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Asamblari Demontabile: M s2 M S

This document contains diagrams and equations for calculating stresses and moments in mechanical assemblies. It includes equations for calculating maximum stresses in shafts and couplings based on applied torques and dimensions. Design recommendations are provided such as dimension ratios and stress limits. Equations are also provided for calculating contact stresses and required surface areas in bolted and pinned connections.

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0% found this document useful (0 votes)
65 views8 pages

Asamblari Demontabile: M s2 M S

This document contains diagrams and equations for calculating stresses and moments in mechanical assemblies. It includes equations for calculating maximum stresses in shafts and couplings based on applied torques and dimensions. Design recommendations are provided such as dimension ratios and stress limits. Equations are also provided for calculating contact stresses and required surface areas in bolted and pinned connections.

Uploaded by

CostelCos
Copyright
© © All Rights Reserved
We take content rights seriously. If you suspect this is your content, claim it here.
Available Formats
Download as PDF, TXT or read online on Scribd
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ASAMBLARI DEMONTABILE 1 s m = σs2 m

ds
tf
Moment de torsiune reactiune
Arbore

Mt

D
Figura 1.47

d
Moment de torsiune actiune
Butuc

σs1 max σs2 max b)


ds
σS tf a)
Figura 1.48
σS
a)
b
D

l
d

σs 2
Mt F a F

b σs 1
F
Figura 1.49 b) M i max
2 σs 2
db F
2 Figura 1.50

Figura 1.51

F F

Figura 1.52

Freza deget

Figura 1.53.a Figura 1.53.b


h

l
b

Figura 1.54.b Figura 1.55

Figura 1.54.a Freza


disc
h

l
b

Figura 1.57 Figura 1.56


1 d 2
 2 ⋅ σ s1max ⋅ 2 ⋅ d s ⋅ 3 ⋅ d = M tc ⇒ σ s1max ≤ σ sa( stift −arbore)

 D−d D+d
σ s 2m ⋅ ⋅ds ⋅ = M tc ⇒ σ s 2m ≤ σ sa( stift −butuc) (1.39)
 2 2
 π 2
τ f ⋅ ⋅ d s ⋅ d = M tc ; τ f ≤ τ af stift
 4
ds D D
Recomandari constructive: = 0,2...0,3 ; = 2 (otel/otel); = 2,5 (fonta/otel).
d d d
 ds d
σ s ⋅ 2 ⋅ l 2 = M tc ⇒ σ s ≤ σ as min d 1
 , recomandari: s = 0,13K0,16; = 1K1,5. (1.40)
d
τf ⋅ d s ⋅ l ⋅ = M tc ⇒ τ f ≤ τ af d d
 2
2
2 ⋅ σs2 ⋅ d ⋅ b = F ⇒ σ s2 ≤ σs2a min

σ s1 ⋅ d ⋅ a = F ⇒ σs1 ≤ σs1a min

 (1.41)
F ⋅  a + b  = M Mi max
 2  4 2  i max ; σi = ≤ σai
 π ⋅ d 3b
 32
h d h
σ s ⋅ ⋅ l ⋅  ±  = M tc
2 2 4
h d
σ s ⋅ ⋅ l ⋅ ≅ M tc ⇒ σ s ≤ σsa (1.42)
2 2
d
τf ⋅ b ⋅ l ⋅ = M tc ⇒ τ f ≤ τaf
2

tf
σs2 σs
σs1

c
t2 t1
h

c
l d
Mt

Figura 1.58 D
d
Figura 1.59 M
-

Figura 1.60 Figura 1.61

σs max
σs max

Mt σs max

Mt
Mt = 0 Mt > 0 Mt > 0 Mt > 0 Mt > 0
Figura 1.62 1.63.a 1.63.b 1.63.c 1.63.d 1.62.e
Fs
L p = p max . cos n ϕ
2

µ⋅N
F
N d N

Fs pm pc
pmax
2
µ⋅N

Figura 1.64 1.65.a 1.65.b 1.65.c


D +d
rm =
2
M tc
Snec =
rm ⋅ σ as
(1.43)
D−d 
s′ = 0,75 ⋅ z ⋅  − 2⋅ c 
 2 
S nec
L nec ≥
s′
1 a 2 
2 ⋅  ⋅ σ s max ⋅ ⋅ l ⋅ ⋅ a  = M tc ⇒ σ s max ≤ σsa (1.44)
2 2 3 
µ ⋅ N ⋅ d ≥ M tc
(1.45)
M tc = k1 ⋅ k 2 ⋅ F ⋅ L
M tc
N= = Fs (1.46)
µ⋅d
3
N (1.47)
σs = ≤ σ as
b⋅d
4 3
Pentru cazul din figura 1.65 c): daca n = 1: p max = ⋅ p c ;daca n = 2: p max = ⋅ p c . 2 2
π 2 d2 + d
σs ⋅
∆b l d 22 − d 2
2 σs
S ∆a
2 2 σr

