TrolleyStructuralAnalysisExhibit08-06-13.pdf

PDF 2 MB Posted Sep 9, 2014

Attached to: Fall Restraint System
Solicitation number: F2VAGS4217AW02
Issued by: Department of the Air Force Air Mobility Command

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From the source

Structural Analysis for Hangar 1 2 - applicable to Hanger 3 and Fuel Cell Hanger

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Job Title

Client

Job No Sheet No Rev

Part

Ref

By Date Chd

File Date/Time

BSStructProp2 1

MacDill AFB Fall Protection System

GS-06 USAF HAF 6 MXS/CCR

TS 30-Jul-13

06-Aug-2013 23:02Trolley Beam.std

Print Time/Date: 06/08/2013 23:38 Print Run 1 of 3STAAD.Pro V8i (SELECTseries 3) 20.07.08.22

Job Information Engineer Checked Approved

Name: TS

Date: 30-Jul-13

Comments

This model is to simulate the various service loads and resulting member capacities for an existing Trolley Beam Fall Protection System.

Structure Type SPACE FRAME

Number of Nodes 34 Highest Node 35

Number of Elements 28 Highest Beam 38

Number of Basic Load Cases 4

Number of Combination Load Cases 0

Included in this printout are data for:

All The Whole Structure

Included in this printout are results for load cases:

Type L/C Name

Primary 1 5KIP SERVICE LOAD EVENLY SPACED

Primary 2 5KIP GANG SERVICE LOAD NORTH END

Primary 3 5KIP GANG SERVICE LOAD MIDDLE OF

Primary 4 5KIP GANG SERVICE LOAD SOUTH END

Nodes Node X

(in)

1 0.000 0.000 0.000

2 600.000 0.000 0.000

3 60.000 0.000 0.000

4 120.000 0.000 0.000

5 180.000 0.000 0.000

6 240.000 0.000 0.000

7 300.000 0.000 0.000

8 360.000 0.000 0.000

9 420.000 0.000 0.000

10 480.000 0.000 0.000

11 540.000 0.000 0.000

12 150.000 0.000 0.000

14 450.000 0.000 0.000

15 -36.000 84.000 -36.000

16 -36.000 84.000 36.000

Client

Job No Sheet No Rev

Part

Ref

By Date Chd

File Date/Time

BSStructProp2 2

MacDill AFB Fall Protection System

GS-06 USAF HAF 6 MXS/CCR

TS 30-Jul-13

06-Aug-2013 23:02Trolley Beam.std

Print Time/Date: 06/08/2013 23:38 Print Run 2 of 3STAAD.Pro V8i (SELECTseries 3) 20.07.08.22

Nodes Cont...

Node X

(in)

17 150.000 180.000 -120.000

18 150.000 180.000 120.000

19 300.000 180.000 -120.000

20 300.000 180.000 120.000

21 450.000 180.000 -120.000

22 450.000 180.000 120.000

23 636.000 144.000 -36.000

24 636.000 144.000 36.000

25 0.000 9.000 0.000

26 150.000 9.000 0.000

27 300.000 9.000 0.000

28 450.000 9.000 0.000

29 600.000 9.000 0.000

30 390.000 0.000 0.000

31 375.000 0.000 0.000

32 30.000 0.000 0.000

33 45.000 0.000 0.000

34 570.000 0.000 0.000

35 555.000 0.000 0.000

Beams Beam Node A Node B Length

(in)

Property (degrees)

11 15 25 90.648 1 180

12 16 25 90.648 1 180

13 17 26 208.904 1 180

14 18 26 208.904 1 180

15 19 27 208.904 1 180

16 20 27 208.904 1 180

17 21 28 208.904 1 180

18 22 28 208.904 1 180

19 23 29 144.281 1 180

20 24 29 144.281 1 180

21 1 32 30.000 2 0

22 3 4 60.000 2 0

23 4 12 30.000 2 0

24 12 5 30.000 2 0

25 5 6 60.000 2 0

26 6 7 60.000 2 0

27 7 8 60.000 2 0

28 8 31 15.000 2 0

29 9 14 30.000 2 0

30 14 10 30.000 2 0

Client

Job No Sheet No Rev

Part

Ref

By Date Chd

File Date/Time

BSStructProp2 3

MacDill AFB Fall Protection System

GS-06 USAF HAF 6 MXS/CCR

TS 30-Jul-13

06-Aug-2013 23:02Trolley Beam.std

Print Time/Date: 06/08/2013 23:38 Print Run 3 of 3STAAD.Pro V8i (SELECTseries 3) 20.07.08.22

Beams Cont...

