem of the borescope probe, resilient washers disposed between the bearings that receive the borescope stem in close fitting relationship therewith, and a locking collar to selectively urge the bearings toward each other so as to deform the washers into gripping engagement with the borescope stem and frictionally lock the bearings.

Inventors

  • 👤 Roger F Feuerstein
  • 👤 Maurice A Freeman
  • 👤 Leonardo B Spinelli

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-23 05:01
CPC Classifications
F; F01; F01D; F01D21/00; F01D21/003; G; G02; G02B; G02B23/00; G02B23/24; G02B23/2476

Claims Analysis

Total Claims: 4
Claim 1
Independent Claim 355 words
A gas turbine engine including a compressor, a turbine and a casing structure extending around said compressor and turbine, an access port formed through said casing structure, a borescope probe having an elongated stem portion projecting through said access port, and means for supporting said borescope probe, said means comprising: a housing having a central opening sized to receive said borescope stem portion said housing adapted to be secured to said gas turbine casing with said central opening in general axial alignment with said casing access port; a pair of spherical bearings, each said bearing having a first portion and a second portion, each said first portion formed with a concave surface and each said second portion formed with a convex surface adapted to seat on the concave surface of its respective first portion, a central opening formed through said spherical bearings and sized to receive said borescope stem portion, said bearings disposed in said housing with said concave surfaces facing each other and said bearing central openings in general axial alignment with said housing central opening; at least one resilient deformable washer disposed between said spherical bearings and formed with an annular opening therethrough which is generally axially aligned with said bearing central openings and is sized, in a nondeformed condition, to slideably receive said borescope stem portion in close fitting relationship therewith; a locking collar threadably engaged in said housing and formed with a central opening therethrough which is sized to receive said borescope stem portion and is generally axially aligned with said housing central opening; the outer portion of one said bearing secured to said housing and the outer portion of the other said bearing secured to said locking collar, whereby when said locking collar is in a loose position, said borescope stem portion may be freely moved along and rotated about its axis and swivelled about a point intermediate said bearings and means when said locking collar is rotated in a direction of deeper threaded engagement with said housing, said resilient washer is deformed by said bearings into gripping engagement with said borescope stem portion and said bearings become frictionally locked.
Claim 2
Dependent Claim 355 words
A gas turbine engine including a compressor, a turbine and a casing structure extending around said compressor and turbine, an access port formed through said casing structure, a borescope probe having an elongated stem portion projecting through said access port, and means for supporting said borescope probe, said means comprising: a housing having a central opening sized to receive said borescope stem portion said housing adapted to be secured to said gas turbine casing with said central opening in general axial alignment with said casing access port; a pair of spherical bearings, each said bearing having a first portion and a second portion, each said first portion formed with a concave surface and each said second portion formed with a convex surface adapted to seat on the concave surface of its respective first portion, a central opening formed through said spherical bearings and sized to receive said borescope stem portion, said bearings disposed in said housing with said concave surfaces facing each other and said bearing central openings in general axial alignment with said housing central opening; at least one resilient deformable washer disposed between said spherical bearings and formed with an annular opening therethrough which is generally axially aligned with said bearing central openings and is sized, in a nondeformed condition, to slideably receive said borescope stem portion in close fitting relationship therewith; a locking collar threadably engaged in said housing and formed with a central opening therethrough which is sized to receive said borescope stem portion and is generally axially aligned with said housing central opening; the outer portion of one said bearing secured to said housing and the outer portion of the other said bearing secured to said locking collar, whereby when said locking collar is in a loose position, said borescope stem portion may be freely moved along and rotated about its axis and swivelled about a point intermediate said bearings and means when said locking collar is rotated in a direction of deeper threaded engagement with said housing, said resilient washer is deformed by said bearings into gripping engagement with said borescope stem portion and said bearings become frictionally locked.
Claim 3
Dependent Claim 22 words
The structure of claim 1 further characterized in that said apparatus includes two resilient washers and a spacer disposed between said washers.
Claim 4
Dependent Claim 32 words
The structure of claim 1 further characterized in that said apparatus includes stop means to prevent said locking collar from being threadably disengaged from said housing and overtightening of said locking collar.

References Cited (Backward Citations)

US3297022A Cited
US3690775A Cited
US3849893A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1978-11-03 1979-05-05 1979-11-04 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1982-11-03 1983-05-05 1983-11-04 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1986-11-03 1987-05-05 1987-11-04 $7700.00 Window Closed / Lapsed

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