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US4569710A Expired / Lapsed US ⏱️ 0.0 years remaining

Process for manufacturing the inner tube element for a double tube coring apparatus

Assignee: DB STRATABIT Inc
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Filing: 1983-12-09
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Granted: 1986-02-11
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Expires: 2003-12-09
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Abstract

Abstract The invention relates to a process for manufacturing an inner tube element made of synthetic resin for a double tube coring apparatus provided for deep boring. The tube element is provided with coupling nipples for connecting it to other inner tube elements. Fibers coated with synthetic resin are wound helically onto a cylindrical mandrel so as to overlap each nipple. This process gives the tube element a higher strength than that of glued nipples.

Inventors

  • 👤 Honore J. Lambot
  • 👤 Johannes H. M. Fliervoet
  • 👤 Pieter Kramer

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-30 10:41
CPC Classifications
E; E21; E21B; E21B25/00; E21B25/005; B; B29; B29C; B29C70/00; B29C70/04; B29C70/28; B29C70/30; B29C70/32; B29C70/68; B29C70/86; E21B25/06; B29L; B29L2023/00; B29L2023/22; B29L2031/00; B29L2031/748; B29L2031/75; F; F17; F17C; F17C2209/00; F17C2209/21; F17C2209/2154

Claims Analysis

Total Claims: 2
Claim 1
Independent Claim 232 words
Process for manufacturing an inner tube element (1) for a double tube coring apparatus, said element consisting of a rigid tube length (2) having a substantially constant section, made of synthetic resin and provided with couplings (3, 4) for connecting it to other inner tube elements, in which process at least one metallic nipple (3) is placed onto a cylindrical winding mandrel (11) at a predetermined axial position corresponding to the length of tube element to be manufactured, a part of said nipple (3) having an inner diameter substantially identical to the diameter of the mandrel (11) and having a rough surface (14), and fibers (16) coated with a synthetic resin are wound helically onto said cylindrical mandrel (11) so as to overlap the rough surface (14) of said nipple (3) the process being characterized by the further steps of providing said nipple (3) both with a gripping ring (13), and helically winding the fibers (16) onto the mandrel (11) and onto the gripping ring (13) in order to allow the tube element to withstand axial tensile stress in a double tube coring apparatus, and also with an annular shoulder (25) with which the threaded portion of a connected inner tube element comes in abutment when the nipple is screwed home and on which the resin body of said connected inner tube element may rely in order to resist axial compression stresses.
Claim 2
Dependent Claim 232 words
Process for manufacturing an inner tube element (1) for a double tube coring apparatus, said element consisting of a rigid tube length (2) having a substantially constant section, made of synthetic resin and provided with couplings (3, 4) for connecting it to other inner tube elements, in which process at least one metallic nipple (3) is placed onto a cylindrical winding mandrel (11) at a predetermined axial position corresponding to the length of tube element to be manufactured, a part of said nipple (3) having an inner diameter substantially identical to the diameter of the mandrel (11) and having a rough surface (14), and fibers (16) coated with a synthetic resin are wound helically onto said cylindrical mandrel (11) so as to overlap the rough surface (14) of said nipple (3) the process being characterized by the further steps of providing said nipple (3) both with a gripping ring (13), and helically winding the fibers (16) onto the mandrel (11) and onto the gripping ring (13) in order to allow the tube element to withstand axial tensile stress in a double tube coring apparatus, and also with an annular shoulder (25) with which the threaded portion of a connected inner tube element comes in abutment when the nipple is screwed home and on which the resin body of said connected inner tube element may rely in order to resist axial compression stresses.

References Cited (Backward Citations)

US2628822A Cited
US3092192A Cited
US3661670A Cited
GB1356353A Cited
US3768842A Cited
US3874465A Cited
US4368124A Cited
US4238539A Cited
US4289557A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1989-02-10 1989-08-12 1990-02-11 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1993-02-10 1993-08-12 1994-02-11 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1997-02-10 1997-08-12 1998-02-11 $7700.00 Window Closed / Lapsed

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