← Back to Patent Explorer
US4314449A Expired / Lapsed US ⏱️ 0.0 years remaining

Non-contacting thermal energy transfer assembly

Assignee: Lockheed Martin Corp
•
Filing: 1980-08-20
•
Granted: 1982-02-09
•
Expires: 2000-08-20
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

Abstract A thermal conducting path between a relatively movable heat source and a relatively fixed heat sink element, defined as a relatively narrow non-contacting conducting gap between opposing conducting surfaces. In an embodiment where the heat source is gimbal mounted, for movement with respect to two orthogonal axes, its conductive surface has a convex partial spherical shape while the relatively fixed surface of the heat sink element has a concave partial spherical shape. In order to maintain a constant gap, the opposing surfaces have a common spherical center located at the crossover of said orthogonal axes and the spherical radii dimensions differ by the distance of said relatively narrow non-contacting gap therebetween.

Inventors

  • 👤 Elias Reisman
  • 👤 David S. Goodsell
  • 👤 Fred S. Masino

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-09 17:55
CPC Classifications
F; F41; F41G; F41G7/00; F41G7/20; F41G7/22; F41G7/2273; F41G7/2293; F25; F25B; F25B21/00; F25B21/02; F41G7/2213; F41G7/2253; G; G01; G01J; G01J5/00; G01J5/02; G01J5/06; G01J5/061; G12; G12B; G12B15/00; G12B15/06

Claims Analysis

Total Claims: 6
Claim 1
Independent Claim 119 words
A radiation detector assembly comprising: a relatively fixed body; a thermoelectric cooler having defined hot and cold conductors; a gimbal assembly attached to said fixed body for mounting said thermoelectric cooler and detector element to provide relative movement about two orthogonal axes; a heat sink mounted within said relatively fixed body; means for transferring heat from said relatively movable hot conductor to said heat sink, which includes: a first low thermal resistivity element mounted on said hot conductor; a second low thermal resistivity element mounted within said body in contact with said heat sink; and a gaseous fluid medium having a low thermal resistivity located between said first and second elements to provide a non-contacting thermal conducting path therebetween.
Claim 2
Dependent Claim 119 words
A radiation detector assembly comprising: a relatively fixed body; a thermoelectric cooler having defined hot and cold conductors; a gimbal assembly attached to said fixed body for mounting said thermoelectric cooler and detector element to provide relative movement about two orthogonal axes; a heat sink mounted within said relatively fixed body; means for transferring heat from said relatively movable hot conductor to said heat sink, which includes: a first low thermal resistivity element mounted on said hot conductor; a second low thermal resistivity element mounted within said body in contact with said heat sink; and a gaseous fluid medium having a low thermal resistivity located between said first and second elements to provide a non-contacting thermal conducting path therebetween.
Claim 3
Dependent Claim 30 words
An assembly as in claim 1, wherein said medium is air and said first and second elements are separated by a continuously spaced gap of approximately 1 mil. (0.0254 mm).
Claim 4
Dependent Claim 23 words
An assembly as in claim 1, wherein said medium has a thermal resistivity below 10° C./watt/cm 2 between said first and second elements.
Claim 5
Dependent Claim 66 words
An assembly as in claim 1, wherein said first element has a convex partial spherical surface of a first radius having its spherical center located at the intersection of said orthogonal axes, said second element has a concave partial spherical surface of a second radius which is greater than said first radius to define a continuous space therebetween and said gaseous fluid medium occupies said space.
Claim 6
Dependent Claim 21 words
An assembly as in claim 4, wherein said medium has a thermal resistivity below 10° C./watt/cm 2 in said continuous space.

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1985-02-08 1985-08-10 1986-02-09 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1989-02-08 1989-08-10 1990-02-09 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1993-02-08 1993-08-10 1994-02-09 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag