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Parameters Screw Parameter (As Per AAMA TIR A9-14)

The document provides parameters for screw fastening including screw material properties, ply material properties, and equations to calculate allowable tension, shear, bearing, and pull-out values. It then calculates these values for a given screw-ply configuration using aluminum for both plies. A unity check is performed comparing actual loads to calculated capacities.

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0% found this document useful (0 votes)
655 views5 pages

Parameters Screw Parameter (As Per AAMA TIR A9-14)

The document provides parameters for screw fastening including screw material properties, ply material properties, and equations to calculate allowable tension, shear, bearing, and pull-out values. It then calculates these values for a given screw-ply configuration using aluminum for both plies. A unity check is performed comparing actual loads to calculated capacities.

Uploaded by

waweng22
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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PARAMETERS

Screw Parameter (As per AAMA TIR A9-14)


D  5.5mm  0.217  in Nominal Thread Diameter
24
N  Threads per inch
1in
4
FUB  600MPa  8.702  10  psi Minimum Ultimate Tensile Strength - Screw
4
FYB  450MPa  6.527  10  psi Minimum Tensile Yield Strength - Screw

KNMAX  0.1810in Maximum minor dia of internal thread


ESMIN  0.1850in Minimum pitch diameter of external thread
DSMIN  0.208in Minimum major dia of external thead
ENMAX  0.1930in Maximum pitch diameter of internal thread
Ply 1 Parameter - Fastened material
M P1  "Aluminum" Ply1 material type
4
FUP1  90MPa  1.305  10  psi Minimum Ultimate Tensile Strength - Ply1
4
FYP1  135MPa  1.958  10  psi Minimum Tensile Yield Strength - Ply1
HT1  "Normal" Hole type on ply 1
t1  3mm Thickness of ply 1
e1  12mm Edge distance for ply1
Ply 2 Parameter - Material not in-contact with screw head
M P2  "Aluminum" Ply2 material type
4
FUP2  210MPa  3.046  10  psi Minimum Ultimate Tensile Strength - Ply2
4
FYP2  160MPa  2.321  10  psi Minimum Tensile Yield Strength - Ply2

HT2  "Normal" Hole type on ply 2

t2  4mm Thickness of ply2


e2  12mm Edge distance for ply2
Allowable Tensile Stress Parameters
SF  3 Safety Factor

 FUB 
FT  min 0.75FYB  200  MPa Allowable tensile stress
 SF 
2
AS    D 
π 0.9743  2
  15.685 mm Tensile Stress Area
4  N 
2
AT  AS  0.024  in
2
AR    D 
π 1.2263  2
  13.869 mm Thread Root Area
4  N 
2
AR  0.021  in

Allowable Tension
TA  FT AT  3.137  kN Allowable Tension

TA  705.226  lbf
Allowable Shear
FT
VA1   AR  1.601  kN Allowable shear
3

VA1  360.014  lbf

tp  10mm Packing thickness


9 D
βp   0.669 Reduction due to packing; note this formula is
8  D  3  tp based on BS EN as AAMA does not have a
section for packing
VA  βp  VA1  1.071  kN Allowable shear with reduction due to packing
VA  240.82 lbf

Allowable bearing at Ply


Note: All edge distance is more than twice the diameter of the screw

PAS1  if M P1 = "Steel" Allowable bearing for Ply1

3
if t1  in
16
0.333  t1  e1  FUP1 if e1  2.7D

0.9D t1  FUP1 otherwise

2.4 D t1  FUP1 otherwise

if M P1 = "Aluminum"

0.667  D t1  FUP1 if e1  2  D

0.333  t1 e1 FUP1 otherwise

PAS1  0.99 kN

PAS2  if M P2 = "Steel" Allowable bearing for Ply2

3
if t2  in
16
0.333  t2  e2  FUP2 if e2  2.7D

0.9D t2  FUP2 otherwise

2.4 D t2  FUP2 otherwise

if M P2 = "Aluminum"

