PSI - Issue 72
Victor Rizov / Procedia Structural Integrity 72 (2025) 128–134
131
i 1 1 1 i i z E E z
i
,
(14)
E E
z z
i 1 1
i
i
where
i i E E E , i
(15)
1 1 1 1 i i z z z .
(16)
The quantities involved in Eqs. (5) and (6) are determined by an approach similar to that defined by Eqs. (7), (8), (9), (10) and (11). The total value of J under load, F a , is estimated by q Fq J J F 2 (17) where J ( F q ) is determined by employing Eqs. (7), (8), (9), (10), (11), (12) and (13) after replacement of P with F q . The method for exploring structures under harmonic load reported by Malenov (1993) is applied in the current article. On this base, we obtain Eq. (18) for J dn under harmonic load.
(18)
dn J k J
dn Fq
where
1
,
(19)
dn k
2
1
P
30 n
,
(20)
1
.
(21)
P
m
P
Here, n is the number of revolutions of the motor per minute, δ is the displacement of point, H 3 , induced by the motor weight (Fig. 1). Equation (22) for δ is written by applying the integrals of Maxwell-Mohr (Malenov (1993)).
C 2 P
(22)
M dx i i
,
1
where κ i is the curvature, M i is the bending moment from the virtual loading, C is the spring constant (the beam is supported by springs (Fig. 1)). The total J is obtained by Eq. (23).
st dn J J J .
(23)
In fact, Equation (23) estimates J max . The minimum J is estimated by Eq. (24).
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