Claims Analysis
Total Claims: 11
Claim 1
Independent Claim
128 words
A thermal management system for cooling electronic equipment on spacecraft, comprising: a plurality of pallets each having a radiator panel and a mounting panel, each of said radiator panels having an interior surface and an exterior surface, each of said mounting panels having a first end and a second end, said first end of said mounting panel being connected to said interior surface of said radiator panel for each of said pallets, said radiator panels of said pallets being connected end to end to enclose an interior space including said second ends of said mounting panels, said mounting panels having electronic equipment mounted thereon; and cooling means for transferring heat from said mounting panel of one of said pallets to said radiator panel of another of said pallets.
Claim 2
Dependent Claim
128 words
A thermal management system for cooling electronic equipment on spacecraft, comprising: a plurality of pallets each having a radiator panel and a mounting panel, each of said radiator panels having an interior surface and an exterior surface, each of said mounting panels having a first end and a second end, said first end of said mounting panel being connected to said interior surface of said radiator panel for each of said pallets, said radiator panels of said pallets being connected end to end to enclose an interior space including said second ends of said mounting panels, said mounting panels having electronic equipment mounted thereon; and cooling means for transferring heat from said mounting panel of one of said pallets to said radiator panel of another of said pallets.
Claim 3
Dependent Claim
37 words
The system of claim 1, wherein said cooling means includes: a closed-loop heat pipe disposed in said interior space; and heat transfer means for transferring heat between said closed-loop heat pipe and each of said radiator panels.
Claim 4
Dependent Claim
52 words
The system of claim 2, wherein said heat transfer means includes: at least one external heat pipe contacting both said radiator panel and said mounting panel of each of said pallets; and at least one internal heat pipe contacting said closed-loop heat pipe and said mounting panel of each of said pallets.
Claim 5
Dependent Claim
18 words
The system of claim 3, wherein said internal heat pipes and said external heat pipes are substantially L-shaped.
Claim 6
Dependent Claim
14 words
The system of claim 2, wherein said closed-loop heat pipe is circular in shape.
Claim 7
Dependent Claim
195 words
A thermal management system for cooling electronic equipment on spacecraft, comprising: a plurality of pallets each having a radiator panel and a mounting panel, each of said radiator panels having an interior surface and an exterior surface, each of said mounting panels having a first end and a second end and including a pair of spaced apart mounting plates, said first end of said mounting panel being connected to said interior surface of said radiator panel for each of said pallets, said radiator panels of said pallets being connected end to end to enclose an interior space including said second ends of said mounting panels, said mounting panels having electronic equipment mounted thereon; and cooling means for transferring heat from said mounting panel of one of said pallets to said radiator panel of another of said pallets, said cooling means including a closed-loop heat pipe disposed in said interior space, at least one pair of external heat pipes contacting both said radiator panel and said mounting panel of each of said pallets, and at least one pair of internal heat pipes contacting said closed-loop heat pipe and said mounting panel of each of said pallets.
Claim 8
Dependent Claim
195 words
A thermal management system for cooling electronic equipment on spacecraft, comprising: a plurality of pallets each having a radiator panel and a mounting panel, each of said radiator panels having an interior surface and an exterior surface, each of said mounting panels having a first end and a second end and including a pair of spaced apart mounting plates, said first end of said mounting panel being connected to said interior surface of said radiator panel for each of said pallets, said radiator panels of said pallets being connected end to end to enclose an interior space including said second ends of said mounting panels, said mounting panels having electronic equipment mounted thereon; and cooling means for transferring heat from said mounting panel of one of said pallets to said radiator panel of another of said pallets, said cooling means including a closed-loop heat pipe disposed in said interior space, at least one pair of external heat pipes contacting both said radiator panel and said mounting panel of each of said pallets, and at least one pair of internal heat pipes contacting said closed-loop heat pipe and said mounting panel of each of said pallets.
Claim 9
Dependent Claim
73 words
The system of claim 6, wherein: each of said internal heat pipes includes a first leg and a second leg and is substantially L-shaped; said first leg of each of said internal heat pipes is disposed in the space between said mounting plates of said respective pallet and fixed to one of said mounting plates; and said second leg of each of said internal heat pipes is fixed to said closed-loop heat pipe.
Claim 10
Dependent Claim
211 words
A thermal management system for cooling electronic equipment on spacecraft, comprising: a. a plurality of pallets each having a radiator panel and a mounting panel, each of said radiator panels having an interior surface and an exterior surface, each of said mounting panels having a first end and a second end, said first end of said mounting panel being connected to said interior surface of said radiator panel for each of said pallets, said radiator panels of said pallets being connected end to end to enclose an interior space including said second ends of said mounting panels, said mounting panels having electronic equipment mounted thereon; and b. cooling means for transferring heat from said mounting panel of one of said pallets to said radiator panel of another of said pallets, said cooling means including: at least two closed-loop heat pipes disposed in said interior space, a plurality of connector heat pipes contacting and interconnecting said closed-loop heat pipes, at least one external heat pipe contacting both said radiator panel and said mounting panel of each of said pallets, and at least two pairs of internal heat pipes, each of said pairs of internal heat pipes contacting one of said closed-loop heat pipes and said mounting panel of each of said pallets.
Claim 11
Dependent Claim
211 words
A thermal management system for cooling electronic equipment on spacecraft, comprising: a. a plurality of pallets each having a radiator panel and a mounting panel, each of said radiator panels having an interior surface and an exterior surface, each of said mounting panels having a first end and a second end, said first end of said mounting panel being connected to said interior surface of said radiator panel for each of said pallets, said radiator panels of said pallets being connected end to end to enclose an interior space including said second ends of said mounting panels, said mounting panels having electronic equipment mounted thereon; and b. cooling means for transferring heat from said mounting panel of one of said pallets to said radiator panel of another of said pallets, said cooling means including: at least two closed-loop heat pipes disposed in said interior space, a plurality of connector heat pipes contacting and interconnecting said closed-loop heat pipes, at least one external heat pipe contacting both said radiator panel and said mounting panel of each of said pallets, and at least two pairs of internal heat pipes, each of said pairs of internal heat pipes contacting one of said closed-loop heat pipes and said mounting panel of each of said pallets.