Esercizi rotismi 1

1

DAT resist.

CA

W3 0 2C copple

= , -

WB Zad/5 10

so 2A Nm

= =

Cc 15Nm 74 32

Z2

= =

20

= &

0

45 m

= 1 amm 20

=

= =

?

?

· Wa We &

ORDINARI

ROTISMI : 3

5-4 2

1-2-3

EPICLOIDALI

ROTISMI : .

. .

3 SATETTITI

SOLARI 5 2 4

1 :

: . .

. ()()

WB 2

IwF -

= 4128

-0

· : .

W1-

IWF-WB-R

wS-2 -5 424

7

= 1

w1

[wc W5

WB

- wa =

=

= ,

/

23 Z5

e

acavo R5-R4

R1 R3-R2

R2 =

+ =

↳ 97

z3 24

22

ES

109 21 =

21 222 + +

=

+ :

= =

== Zad/5

168 = wa

Ing =

wF & 574 8 2ad/5

= wa

W1 = =

,

%

CB

· CA CBWB Ca

+

WA O

+ =

WC

- - - - - - -

~ &

& O & 8

/ccwcl

CAwAl

I Nm

+ 165 4

CB =

= ,

WB

?

F23

· sistema

equilibrio rotazione

C3

ricavo da .

Assumo positivo

C3

C

E -[3

++ = 0 -140

13

+ Nre

4

= ,

3

zuota

Q23 : 131 1298N

Q23 :

* ,

A R23 of 71

Q23 + 468

R23 80 = ,

=

c3 Q232 R232 ON

F23 737

=

+

= DAT I 45

21 Z2 Z3 38

20 =

= =

24

= 20 25

4 = =

4002ad/s 200Nm

(C =

wa = 20

8

10mm

m = =

concord

WB

wa e

Caresistante

?

wa

·

ROTISMI ORDINARI 1-2

: 3-4-5-6

EPICICLOIDALI

ROTISMI : 5

3 4

6 SATELLITE

:

SOLARI : .

. --w2

= 2ad/

7

772 -266

= ,

1

W L

(W3 WI

= ()

Wor

Tw = .

(26 82)

75 5562

24

23 Iw

>

- = + -0

+ = - = ,

CwA Wal

WG

R =

= , 72ad/5

770

Iw(w3-Wal Wa-WA-wc

= = ,

?

F34

· (2951stemte)

= Nm

200

-

zuota 6

QSG &

↑ RSG · ·

RCx E 487 8N

asG :

* : .

A C C

& 4

Satelliti

eg

. S

G

Q

&

ROS R5

QGS &Q34

Q34 R4

= =

. .

R34 +

Q34 go

=

4

5 Q34 Q342

K34

F34 623N

= +

* =

↑ R 34 I

DAT CB

Tad/5

150 65Nme

wa = = Z5 95

55 Z2

2 24 38

22 =

= = = 20

0

23

Z6 10mm :

= =

m

resistente

↳ B coppia

?

WB

· 27

23 e

acavo R3

RI R4 39

=

R2