Beam Node A Node B Length

(in)

Property (degrees)

31 10 11 60.000 2 0

32 11 35 15.000 2 0

33 30 9 30.000 2 0

34 31 30 15.000 2 0

35 32 33 15.000 2 0

36 33 3 15.000 2 0

37 34 2 30.000 2 0

38 35 34 15.000 2 0

Section Properties Prop Section Area

(in2)

Iyy

(in4)

Izz

(in4)

Material

1 L40408 3.750 8.828 2.295 0.323 STEEL

2 TROLLEYSECTION 19.244 78.690 859.501 1.548 ALUMINUM

Materials Mat Name E

(kip/in2)

Density

(kip/in3)

(/°F)

1 STEEL 29 E +3 0.300 0.000 6 E -6

2 STAINLESSSTEEL 28 E +3 0.300 0.000 10 E -6

3 ALUMINUM 10 E +3 0.330 0.000 13 E -6

4 CONCRETE 3.15 E +3 0.170 0.000 5 E -6

Supports Node X

(kip/in)

(kip/in) rX

(kip-ft/deg) rY

(kip-ft/deg) rZ

(kip-ft/deg)

15 Fixed Fixed Fixed Fixed Fixed Fixed

16 Fixed Fixed Fixed Fixed Fixed Fixed

17 Fixed Fixed Fixed Fixed Fixed Fixed

18 Fixed Fixed Fixed Fixed Fixed Fixed

19 Fixed Fixed Fixed Fixed Fixed Fixed

20 Fixed Fixed Fixed Fixed Fixed Fixed

21 Fixed Fixed Fixed Fixed Fixed Fixed

22 Fixed Fixed Fixed Fixed Fixed Fixed

23 Fixed Fixed Fixed Fixed Fixed Fixed

24 Fixed Fixed Fixed Fixed Fixed Fixed tsizemore Text Box Wire Model for Trolley Beam and Super Structure

Rendered Isometric View of Whole Structure

Rendered Straight On View of Whole Structure

Rendered View Down the Section Axis

Three Individual 5 Kip Loads applied at even intervals tsizemore Oval tsizemore Oval tsizemore Oval

Oval

Three 5 Kip Gang Loads applied at North End of Trolley Beam tsizemore Oval

Three 5 Kip Gang Loads applied at Middle Section of Trolley Beam tsizemore Oval

Three 5 Kip Gang Loads applied at South End of Trolley Beam tsizemore Oval

Resulting Max Nodal Displacement from the 5 Kip Gang Load Applied at the North End: 0.416 inches at Node 32 tsizemore Oval tsizemore Text Box Node 32 tsizemore Oval

Max Super Structure Support Reactions. All are well within Max Allowable.

Max Super Structure Principal Member Stresses. Happens in Angle 11 Resulting from 5 Kip Gang Load at North End.

tsizemore Oval tsizemore Oval tsizemore Oval tsizemore Text Box Max Tension Stress tsizemore

Max Compressive Stress

Max Trolley Beam Principal Member Stresses. Happens in Member 12 Resulting from 5 Kip Gang Load at North to Middle Section.

tsizemore Oval tsizemore Oval tsizemore Oval tsizemore Text Box Max Tension Stress tsizemore

Max Compressive Stress

Max Trolley Beam Von-Mis Member Stresses. Happens in Solid 54. Resulting from 5 Kip Gang Trolley Load Applied at a Mid Span Between Supports tsizemore Oval tsizemore Oval tsizemore Oval

Max Trolley Beam Von-Mis Member Stresses. Happens in Solid 54. Resulting from 5 Kip Gang Trolley Load Applied at a Mid Span Between Supports.

Underneath View.

tsizemore Oval

Amplified Center Trolley Beam Deflection Resulting from 5 Kip Gang Trolley Load Applied at Mid Span of Center Section.

tsizemore Oval tsizemore Oval

File details come from the government source that posted it. Updated Nov 14, 2017.