0.667  D t2  FUP2 if e2  2  D

0.333  t2 e2 FUP2 otherwise

PAS2  3.082  kN

0.5 t2
1.4  t2  D
3
PAST   FUP1 if  2.5
  t1


min VA PAS1 PAS2  otherwise

PAST  2.364  kN

PB  PAST  2.364  kN Allowable bearing


Allowable Pull-out

ATSE  π KNMAX   0.57735 ESMIN  KNMAX   8.49 mm


1
  2N
 
2

2
ATSE  0.013  in External thread stripping area

 TA SF 3 TA 3 


tm1  max   9.676  mm Minimum thickness to develop the allowable
 N ATSE FUP2 0.75 N ATSE FYP2  tension based on external threads

tm1  0.381  in

 t2 N ATSE FUP2 t2 N ATSE 0.75FYP2 


PA1  min   1.297  kN
 SF 3 3 
PA1  291.541  lbf Allowable external stripping strength

 2 N   0.57735 DSMIN  ENMAX  12.434 mm2


1

ATSI  π DSMIN

2
ATSI  0.019  in Internal thread stripping area

Steel parameter for pull-out (applicable only if ply2 is steel)

0.85 D t2  FUP2
PE   1.309  kN Thin region capacity for steel
SF
0.375in N ATSI  FUP2
PF   4.523  kN Transition region capacity
SF 3

TA SF Minimum thickness to develop the allowable


tm2s  if t2  0.25in
0.85 D FUP2 tension based on internal threads if steel

0.125TA  0.375  PE  0.25PF


 in if 0.25in  t2  0.375in
PF  PE

TA SF 3
otherwise
N ATSI  FUP2

tm2s  0.377  in

0.85 D t2  FUP2
PAS  if tm2s  0.25in
SF

  3 N ATSI  FUP2   1.7 D FUP2 


 t2  0.25in  S  3   0.375in  t2 S  if 0.25in  tm2s  0.375in
  F   F 
t2  N ATSI  FUP2
if tm2s  0.375in
SF 3

PAS  1.899  kN
Aluminum parameter for pull-out (applicable only if ply2 is aluminum)

0.665  π D FYP2 in
C1 
SF 3

2  N ATSI  FUP2 in
C2 
SF 3

TA SF Minimum thickness to develop the allowable


tm2a  if t2  0.08in
0.56 D FYP2 tension based on internal threads if aluminum

TA SF 3
if 0.08in  t2  0.125in
0.665  D FYP2

TA  0.25 C1  0.125C2
 in if 0.125in  t2  0.25in
C2  C1

TA SF 3
otherwise
N ATSI  FYP2

tm2a  0.258  in

0.85 D t2  FUP2
PAA  if tm2a  0.25in
SF

  3 N ATSI  FUP2   1.7 D FUP2 


 t2  0.25in  S  3   0.375in  t2 S  if 0.25in  tm2a  0.375in
  F   F 
t2  N ATSI  FUP2
if tm2a  0.375in
SF 3

PAA  0.269  kN
Actual force occuring on single screw
v  0.35kN Actual shear
t  0.73kN Actual tension

Summary of capacity of the screw


VA  1.071  kN Shear capacity

TA  3.137  kN Tension capacity

PB  2.364  kN Bearing capacity of both plys


PA  PAS if M P2 = "Steel"  0.269  kN Allowable pull-out capacity

PAA otherwise

Unity check
Bearing
v
RM1   0.148
PB Result1  "RM1 < 1; Therefore OK"

Pull-out
t
RM2   2.717
PA Result2  "RM2 > 1.0; revise"

Combined shear and tension


2 2
RM3  
v 
 
t 
   0.161 Result3  "RM3 < 1; Therefore OK"
 VA   TA 
As per AAMA TIR A9-14 the unity ratio is
utilizied with the shear and tension not with
the bearing and pull-out capacity (formula 7.6)

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