ML19338D679
| ML19338D679 | |
| Person / Time | |
|---|---|
| Site: | Calvert Cliffs |
| Issue date: | 08/27/1980 |
| From: | ABB COMBUSTION ENGINEERING NUCLEAR FUEL (FORMERLY |
| To: | |
| Shared Package | |
| ML19260G298 | List: |
| References | |
| CEN-137(B), NUDOCS 8009230646 | |
| Download: ML19338D679 (8) | |
Text
Br;;(
qj 9.w 9f: ty rg
^
,,~c
.h; e
,~
g-
=
ca g-TCEN-137(B)
~
-r A-7.
~
- eJ
.s v.
I y
. -} ( '
-fl -
,:.I, 3 ;3 y/.
t a-3
.g;.
~
- APPENDIX'D
' s.
$$e-d A'b t-j
<3 p
. f:
,,v b.
y:
- 2:
g
- A '.
34 e
'-?.
g
- y i
-c<.
.4 f
'?.
. cdscription-of:the PROTOTYPE Test Program
-in Calvert Cliffs-I Cycle 5-9 6
w.
k u
1 f
-W
- g;
, + ' \\
4
.Y
} ' Pb '
I.' l 3
l h.
..'l -
V f
f
+
'j"'
4 g
3..
ts t
5 J
3 6
4e
-1
/f.
s
,e
- +
~
x
=-
t'"
.,_s--
4,
,a...
,e
~
r'
?c
. s.
g l'
i CRITERIA FOR PROPRIETARY lilFORMATIOil
~
Information contained in this report which is delimited by means
~
of surrounding brackets is proprietary to Combustion Engineering, Inc.
The reason for classification of. this information as proprietary to Combustion Engineering, Inc. is as follows:
, The information reveals data or material concerning Combustion
- Engineering or customer funded research or development plans or programs of substantial present or potential competitive. advantage
' -to Combustion-Engineering, Inc.
4 f.
i_ 'r y
n.
l
^l. Y,
L-o y
I, - i.; _
~
Jl3 1;-
}
?*:
~
w
- /,-
j'.g -
,o-THE PROTOTYPE DEf10hSTRAT10N ASSEMBLIES ~
I
~ !
INTRODUCTION ~
LTo further the' demonstration effort begun in SCOUT, the PROTOTYPE Program was established to irradiate a large number of' test fuel : rods for the purpose of providing statistical data. on fuel perfo'rmance of alternate high burnup fuel designs.
This process is being accomplished
.in discrete step-wise ' fashion (with SCOUT and PROTOTYPE). to potentially.
l lead-the design of future'rel.oads.
l alternate fuel designs
~
which offer high potential for extended burnop are the: primary-design concepts used in this program.
PROTOTYPE ~ consists of 4 assemblics, three of which are identical.
The assemblies will be irradiated in symmetric positions within the core
- f-PROTOTYPE Gul0ELINES
- In designing the PROTOTYPE demonstration, certain guidelines were followed which aid in a description of the demonstration:
s
, 1.
No exterior changes' were made in the fuel rods or assemblies, 6
i.e., all changes wera limited to fuel and inte,rnals of the fuel rod.
-. 2. -
Test rod locations are non-limiting.
3.
. Alternate fuel designs have the potential for improving fuel performance in~ one -or more' of the following areas:
e 6
g O
[3.'.
?
+
].l '_
4.
e Alternate fuel designs have the capability of being applicable i'
L,-
to full reloads in the. future.
.i PROTOTYPE Fuel Design 9
A PROTOTYPE. fuel design.s is the This design utilizes a standard density, with dished. and chamfered ends.
I e
2.
i L
The PROTOTYPE fuel design is the eum This pellet is of standard density and contains dished and chamfered Inds.
3.
met m
M e
e e
t O
4 pi
%.sm 4.
4 Stem t
"mun
.-=
f'_'.
m --_
n,
--s_._
~.
,,ur_
- - L
. V}i.
../
=:
. m 5;
=
sm - -
6 W
i
. PROTOTYPE Assembiies Table 1..contains the list of fuel rod types in each PROTOTYPE -
assembly. Assemblies #2, #3 and #4 are identical. Assembly #1-contains Figures 1 and.2 are assembly maps showing the location of PROTOTYPE test rods within each type of assembly.
Pin _ locations within each assembly were chosen to maximize burnup and information attainable.
at each inspection.
REFERENCE:
1.
" Irradiation of Test Fuel Rods in Calvert Cliffs-I", CEN-36 (B)lP, August 1976.,
O t
O 4-e 5
4.
L-i 8 ? j,.
s.
e 2
3 4
k h
?
9 E
e 4
y l
bme ss A
E P
Y TO 3 T
O o
4 R
P L.
n i
s s
d I
o I
R S
l 2
F e #
F u
I F
L C
f o
TR r
E e
V b
L m
A u
C N
1 T
w A
1 M
A e
R l
G b
O a
R T
P E
P YTO TO R
b P
4 E
G B
)
/
o E
/
C
'w
.5
.6 a
3
(
leu F
fo ep
.y
.T j
e r
, a
- l.
h p
J.
c
F"
< G U' rt s
w
,m A6SCH&Y loAOwC,f.AA) ENA A % Uf8ff
~
D e
S O
(
4 D
9 l
l I
l
~i
==
{ O' W
. L' i. :
i m-m k
-o :
r.
i GURr 2
J,
~
.[.
. k%CH8df boat >/AJC 'L/]t)' fog ) SS Efigut 2, 3, pp) -if, y
u i
e h
4 9
O W
e h
O l
l i
3 n