tile
initial cost and the capitalized cash value of the loss during thc useful lifc of the
turbine, where the loss is split into its components.
This problem was treated by the author for a
FT
[4.15]. In the following an attenipt is
to determine
Ku by limiting the economic aspect to the following items: a) cost
K,
due to fabrication, crection and assembly of the turbine, see (4.2-13); b) cost due to
superstructure
of power house
K,,
see (4.2-5) of one set; c) the same due to excavation,
see
(4.2- 18); d) cost due to capitalized loss, see (4.3-20-22).
-
Simplifications in the cost terms: Assuming the term
H,
+
k,
D in (4.2-5) to be
proportional to D, the cost of the power house superstructure per set is now
k,,
being a specific cost factor per unit volume.
The volume excavated per turbine has, (Fig. 4.3.1 b) and
(10.3.18), the streamwise length
k,
Dl, see (4.2-7), the depth underneath the bed
of tailwater, see (4.2-6),
d,
=
(k,
Dl
-
h,
-
d,)
$,
(d,
being the depth of tailwater bed below the lowest tailwater level,
11,'the suction head) and a width b,
=
bl D, see (4.2-8). Using the head-linked diameter
.
ratio Dl/D2 and
cf,
=
$
k,
k, D2/Dl, this value may be expressed by the rotor tip dial~leter
D (D
=
D,) as follows
I/,
=
@
D2 [k, (Dl/D2) D
-
h,
-
d,], Dl being the throat diameter.
Expressing the suction head (Cap. 8.2.) by
h,
=
B
-
NPSH
with
B
from (4.2-9), and
splitting
NPSH
according to (4.2-10) (see also Cap. 8.2), the excavation cost reads
where
Kc,,
=
cl1,,/~, Ku,
=
1i1/J2SH, and
ke,
is a specific cost factor per znit
volume.
-
Steps, to reduce the runner diameter D to the coeficient Ktc:
a)
Rated head
H
and rated discharge Q are given at the bep.
b)
The nondimensional type number
n,
results from the working data
H
and
Q
in a)
according to the state of the art, Cap. 10.3, especially with respect to
n,(H) (see
Table
9.2.1).
c)
With
n,
known, the geometry of the runner and distributor with their essential features
is also known,
i.e.: b,/D,, D,/D, in which D, is the runner tip diameter at inlet (see
Table
9.2.1), b, the inlct breadth of the runner, Dl the runner throat diameter. In the
following for
convenience D,
=
D (without ifidex).
d)
With the reservations made in Cap. 4.3.1, the angular velocity
o
of the set results from
the type number
n,,
the head
H
and the rated flow by
w
=
n,(y~)~/~/Q"~.
With
o
known, the diameter
D
as a function of Ku follows via the relation
D
=
2
u/o
as
e)
From the known relation between n,,
Ku
and Kc,,,, (Cap. 9.2) at b,/D given
I1,=
2'14
n1I2
(h2/D2)lI2
KU
KC:,';
it is also possible to exprcss Kc,, in terms of the non-
dimensional
runner inlet breadth b,!D,, given according to
c)
and hence