da d1 d2 d1
db d
Figura 1.67

S ∆a σt
N L 2
Fs 2
µ⋅N ∆b
F 2
d
d2
N d2 2 2 − 2⋅σs ⋅
− 2 ⋅ σs ⋅ d + d1 d − d12
2
Fa d 2 − d12 − σs ⋅
µ⋅N d − d12
2
a
A R
N Ft
Figura 1.66 Figura 1.68 Figura 1.67
 d d d
Fs ⋅  a +  − N ⋅ − µ ⋅ N ⋅ = 0 (1.48)
 2 2 2
µ ⋅ N ⋅ d ≥ M tc (conditia de ne-patinare).

N ⋅ ⋅ (1 + µ )
d
M tc 2
⇒N= ; Fs = (1.49)
µ⋅ d d
a+
2
M tc ⋅ (1 + µ)
⇒ Fs = → Cu Fs se dimensioneaza suruburile. (1.50)
µ ⋅ (2 ⋅ a + d )
N
σs = ≤ σ as (1.51)
d⋅b
Fa
p min = σs min = (1.52)
µ ⋅ π⋅ d ⋅ l
2 ⋅ Mt
p min = σ s min = (1.53)
µ⋅ π ⋅ d2 ⋅ l
R N
R = Fa2 + Ft2 ; N = ; p min = (1.54)
µ π⋅ d ⋅ l
2
 2 ⋅ Mt 
Fa2 +   (1.55)
 d 
p min = σs min =
µ ⋅π ⋅d ⋅ l
Smin = ∆d + ∆b = d a − d b (1.56)
Ka d + d 12
2
∆a = σ s min ⋅ ⋅ d; K a = − µa
Ea d 2 − d 12
(1.57)
Kb d 2 + d12
∆b = σs min ⋅ ⋅ d; K b = − µb
Eb d 2 − d12
K K 
Smin = σ s min ⋅  a + b  ⋅ d (1.58)
 Ea E b 
Smin tot = Smin + Sr + S t (1.59)
Sr = 1,2 ⋅ (R maxa + R max b ) (1.60)
St = [α b ⋅ (t b − t 0 ) − αa ⋅ (t a − t 0 )] ⋅ d (1.61)
σ t max − σ r max
= 0,5 ⋅ σ c → dupa teoria tensiunilor tangentiale (1.62)
2
4
σ t max − σ r max
= 0,75 ⋅ σ c → dupa teoria energetica (1.63)
2
d 22 + d 2
Pentru butuc: σ t max b = σ s ⋅ ; σ r max b = − σ s
d 22 − d 2
d2
Pentru arbore: σ t max a = −2 ⋅ σ s ⋅ ; σ r max a = σ s
d − d12
2

 d2 + d 2 
σ s max ⋅  2 − (− 1)
 d 2 − d
2 2
 σ (1.64)
b

= 0,5 ⋅ cb
2 cc
 d2 
σ s max a ⋅ − 2 ⋅ 2 − (1)
 d − d1
2
 σ
= 0,5 ⋅ ca (1.65)
2 cc

(
σ s max = min σ s max b , σs max a ) (1.66)
K K 
Smax = σs max ⋅  a + b  ⋅ d (1.67)
 a Eb 
E
Smax tot = Smax + Sr + St (1.68)
SSTAS
max ≤ Smax tot si SSTAS
min ≥ Smin tot (1.69)

SSTAS
max + J = α b ⋅ (t − t 0 )⋅ d ⇒ t (1.70)

SSTAS
max + J = α a ⋅ (t 0 − t ) ⋅ d ⇒ t (1.71)

µN Q
α
V
N α
ϕ
dm

σs max
σs m = σs α
Q σs max

1.71.a 1.71.b 1.71.c 1.72


Figura 1.70
l

Q = N ⋅ (µ ⋅ cos α + sin α )
2 ⋅ M tc (1.72)
N=
µ ⋅ dm
Mtc = k1 ⋅ k 2 ⋅ M t nomin al (1.73)
N
σs = ≤ σ sa (1.74)
π ⋅d m ⋅ l
M tc = K1 ⋅ K 2 ⋅ M tn
2 ⋅ M tc N
N= ; σs = ≤ σ sa (1.75)
µ⋅d π ⋅ d ⋅l
Fa1 = N ⋅ [tg(α + ϕ1 ) + tgϕ] (1.76)
E ⋅S
Fa 0 = ⋅ ∆l r (1.77)
l0
∆l r
tg(α + ϕ1 ) = (1.78)
∆l a

