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US4377198A Expired / Lapsed US ⏱️ 0.0 years remaining

Passive, recyclable cooling system for missile electronics

Assignee: Motorola Solutions Inc
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Filing: 1980-10-14
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Granted: 1983-03-22
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Expires: 2000-10-14
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Abstract

Abstract A cooling system is described which is appropriate to many high performance missiles. The invention comprises heat pipe/thermal diode devices, and a heat storage medium. Heat generated by electronic components of a missile is either conducted to the skin of the missile to be dissipated or is stored internally for later dissipation.

Inventors

  • 👤 John R. Welling
  • 👤 Donald L. Mattox

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-05 21:30
CPC Classifications
H; H10; H10W; H10W40/00; H10W40/70; H10W40/73; F; F28; F28D; F28D15/00; F28D15/02; F28D15/04; F28D20/00; F28D20/02; Y; Y02; Y02E; Y02E60/00; Y02E60/14

Claims Analysis

Total Claims: 10
Claim 1
Independent Claim 254 words
In an air-launched missile having a skin portion, apparatus comprising: a first shell internal to said portion of skin and defining a first space therebetween, said first shell being heat conducting; a second shell internal to said first shell and defining a second space therebetween and a third space interior to said second shell, said second shell being heat conducting; unidirectional conduction means for conducting heat from at least one heat input portion to at least one heat output portion and for preventing heat conduction from said at least one heat output portion to said at least one heat input portion, said at least one heat input portion being in intimate thermal contact with said first shell and said at least one heat output portion being in intimate thermal contact with said skin portion; means for insulating said first shell from said skin portion, said insulating means occupying at least a portion of said first space not occupied by said unidirectional conduction means; means for distributing beat, said heat distributing means comprising a plurality of heat conducting partitions extending from said second shell to said first shell and defining in said second space a plurality of closed cells; means for storing heat, said heat storing means comprising a quantity of a material having a high heat of fusion, said heat storing means occupying at least a portion of said second space in said plurality of closed cells; and electronic components occupying said third space and being in intimate thermal contact with said second shell.
Claim 2
Dependent Claim 254 words
In an air-launched missile having a skin portion, apparatus comprising: a first shell internal to said portion of skin and defining a first space therebetween, said first shell being heat conducting; a second shell internal to said first shell and defining a second space therebetween and a third space interior to said second shell, said second shell being heat conducting; unidirectional conduction means for conducting heat from at least one heat input portion to at least one heat output portion and for preventing heat conduction from said at least one heat output portion to said at least one heat input portion, said at least one heat input portion being in intimate thermal contact with said first shell and said at least one heat output portion being in intimate thermal contact with said skin portion; means for insulating said first shell from said skin portion, said insulating means occupying at least a portion of said first space not occupied by said unidirectional conduction means; means for distributing beat, said heat distributing means comprising a plurality of heat conducting partitions extending from said second shell to said first shell and defining in said second space a plurality of closed cells; means for storing heat, said heat storing means comprising a quantity of a material having a high heat of fusion, said heat storing means occupying at least a portion of said second space in said plurality of closed cells; and electronic components occupying said third space and being in intimate thermal contact with said second shell.
Claim 3
Dependent Claim 18 words
The apparatus according to claim 1 wherein said unidirectional conduction means comprises at least one heat pipe/thermal diode.
Claim 4
Dependent Claim 18 words
The apparatus according to claim 1 wherein said means for storing heat comprises a mass of an n-paraffin.
Claim 5
Dependent Claim 116 words
In an air-launched missile passive, recyclable cooling system for operation between a heat source and a heat sink comprising: heat conduction means in intimate thermal contact with said heat source for conducting heat away from said heat source, said heat conduction means defining a plurality of substantially closed cells; unidirectional conduction means in intimate thermal contact with said heat sink and said heat conduction means for conducting heat from said heat conduction means to said heat sink and for preventing the conduction of heat from said heat sink to said heat conduction means, said unidirectional conduction means being substantially independent of gravity; and heat storage means disposed in said plurality of closed cells for storing heat.
Claim 6
Dependent Claim 116 words
In an air-launched missile passive, recyclable cooling system for operation between a heat source and a heat sink comprising: heat conduction means in intimate thermal contact with said heat source for conducting heat away from said heat source, said heat conduction means defining a plurality of substantially closed cells; unidirectional conduction means in intimate thermal contact with said heat sink and said heat conduction means for conducting heat from said heat conduction means to said heat sink and for preventing the conduction of heat from said heat sink to said heat conduction means, said unidirectional conduction means being substantially independent of gravity; and heat storage means disposed in said plurality of closed cells for storing heat.
Claim 7
Dependent Claim 38 words
A cooling system according to claim 4 further comprising: insulating means separating said heat conduction means and said heat source from said heat sink for preventing the conduction of heat from said heat sink to said heat source.
Claim 8
Dependent Claim 19 words
A cooling system according to claim 5 wherein said unidirectional conduction means comprises: at least one heat pipe/thermal diode.
Claim 9
Dependent Claim 16 words
A cooling system according to claim 5 wherein said heat conduction means comprises: a metal honeycomb.
Claim 10
Dependent Claim 23 words
A cooling system according to claim 5 wherein said heat storage means comprises: a mass of material having a high heat of fusion.

References Cited (Backward Citations)

US2499736A Cited
US3613774A Cited
US3651865A Cited
US3735806A Cited
US4000776A Cited
US4057101A Cited
US4057104A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1986-03-21 1986-09-20 1987-03-22 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1990-03-21 1990-09-20 1991-03-22 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1994-03-21 1994-09-20 1995-03-22 $7700.00 Window Closed / Lapsed

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