Abstract The disclosed invention is a device and method for optimizing the weight and/or the heat transfer (conduction) capability of a heat transfer cylindrical sleeve. The sleeve is designed to fit around a cylindrical heat source. One particular application for this invention is where the heat source is a battery such as a metal gas battery in a satellite (where weight savings is important). Two sets of functional relationships are generated showing the relationship between the thickness of the sleeve at its top and bottom, an "area factor" (which is directly proportional to its heat transfer capability), the material thermal conductivity, and its volume per unit length (which is directly proportional to its weight). One can specify the desired heat transfer capability of the sleeve and optimize (minimize) its weight. Conversely, one can specify the desired weight for the sleeve and optimize (maximize) its heat transfer capability. Assuming that the heat source has a uniform heat generating propensity along its cylindrical surface, the optimum shape for the sleeve is tapered with dimensions as described herein.
In combination, a cylindrical battery cell which generates substantially uniform amounts of heat along its cylindrical surface; and a roughly cylindrically shaped sleeve having a top and a bottom, said sleeve fitting snugly around said battery cell and having a uniformly tapered thickness along its longitudinal axis, the greatest sleeve thickness being at the bottom thereof.
Claim 2
Dependent Claim
56 words
In combination, a cylindrical battery cell which generates substantially uniform amounts of heat along its cylindrical surface; and a roughly cylindrically shaped sleeve having a top and a bottom, said sleeve fitting snugly around said battery cell and having a uniformly tapered thickness along its longitudinal axis, the greatest sleeve thickness being at the bottom thereof.
Claim 3
Dependent Claim
23 words
The apparatus of claim 1 further comprising the additional element of a base plate in intimate contact with the bottom of said sleeve.
Claim 4
Dependent Claim
18 words
The apparatus of claim 1 wherein said apparatus is situated in a spacecraft and provides electrical power therefor.
Claim 5
Dependent Claim
13 words
The apparatus of claim 1 wherein said sleeve is fabricated of aluminum alloy.
Claim 6
Dependent Claim
27 words
The apparatus of claim 1 wherein said cell comprises a pressurized container enclosing a gas as a first reactant and a metal oxide as a second reactant.
Claim 7
Dependent Claim
20 words
The apparatus of claim 5 wherein said first reactant is hydrogen and said second reactant consists of hydrated nickel oxides.
Claim 8
Dependent Claim
21 words
The apparatus of claim 5 wherein said first reactant is hydrogen and said second reactant consists of silver plus silver oxides.