← Back to Patent Explorer
US3632140A Expired / Lapsed US ⏱️ 0.0 years remaining

Torsional disconnect unit

Assignee: National Aeronautics and Space Administration
•
Filing: 1970-07-31
•
Granted: 1972-01-04
•
Expires: 1990-07-31
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

Abstract A torsional disconnect unit particularly suited for use in releasably coupling distal ends of mutually displaceable, coaxially related portions of a fluid conduit, characterized by a substantially rigid tube, wound to a configuration conforming to a uniform helix and having an end thereof fixedly secured to one rotatably supported coupling component, of a pair of concentrically mated coupling components, while its opposite end rigidly is fixed against rotation. A particular feature of the invention resides in utilizing those characteristics of a helix which cause a helix to unwind, as it is elongated, in developing torque of a magnitude sufficient to overcome static friction as a mutual rotation between the components is initiated, whereby an axial separation of the components is attainable employing an axially directed force of magnitude sufficient to overcome sliding friction.

Inventors

  • 👤 Donald J Starkey
  • 👤 Kenneth C Curry

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-10 02:00
CPC Classifications
F; F16; F16L; F16L27/00

Claims Analysis

Total Claims: 5
Claim 1
Independent Claim 115 words
A torsional disconnect unit comprising: a. an elongated member having a configuration conforming to a uniform helix concentrically related to an axis of symmetry; b. a torque-actuatable, coupling component rigidly coupled to a first end of the member adapted to be rotated about said axis of symmetry; c. a support means rigidly coupled to a second end of the member adapted to be displaced relative to said coupling along a path parallel to said axis of symmetry for developing tension in said member, whereby the member responsively is deformed about the axis of symmetry for applying torque to said coupling; and d. means for inhibiting rotation of said support means about said axis of symmetry.
Claim 2
Dependent Claim 115 words
A torsional disconnect unit comprising: a. an elongated member having a configuration conforming to a uniform helix concentrically related to an axis of symmetry; b. a torque-actuatable, coupling component rigidly coupled to a first end of the member adapted to be rotated about said axis of symmetry; c. a support means rigidly coupled to a second end of the member adapted to be displaced relative to said coupling along a path parallel to said axis of symmetry for developing tension in said member, whereby the member responsively is deformed about the axis of symmetry for applying torque to said coupling; and d. means for inhibiting rotation of said support means about said axis of symmetry.
Claim 3
Dependent Claim 25 words
The unit of claim 1 wherein said member comprises a tubular conduit communicating with said coupling and adapted to accommodate a passage of fluid therebetween.
Claim 4
Dependent Claim 21 words
The unit of claim 2 wherein said coupling concentrically is seated on a nipple operatively associated with a body of fluid.
Claim 5
Dependent Claim 21 words
The unit of claim 3 wherein said support means is coupled to a second nipple operatively associated with a fluid conduit.

References Cited (Backward Citations)

US1126780A Cited
US1730022A Cited
US2449555A Cited
US2626029A Cited
US2558695A Cited
US2905194A Cited
US3211473A Cited
US3402743A Cited
US3327825A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1975-01-03 1975-07-05 1976-01-04 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1979-01-03 1979-07-05 1980-01-04 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1983-01-03 1983-07-05 1984-01-04 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag