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Definition of Screw Thread Basic Terms ………………………………………………..…26 -27

In document Ssss (Page 37-82)

Figure 3.4: Screw Nomenclature (Bhandari, 2010

The terminologies of the screw thread are defined as follows (Gupta, 2005):

(i) Pitch ()

The pitch is defined as the distance m easured parallel to the axis of the screw from a point on one thread to the corresponding point on the adjacent thread.

(ii) Lead ()

The lead is defined as the distance measured parallel to the axis of the screw that the nut will advance in one revolution of the screw.

For a single threaded screw =

For a double threaded screw =

It is the largest diameter of the screw. It is also called major diameter.

(iv) Core or Minor Diameter ()

It is the smallest diameter of the screw thread. =−

(v) Mean Diameter ()

=(+)/2 =−0.5

(vi) Helix Angle()

It is defined as the angle made by the helix of the thread with a plane perpendicular to the axis of the screw. The helix angle is related to the lead and the mean diameter of the screw.

Taking one thread of the screw and unwinding, one complete turn is developed. The thread will become the hypotenuse of a right-angled triangle with the base  and height being equal to the lead .

Figure 3.5: Unwound thread

This right-angled triangle gives the relationship between the helix angle, mean diameter and lead, which can be expressed in the following form: tan= /

Where = ℎ ℎ   ℎ ℎ.

The following conclusions can be drawn on the basis of the development of thread:

The screw can be considered as an inclined plane with  as the angle of inclination.

The load  always acts in the vertical downward direction. When the load  is raised, it moves up the inclined plane. When the load  is lowered, it moves down the inclined plane.

The load  is raised or lowered by means of an imaginary force  acting at the mean radius of the screw. The force  multiplied by the mean radius (/2) gives the torque  required to raise or lower the load. Force  is perpendicular to load .

3.4 Torque Requirement - Lifting Load

The screw is considered as an inclined plane with inclination  when the load is being raised. The following forces act at a point on this inclined plane:

Figure 3.6: Force diagram for lifting load Load : It always acts in the vertical downward direction.

Normal reaction : It acts perpendicular (normal) to the inclined plane.

Frictional force : Frictional force acts opposite to the motion. Since the load is moving up the inclined plane, frictional force acts along the inclined plane in downward direction.

Effort : The effort  acts in a direction perpendicular to the load . It may act towards the right to overcome the friction and raise the load.

Resolving forces horizontally,

=cos+sin  (3.0)

Resolving forces vertically,

=cos−sin  (3.1)

Dividing equation (3.0)  (3.1) we get:

=(cos+sin)(cos−sin) (3.2)

Dividing the numerator and denominator of the right hand side of e quation (3.2) by   we get:

=(+tan)(1−tan) (3.3)

The coefficient of friction μ can be expressed as follows:

=tan  (3.4)

Where

 = the friction angle.

Substituting (3.4) into equation (3.3),

=(tan+tan)/(1−tantan) (3.5)

=tan(+) (3.6)

The torque  required to raise the load is given by: =×/2 Whence

=[tan(+)]/2 (3.7)

3.5 Torque Requirement - Lowering Load

When the load is being lowered, the following forces act at a point on the inclined plane:

Load : It always acts in the vertical downward direction.

Normal reaction : It acts perpendicular (normal) to the inclined plane.

Frictional force : Frictional force acts opposite to the motion. Since the load is moving down the inclined plane, frictional force acts along the inclined plane in the upward direction

Figure 3.7: Force diagram for lowering load 

Effort : The effort  acts in a direction perpendicular to the load . It should act towards left to overcome the friction and lower the load.

Resolving horizontally,

 =     −     (3.8)

Resolving vertically,

 =    +      (3.9)

Dividing expression (3.8) by (3.9) we get as follows:

=(cos−sin)/(cos+sin) (3.10)

Dividing the numerator and denominator of the right hand side of e quation (3.10) by cos α:

=(−tan)/(1+tan) (3.11)

Substituting equation (3.4) into Equation (3.11),

=(tan−tan)/(1+tantan) (3.12)

Whence

 =   ( − ) (3.13)

The torque  required to lower the load is given by, =×/2 Whence

=[tan(−)]/2 (3.14)

3.6 Over Hauling and Self-Locking Screws

From equation (3.14), we know torque re quired to lower load is given by: =[tan(−)]/2 18

Case 1: When <

The torque required to lower the load becomes negative. This indicates a condition that no force is required to lower the load and the load itself will begin to turn the screw and descend down, unless a restraining torque is applied. This condition is called overhauling of the screw.

Case 2: When >

The torque required to lower the load becomes positive. Under this condition, the load will not turn the screw and will not descend on its own unless effort  is applied. This condition is called self- locking.

