FIELD: electricity.
SUBSTANCE: invention is related to the electric engineering industry and may be used for the development and further operation of accumulators and accumulator batteries of different types in independent power supply systems of space vehicles, in particular of artificial Earth satellites (AES). The technical result consists in the reduced mismatch of capacity for separate accumulators. The set task is solved by the design of the AES accumulator battery consisting of n in-series accumulators and heat-transfer devices of a heat pipe type and incorporation of an evaporating section of heat-transfer devices into central areas of accumulator electrode units and heat contact of capacitors of the heat-transfer devices with cases of the accumulators. The claimed design of the accumulator battery for AES allows the reduction of temperature difference inside the accumulator (so called temperature gradient) thus leading to the reduced mismatch in capacity of individual accumulators.
EFFECT: increased permitted safe cycling depth, which is equal to the decreased degradation of the battery specific energy.
6 dwg
Title | Year | Author | Number |
---|---|---|---|
ACCUMULATOR STORAGE BATTERY OF SPACE VEHICLE | 2008 |
|
RU2390885C1 |
SPACECRAFT ACCUMULATOR BATTERY | 2007 |
|
RU2339125C1 |
STORAGE BATTERY WITH SELF-CONTAINED HEAT CONTROL SYSTEM | 2009 |
|
RU2394307C1 |
SPACECRAFT AT REGULAR ORIENTATION RELATIVE TO SUN | 2003 |
|
RU2264954C2 |
SPACECRAFT | 2000 |
|
RU2196079C2 |
METHOD FOR INCREASING SERVICE LIFE OF STORAGE BATTERIES ON SPACECRAFTS | 2018 |
|
RU2689887C1 |
SPACECRAFT | 2024 |
|
RU2819232C1 |
DEVICE FOR CELL-BY-CELL EQUALIZING CAPACITIES OF BATTERY-FORMING SERIES-CONNECTED NICKEL-HYDROGEN CELLS | 2005 |
|
RU2280299C1 |
SPACECRAFT | 2000 |
|
RU2192370C2 |
METHOD OF OPERATING NICKEL-HYDROGEN STORAGE BATTERY INCORPORATED WITH UNTIGHT SPACECRAFT WITH RADIATION COOLING AND SPACECRAFT TO THIS EFFECT | 2007 |
|
RU2371361C2 |
Authors
Dates
2015-04-27—Published
2013-10-23—Filed