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19/18  Nickel batteries

              cell  container  material  thickness  would  have  to  be   demonstrate the deep depth-of-discharge (DOD) capa-
              increased to withstand the higher pressure, although it   bilities  of  the  nickel-hydrogen  system  ‘cylindrical’
              would not be a directly proportional increase because   50 Ah cell designs have been placed  on  100% DOD
              the reduction in the size of the pressure vessel increases   cycles and have  to date successfully passed  approxi-
              strength with  respect  to  internal pressure.  The prob-   mately 600 cycles. The nickel-hydrogen  battery has a
              lem results from the fact that a decrease in the volume   projected capability of  more than 600 deep discharge
              of  the  vessel  does  not  produce  an  equivalent reduc-   cycles (in excess of  70% DOD) at an energy density
              tion  in  the  surface  area  of  the  vessel.  The  projected   of  up to 70 W hkg. Representative results of  this test
              energy density for the nickel-hydrogen  system is again   are shown in Figure  19.20.
              60 W Wkg,  with  90 W Wkg  for  the  silver-hydrogen   A  low-cost  nickel-hydrogen  system  proposed  by
              system.                                     Eagle Picher is based  on the multiple cell per  single
                The  advantages  of  the  high-pressure  design  are   battery pressure vessel concept. Additional system cost
              demonstrated in  the  volume  parameters.  A  volumet-   reduction is proposed through use of standardized com-
              ric  energy  density  of  183 Wh/dm3  and  a  volumet-   ponents, ease of  manufacture and an inherent design
              ric  capacity  of  146Ah/dm3 are  achievable  with  the   versatility  able to  meet  various  voltage  and  capacity
              nickel-hydrogen  system.                    requirements with only minor modifications.
                Another approach to the design of nickel-hydrogen   Figure  19.19 shows the proposed nickel-hydrogen
              systems  involves  designs  operating  at  relatively  low   battery design. Essentially, the battery container con-
              pressure,  eliminating the  need  for  a  pressure  vessel.   sists  of  a  long cylinder  or  tube  of  a  length  selected
              Hydrogen readily reacts with certain alloys to form a   to  accommodate a desired number of  cells. The  sys-
              hydride and may be chemically stored in this fashion   tem depicted is a 10-cell 12 V battery which will yield
              rather  than  as  a  gas.  Many  metals  and  intermetallic   3 Ah capacity at an energy density projected to be in
              compounds are known to form hydrides. Compounds   excess of  55 W hkg. During assembly, the  long tube
              such  as  lanthanum  nitride  adsorb  and  desorb  large   is loaded with pre-manufactured cells spaced apart and
              quantities of  hydrogen gas under relatively low pres-   positioned by  the gas volume spacer component. The
              sures  at  room  temperature.  This  hydride  limits  the   spacer component length is selected to render sufficient
              maximum  operating  pressure  for  a  metal-hydrogen   free volume to store the reactant gas at a desirable max-
              system to approximately 0.7 kN/m2. Operation of mod-   imum pressure. The battery end-plate is of  a recessed
              ular  cells  at this  pressure  is not  only  attractive from   spherical configuration to facilitate tungsten inert gas
              a  safety  standpoint, but  permits  the  use  of  conven-   (TIG) welding of  the interface joints and to ensure a
              tional, sealed nickel-cadmium,  prismatic cell and bat-   reliable hermetic  seal. Each end-plate accommodates
              tery assembly technology.                    a single low-cost high-pressure compression seal.
                Again,  the  projected  energy  density  of  the  low-   System  versatility  could  be  greatly  enhanced  by
              pressure  cell  design  does  not  appear  to  be  as  high   grouping  the  proposed  battery  designs  into  multi-
              as  that  of  the  modular  cell  design  operating  at   ple  battery  units.  Figure  19.21  shows  a  12-battery
              3.5 N/m2.  The  lower  operating  pressure  permits  the   nickel-hydrogen  system. In this diagram, the battery
              use  of  lightweight cell  container materials; however,   has  been  wired  to  produce  36V  and  yield  12Ah
              the  weight  of  current hydride  compounds more than   capacity. Because the batteries are self-contained pres-
              compensates for this advantage. The projected energy   sure vessels, the retaining  and mounting components
              density  for  the  nickel  system  is  60 Whkg.  The
              hydride  systems  offer  an  advantage  with  respect  to
              minimizing  cell  volume  and  an  improvement  in  the   1.6
              volume parameters. The volumetric energy density of
              the  nickel-hydrogen  system  is  213WWdm3  with  a
              volumetric capacity of  170 Ah/dm3.
                Table 19.4 presents comparative data on energy den-
              sity  for  the  four  designs  of  nickel-hydrogen  sys-
              tem  discussed  above;  data  are  also  given  for  sil-
              ver-hydrogen  systems.                          0.7 k                           !
                Of  the  various  designs,  Eagle  Picher  appear  to                   600 cycles\
                                                                                                I
                                                                                        I
                                                                                I
                                                                        I
              have made most progress with the modular cylindrical   0.6 t   .   0.5   1.0   1.5   2.0
                                                                0
              design  (A in  Table 19.4). They  report  that  the  per-     Discharge (h)
              formance  recorded  for  this  type  of  nickel-hydrogen   0   1 .o   2.0   3.0   4.0
              cells  and  batteries  is  very  encouraging.  Such  sys-      Charge (h)
              tems have successfully completed thousands of cycles
              under  both  static  and  dynamic  environmental  con-   Figure 19.20 Cycling  of  50Ah  Eagle  Picher  nickel-hydrogen
              ditions,  under  both  simulated  low  Earth  orbit  and   RNH-50-3 battery, cylindrical modular design. Charge:  15A, 4 h.
                                                           Discharge:  25A,  2h.  Ambient  temperature  21°C.  100%  DOD
              synchronous  orbit  cycle  regimens.  In  addition,  to   cycles (Courtesy of Eagle Picher)
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