The rule for self-locking screw states that: A screw will be self-locking if the coefficient of friction is equal to or greater than the tangent of the helix angle.

For self-locking screw, tan≥tan

Or ≥/

Therefore, the following conclusion are made:

(i) Self-locking of the screw is not possible when the coefficient of friction (μ) is low. The coefficient of friction between the surfaces of the screw and the nut is reduced by lubrication. Excessive lubrication may cause the load to descend on its own.

(ii) The self-locking property of the screw is lost when the lead is large. The le ad increases with number of starts. For double-start thread, lead is twice of the pitch and for triple threaded screw, three times of pitch. Therefore, the single threaded screw is better than multiple threaded screws from self-locking considerations. Self-locking condition is essential in applications like screw jack (Naik, Apr 15, 2015).

3.7 Efficiency of the Square Threaded Screw

Referring to Figure 3.6: Force diagram for lifting the load ,the output consists of raising the load if the load  moves from the lower end to the upper end of the inclined plane.

Therefore,   =      ℎ   

  =   

The input consists of rotating the screw by means of an effortP.   =   

  ℎ   

 =   () The efficiency  of the screw is given by,

=    (3.15b)

This equation can also be expressed as:

=l/() (3.15c)

And

tan=/

Therefore

=tanα/  (3.15d)

Substituting for =tan (+) we get;

=tan/tan (+) (3.15e)

From the above equation, it is evident that the efficiency of the square threaded screw depends upon the helix angle  and the friction angle. The following figure shows the variation of thefficiency of the square threaded screw against the helix angle for various values of the coefficient of friction. The graph is applicable when the load is being lifted

The efficiency of square threaded screw is given by (From equation 3.15e):

=tan/tan(+) For self-locking screw ≥

Substituting the limiting value ( = ) into the equation above

≤tan/tan(+)

Substituting for tan2 into the above expression,

≤tan/(1−2)tan(2) (3.16c)

Simplifying

≤1/2(1−2) (3.16d)

From the above expression we can deduce that the efficiency of self-locking square threaded power screw is less than 0.5 or 50%. If the efficiency is more than 50%, then the screw is said to be overhauling (Gupta, 2005).

3.9 Coefficient of Friction,

It has been found that the coefficient of friction () at the thread surface depends upon the

workmanship in cutting the threads and on the type of the lubricant used. It is practically independent of the load and dependent on rubbing velocity or materials. An average of 0.1 can be taken for the coefficient of friction when the screw is lubricated with mineral oil (Gupta, 2005

Chapter 4

Designing procedure for the screw jack

4.0 introduction

The generalized adopted design procedure for screw jack to rise a load of 3500kg, mini height=200mm, max height=400mm

4.1 Design for Screw Shaft

Material specification selected for the screw shaft is plain carbon steel to British Standard specification BS 970 080M30, Hardened and Tempered, whose properties are as shown in Appendix B and the

material yield strength is 700 MPa both in tension and pure compression and 450 MPa in shear. 4.1.1 Core Diameter

The core diameter is determined by considering the screw to be under pure compression. That is;

W=

c

Ac

Where

c is pure compression stress=700mpa

Ac is cross sectional area of screw shaft=

/4(dc)

2

Dc is core diameter

There for W=

c



/4(dc)

2

dc=

(4W/



c/)

Taking factor of safety f.s=5

dc=

(4W/



c/5)

dc=

4

8583.75/

700/5)

dc=0.008835m=8.835mm

For square threads of fine series, the following dimensions of screw are selected from Appendix D (Gupta, 2005) hence,,

The core diameter dc=10mm,do=12mm,pitch p=l=2mm

 

 = tan

=0.1,

=5.71

Section of screw spindle

4.1.2 Torque required to rotate the screw

When the torque required to rotate the screw is the same to torque required lift the load is given by

T1

P

dm



W

tan



dm



dm



do

dc



12

10



11mm

tan



l



dm

2



11

0.05787

Then T1=(8583.75tan(3.31227

5.71)0.011)/2=7.496Nm

4.1.3 Screw Stresses

Compressive stresses duo to axial loads using the new c ore diameter is

c=W/Ac=W/(

dc

2/4)=4

8583.75/



0.01

2=109.29Mpa

The shear stress due to this torque using the new core diameter is given

=T1dc/2J, where J is polar moments=

dc

4/32

=16T1/

dc

3=16

7.496/



0.01

3=38.177Mpa

4.1.4 Principal Stresses

Maximum principal stress is as follows:

c max=



c



(

c)



(

)



c max=



.



.



4

3

.



7



=

c

max

=121.3068Mpa

And maximum shear stresses as follows:



max

=



c





max

=

/2



.



.



=66.66Mpa

Design value of

 is 450



=90Mpa

Cheek; those maximum shear and compressive stresses ar e less than the permissible stresses which is safe design

.