2⋅E⋅
(
π⋅ D2 − d 2 )
Fa 0 = 4 ⋅ ∆l a ⋅ tg(α + ϕ1 ) (1.79)
D+d
4
d
σ sm ⋅ π ⋅ d ⋅ l ⋅ µ ⋅ = M tc (1.80)
2
5
µ

µ1 N

µN
Fa1
σs

D
d
α
l N ϕ1
α N′
Figura1.76

µN′
H′ = N⋅(µ1⋅cos α +sin α)

Figura 1.73

1 1 1
M t1 ⋅ M t1 ⋅ M t1 ⋅ M t1 K
4 4 8
Figura 1.74 Figura 1.75

d D
l
d

σs max
Figura 1.77 Figura 1.78 Figura 1.79

Tabelul 1.2
σc σR Alungirea la
Marca STAS Tipuri de arcuri
[MPa] [MPa] rupere, A%
OLC 55A 880 1080 6 lamelare, cu foi, spirale
795-80
OLC 65A 780 980 10
OLC 75A 880 1080 9 lamelare, cu foi, spirale, elicoidale
OLC 85A 980 1130 8
51 Si 18A 1080 1180 cu foi, elicoidale
795-80
56 Si 17A 1270 1480 6 cu foi, elicoidale, disc, inelare
60 Si 15A 1080 1270
51 VCr 11A 1180 1320 cu foi, elicoidale, disc, inelare, bara de torsiune
61 Si 2 WA 11514-80 1668 1864 5 elicoidale, bara de torsiune
40 Cr130 3583-80 1250 1650 − elicoidale
12 TiNiCr 180 11523-80 1450 1650 − elicoidale
F F F F F
- l M
(M) (M) (M) (M) (M)

f f f f f Mt
arcuri metalice arcuri metalice arc disc arcuri metalice arcuri din
θ de înaltimiθ arc θ cu foi θ cauciuc θ
d θ
(Hooke) θ
diferite spiral (histerezis) (histerezis)
1.80.a 1.80.b 1.80.c 1.80.d 1.80.e 1.81.a 1.81.b
dF dM
c= sau c = (1.81)
df dθ


L = F ⋅ df sau L = M ⋅ dθ ∫ (1.82)
L
kv = (1.83)
V
6
L
ku = V , pentru solicitarea de torsiune, sau
τ 2max
G (1.84)
L
ku = 2 V , pentru solicitarea de încovoiere sau de tractiune-compresiune.
σ max
E
G
ku = kv ⋅ , pentru solicitarea de torsiune, sau
τ 2max
(1.85)
E
ku =kv ⋅ , pentru solicitarea de încovoiere sau de tractiune-compresiune.
σ 2max
Lh = L − L′ (1.86)
L′ L
η= =1 − h (1.87)
L L
L − L′ 1 − η
δ= = (1.88)
L + L′ 1 + η
Mt
τt = ≤ τ at (1.89)
Wp
M t ⋅ l 32 ⋅ M t ⋅ l
θ= = (1.90)
G ⋅ Ip π ⋅ G ⋅d 4
π ⋅d 4 ⋅ G
c= (1.91)
32 ⋅ l
2
 π 3 

L=
Mt ⋅ θ
=
M 2t ⋅l
=
(Wp ⋅ τ at )
2
⋅l
=
 ⋅ d ⋅ τ at  ⋅ l
 16  (1.92)
2 2 ⋅ G ⋅ Ip 2 ⋅ G ⋅ Ip π ⋅d
4
2⋅G⋅
32
2
τ t max
L = 0,25 ⋅ ⋅V (1.93)
G
16 ⋅ M t π ⋅ d4 ⋅ θ ⋅G
d nec = 3 sau l nec = (1.94)
π ⋅ τa t 32 ⋅ M t
F
caneluri F1 F2 Fb
F