4.2 Design for Nut 4.2.1 Height of the Nut

We find the height of the nut (h) by considering the bearing pb on the nut

Pb=W/



4



do



dc



n, where n is

number of treads in contact with screwed spindle

Material specification for the nut is phosphor bronze which has tensile stress=150Mpa, compressive stress 125Mpa,shear stress=105Mpa specific bearing pressure not exceed 17Mpa and

=0.1

17



=



.



.



.



17



248.39



n

n

14.6

Say n

15

Then height of the nut is as follows;

h

n

p

15

2mm

30mm

Check:For a safe nut height ℎ ≤ 4dc

40mm

4.2.2 Stresses in the Screw and Nut Shear stress in the screw is as follows



Screw



w/

n

dc

t where t is thickness of screw

p/2

2/2

1mm



Screw



8583.75/



15

0.01

0.001

18.215Mpa

4.2.2 Stresses in the Screw and Nut Shear stress in the screw is as follow



Nut



W/

n

do

t ,8583.75/



15

0.012

0.001

15.179Mpa The given value of

 is 105/5

21Mpa

Check :These stresses are within permissible limit, hence, design for the nut is safe.

4.2.3 The outer diameter of Nut

Outer diameter of D1 is found by considering the tearing strength of the nut

t

W/



4



D1



2



do



2

t is tearing strength the nut

Tensile stress



t/f.s

150/5

30Mpa

Then we get D1 as follows

30

8583.75/

/4



D1



2



12



2

D1

22.097mm,say D1

23mm

4.2.4 The outside diameter of Collar

Outside diameter D2 is found by considering the cr ashing strength of the nut collar

c

W/



4



D2



2



D1



2

where

c is crushing strength of the nut

compressive strength



c

125/5

25Mpa

Then we get D2 as follow

25

8583.75/



4



D2



2



23



2

D2

 31.083mm,sayD2

32mm

4.2.5 Thickness of the Nut Collar

The thickness of nut collar t1 is found by considering shearing strength of the nut color

T1

 W/

D1

 is shearing strength of nut collar

105/5

21Mpa

T1

8583.75/



23

 21

5.656mm,say t1

6mm

4.3 Designs for Head and Cup

4.3.1 Dimensions of Diameter of Head on Top of Screw and for the Cup D3

ASSUMING

D3

1.75do

1.75

12mm

21mm

The seat for the cup is made equal to the diameter of the head and then chamfered at the top the cup prevents the load from rotating and is fitted with pine of diameter D4

D3/4

D4

5.25mm,say D4

6mm

Section of pin

Take length of pin to be 9mm.

Other dimensions for the cup are taken as:

Diameter at the top of the cup = Diameter of the head = 52mm Height of cup = 9mm

Thickness of cup = 3mm Fillet radii = 1mm

Figure 5.4: Section of Cup

4.3.2 Torque Required to Overcome Friction

We know that by assuming uniform pressure condition torque required to overcome friction is given as follows;

T2



W



D3



D4



D3



2



D4



2

Where D3

diameter of head

21mm

D4

diameter of pin

6mm

T2



0.1

8583.75



0.021



0.006



0.021



2



0.006



2



63.90Nm

4.3.3 Total Torque Subjected to the Handle

Total torque to which the handle is subjected is given by

T

T1

T2

T

7.496Nm

63.90Nm

71.396

Activity Professional use Domestic use

Pushing 200N (20.4kg) 119N (12.1kg)

Pulling 145N (14.8kg) 96N (9.8kg)

Table 4.2: Maximal Isometric Force by General European Working Population for Whole Body Work in a Standing Posture

Therefore taking the force of 96N in domestic use (J.J. Fereira, 2004) then the length of the handle required is

T

F

L

L

T

F

L

T/F

71.396Nm/96N

0.7437m

743.7mm, say 744mm

The length of the handle may be fixed by giving some allowance for gripping 70mm

Therefore, the length of the handle/lever is 814mm

Section of Lever

4.3.4 Diameter of Handle/Lever

The diameter of the handle/lever, D may be obtained bending effects

M



32

c

D



While

b



t



c

700/5

140Mpa

M

Force applied

length of lever

M

96N

0.7437m

71.395Nm

71.395

 

32

140

10

6

D



D

0.0173m

17.3mm,say D

18mm

4.3.5 Height of Head

The height of head is usually taken as t wice the diameter of handle.