f1
t; t 0 d
f2
Dm fb
H0 H1 H2 Hb

f
Figura 1.82
Figura 1.83
F

F·cos
a
a
tt
F·sina
Dm
k·t t
Figura 1.84 Figura 1.85
F ⋅ cos α ⋅ D m
Mt = (1.95)
2
F ⋅ sin α ⋅ D m
Mi = (1.96)
2
7
F⊥ = F ⋅ cos α (1.97)
FN = F ⋅ sin α (1.98)
M t 8 ⋅ F ⋅ Dm
τt = = (1.99)
Wp π ⋅d3
F 4⋅ F
τf = = , (1.100)
A π ⋅ d2
4 ⋅ F  Dm  4⋅ F
⋅ (2 ⋅ i + 1) , unde: i = m este indicele arcului (raportul de înfasurare)
D
τ= ⋅ 2 ⋅ + 1 = (1.101)
2  2
π ⋅d  d  π⋅ d d
8 ⋅ F⋅ i
τ = τt = (1.102)
π ⋅ d2
τ max = k ⋅ τ (1.103)
i + 0,5
k= (1.104)
i − 0,5
8⋅ k ⋅D m ⋅ F 8⋅ k ⋅i ⋅ F
τ max = = ≤ τa (1.105)
π ⋅ d3 π ⋅ d2
8 ⋅ k ⋅ F⋅ i
d nec ≥ ; cu D m = i ⋅ d (1.106)
π ⋅ τ at
Dm M ⋅l
f = ⋅ θ; θ = t (1.107)
2 G ⋅ Ip

8 ⋅ F ⋅ i3 ⋅ n
f = (1.108)
G⋅d
G ⋅ d4
c= (1.109)
8 ⋅ n ⋅ D 3m
f ⋅ G ⋅ d4
n= (1.110)
8 ⋅ D 3m ⋅ F
F⋅ f
W= (1.111)
2
π ⋅ d 3 ⋅ τa
F= (pentru k = 1)
8⋅ D m
(1.112)
π ⋅ d 2 ⋅ τa
F= (pentru k real )
8 ⋅ k ⋅ Dm
Dm
F⋅ ⋅ π ⋅ Dm ⋅ n
M ⋅ π ⋅ Dm ⋅ n 2 π ⋅ n ⋅ D 2m ⋅ F (1.113)
f = t = =
G ⋅ Ip G ⋅ Ip 2 ⋅G ⋅ Ip

 0,25  τ 2
W =  2  ⋅ max ⋅ V (1.114)
 k  G

F F

Figura 1.86 1.87.a 1.87.b 1.87.c 1.87.d


6 ⋅ F⋅ l
σ i max = ≤ σ ai (1.115)
b⋅h2
M 6 ⋅F ⋅l
σ i max = max = ≤ σa i (1.116)
Wz b ⋅ h2
Mx F⋅x F⋅ l
σi x = = = = σ i max
Wz x x Wz (1.117)
Wz ⋅
l
b x ⋅ h 2x x b⋅h2 x
Wz x = = Wz ⋅ = ⋅ (1.118)
l l 6 l

b x = b 0 + (b − b 0 )⋅
x
(1.119)
l
6 ⋅ F⋅ l
S nec =
3  b (1.120)
  ⋅σa i
h
8
(1.121)
F ⋅ l3 b ⋅ h3
f1 = ; Iz = (figura 1.78.a)
3⋅ E ⋅ Iz 12 l
F ⋅ l3
f2 = ; f 2 > f1 (figura 1.78.b)
2⋅ E ⋅ Iz b F

f3 =
F ⋅l

(
3 ⋅ 3 ⋅ β − 4 ⋅ β + 2 ⋅ β ⋅ ln β
3 2 2
)
; (figura 1.78.c) a) F
2 ⋅ (1 − β )3
3⋅ E ⋅ Iz h

f 2 > f 3 > f1
2
1 σ i max l
L1 = ⋅ ⋅ V;
18 E
2 b F
1 σ i max
L2 = ⋅ ⋅ V; (1.122)
6 E F
( )
b)
1 3 ⋅ β 2 − 4 ⋅ β + 1 − 2 ⋅ β 2 ⋅ ln β σ 2i max h
L3 = ⋅ ⋅ ⋅V
2 ⋅ (1 − β ) ⋅ (1 + β )
6 3 E
l
Ee = k e ⋅ E (1.123)

F (M) F b F b0
energie disipata prin frecari 1 2 3
încarcare
interne (max 40%)
c) F
h

descarcare
f (?) f
Figura 1.89 Figura 1.90 Figura 1.88
F
f β
a) dupa încarcare, sub sarcina F = ct;
b) dupa îndepartarea sarcinii.
a)
h 10
b)
timp
5
Figura 1.91 a
5 10 a/h
Figura 1.92 F Figura 1.93
A
F= E ⋅ ⋅f (1.124)
h
A a
F = β ⋅ E ⋅ ⋅ f , unde β = f   cu variatia prezentata în figura 1.93 (1.125)
h h
F F f
τf = = γ ⋅ G; γ = tgγ = (1.126)
A A⋅ G s

f
?
F
s

Figura 1.94

Figura 1.95 Figura 1.96

Figura 1.97

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