H

2D

H

2

18mm

36mm

4.3.6 Design Check against Instability/Buckling

Effective length of screw, =  + 1/2  ℎℎ  

=1+ℎ/2 Leff 

200

30/2

215mm

When the screw reaches the maximum lift, it can be regarded as strut whose lower end is fixed and the load end is free. Therefore, buckling or critical load for this given condition is as follows (Gupta, 2005

Wcr

Ac.

y



y

4c



E

Leff 

 k



Wcr

13199.04N W

8583.75N

4.4 Design of Body

4.4.1 Dimensions for the body of the screw

The dimension of the body may be fixed and given as in shown in the figure above (Gupta, 2005)

1. Diameter of the Body at the Top

D5

1.5D2

2. Thickness of the body

3. t2

0.25do, t2

0.25

12mm

3mm 3Inside Diameter at the Bottom

D6

2.25D2 D6

2.25

32

72mm

4. Outer Diameter at the Bottom D7

1.75

D6

D7

1.75

72mm

126 5. Thickness of Base

t3

2t1, t3

2

6mm

12mm 6. Height of the Body

Height of the body

max lift

height of nut

extra50mm

200mm

30mm

70mm

300mm

Finally, the body is tapered in order to achieve stability of the jack.

4.5 Efficiency of the Screw Jack

Efficiency of screw jack is given as follows:



torque required to rotate screw with no friction

torque required out put



To

T

But To

 

W

tan



dm/2

To

8583.75

0.05787

0.011

2 To

2.732Nm

And

T

71.396Nm



To/T

2.732/71.396

0.038

3.8

4.6 result and dissection

the results I find from my project are listed as follows to design individual parts of the screw jack

1 to design body(frame) 2 to design nut

3 to design handl (Tommy bar) 4 to designs the cup

5 to design set screw 6 to design washer 7 to design screw

Dissection

RESULTES OF NUMERICAL VALUE OF THE DESIGNE

Dc 10mm LPIN 9mm D5 =48mm

Do

12mm Dhead 52mm t2 =3mm

H

30mm H cup 9mm D6 =72mm

D1

23mm tcup 3mm D7 =126mm

D2

32mm Filit raduis 1mm t3 =12mm

t1

6mm Lhandl 814mm Hbody =300mm

D3

21mm Dhandl  18mm

D4

6mm H head  36mm

4.7 CONCULUTION

From my project I am concluded that from introduction part to design analysis we are seen clearly its working principle of the screw j ack and operation of the screw jack, efficiency of this designed screw jack, methods of increasing efficiency of the screw jack. A screw jack is an example of a power screw and referred to as a mechanical device that can increase the magnitude of an effort force. Screw jacks are used for raising and lowering platforms and they provide a high me chanical advantage in order to move moderately heavy and large weights with minimum effort. Based on my calculations and assumptions the designed values are safe.

4.8 Recommendation

From the case study, I concentrated on design of a simple mechanical screw jack where the nuts fixed in a cast iron frame and remains stationary while the spindle is being rotated by the lever. This design can only work for light loads hence when a screw jack is needed for heavy load application different designs required where the nut is rotated as the spindles moves. I therefore recommend design of a screw jack for the heavy loads. I recommended that the workshops and AutoCAD rooms open in order to practice more.

)

.1 Appendix A: Mechanical Properties of Cast Iron (Nyangasi, 18 December, 2006)

6.2 Appendix B: Mechanical Properties of Steels (Nyangasi, 18 December, 2006)

CD 63 510 650 10

Key:HR - Hot- Hot rolled and normalized CD - Cold drawn

H&T - Hardened and tempered

Appendix C: Safe Bearing Pressure for Power Screws (Gupta, 2005)

Type of power screw Material Safe bearing pressure,MPa

Rubbing speed m/s

screw Nut

Hand press Steel Bronze 17.0-24.1 Low speed ,well lubricated Screw jack Steel Cast Iron 12.0-17.0 Low speed <

2.5

Screw jack Steel Bronze 11.0-17.0 Low speed < 3 Hoisting screw Steel Cast Iron 4.0-7.0 Medium speed

(6-12)

Hoisting screw Steel Bronze 5.5-10.0 Medium speed (6-12)

References

1. Ashby, M. F., 2005. Material Selection in Mechanical Design. 3rd ed. New York: Pergamon Press .

2. Bhandari, V. B., 2010. Design of Machine Elements. Third Edition ed. New Delhi: Tata McGraw-Hill Education.

3. Collection, J., 2015. hubpages.com › Autos › Automobile History. [Online] Available at:

https://www.history of screw jacks.com [Accessed 11 November 2015].

4. Fasteners, C. o., 2005. Technical Reference Guide. Ninth Edition ed. Winona, Minnesota: Fastenal Industrial & Construction Supplies.

5. Gupta, R. K. &. J., 2005. Theory of Machines. Revised Edition ed. Punjab, India: S. Chand and Company

“IF MECHANICAL AT REST

WORLED BECOMS RUST”

“MECHANICAL ENGINERING DEPARTMENT IS THE POWER OF THE WORLED”

“ THE WORLED IS NULL WITH OUT MECHANICAL

ENGINEER

In document Ssss (Page 37-82)

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