AD-AO83 498 NAVAL WEAPONS CENTER CHINA LAKE C A FIG/ 7STRESS ANALYSIS OF THE EXTERNA L STORES OP EJECTION LAUNCHER/INN-ETC(U)

UN A .. D NOV 78 A L FREEMAN. E R HANBLE4, 8 A PAXTON

UNCLASSIFIED NW-T356 GIDP402365M

mmmmmmmmm

NWC Technical Memorandum 3358/

w~j STRESS kjNALYSIS OF THE EXTERNAL/9 /v'-STORES DFEJECTION LAUNCHER/

V41INNER TME SUBSYSTEM.

=by/r

;Anthony L. /FreemanEarl R. Hanblem

*Gale W. Paxton'--rh-3n---e1-n-gDi ifs ionCOMARCO INC.

for thePropulsion Systems DivisionOrdnance Systems Department

ft Nov 7 8

' APR 19580 K

0 Ac eS S;iLn ForNTIS QG,..ak&

DDC TAB

JUStific~tion

NAVAL WEAPONS CENTERChina Lake, California B ____

Aai Ianid/ol.

-;Dist spec

DISTRIBUtMON STATEMN A

alllaC.) Approved for public rele"Distributim ni_(fhmll4_ __ _ _ __ _ _ _

OMB MO. 22-111336

GOVERNMENT-INDUSTRY DATA EXCHANGE PROGRAM

GENERAL DOCUMENT SUMMARY SHEET 1

Plo.* Type All nom.on -n As toe ononfto

. ACCESS NUMBR 2. COMPONEN/PAR NAME PFR GIDEP SUBJECT NE$AURUS

EI40-01:3405 Mechanical Assemblies, Launcher, Rocket3. APPLICATION . MFR NOTIFICATION 5 DOCUMENT ISSUE

Engineering D NOTIFIED NOT APPLICABLE November 19786 ORIGINATOR'S DOCUMENT TITLE7 DOCUMENT TYPE

Stress Analysis of the External Stores DP Ejection E-] G

EN RPT [] NONSTD PART []SPECLauncher/Inner Tube SubsyRt

IM8. ORIGINATOR'S DOCUMENT NUMBER 9. ORtGINAOR'S PART NAME/IDENTIFICATtON

NWC TM 3358 N/A10. DOCUMENT (SUPERSEDES, ISUPPLEMENTS' ACCESS NO. I. ENVIRONMENTAL EXPOSURE CODES

None N/A12. MANUFACTURER 13. MANUFACTURER PART NUMBER 14. INDUSTRY/GOVERNMENT STANDARD NUMBER

N/A N/A15. OUTLINE, TABLE OF CONTENTS. SUMMARY. OR EQUIVALENT DESCRIPTION

I

The contents of this report are the results of a stress analysisconducted on the critical areas of the DP Ejection Launcher Inner TubeSubsystem. It was determined that the hardware and/or assembliesexperiencing the critical load conditions were the tube, power cylinderassembly, detent assembly, warm cable cutter assembly, plumbing fittingsand tubing. The stress analyses on these components and subsystems arepresented on the following pages in the form of mathematical calculationsand accompanying sketches without explanatory text. The drawings inIjgures 1-5 (pages 50-54) show how the components relate to the overallsystem and give more detail on the items tested.

DTIC, i ;_ECTE

APR 2 5 1980.

T -

C

79 09 24 292

,6. KEY RORDS FOR INDEXING

Stress Analysis; Inner Tube Subassembly; Safety Factors; External Stores (Doc Des--P)17. GIDEP REPRESENTATIVE 11R PARTICIPANT ACTIVITY AND CODE

M. H. Sloan Naval Weapons Center, China Lake, CA (X7-D .. 2000REPRODUCTION OR DISPLAY OF THIS MATERIAL FOR2000 SALES OR PUBLICITY PURPOSES IS PROHIBITED

L ' I l II " I.. I " i_-zm.

NWC TH 3358

CONTENTS

Introduction ........................................................ 3

Abbreviations and Symbols ........................................... 4

1.0 Tube ........................................................... 6

2.0 Power Cylinder Assy ............................................ 7

t.2.1 Cylinder Wall ............................................. 72.2 Threaded Cylinder Heads ................................... 102.3 Traction Rod .............................................. 132.4 Threaded Hole, Piston End ................................. 152.5 Pin, Rod End .............................................. 152.6 Rod End ................................................... 162.7 Cap, Cylinder ............................................. 172.8 Bracket, Cylinder ......................................... 192.9 Mounting Screws, Bracket .................................. 20

3.0 Warm Cable Cutter Assy ......................................... 233.1 Piston Housing ............................................ 233.2 Fasteners, Piston Closure ................................. 25

4.0 Detent Assy .................................................... 274.1 Detent Pin ............................................... 274.2 Cover ..................................................... 284.3 Fasteners, Cover .......................................... 294.4 Housing ................................................... 304.5 Fasteners, Mounting ....................................... 34

5.0 Lockout Bar ................................................... 38

6.0 Plumbing Lines ................................................. 40

7.0 Pipe and Tube Fittings ......................................... 42

8.0 Summary ...... ................................................. 45

1

.3

NWC TM 3358I

Figures:1. DP Launcher Inner Tube Actuation System Diagram ............. 502. DP Launcher Assy ............................................ 513. DP Power Cylinder Assy ...................................... 524. DP Warm Cable Cutter ........................................ 535. DP Detent Assy .............................................. 54

Tables:8.1 Mechanical Properties Table ................................ 468.2 Data Summary Table ......................................... 47

2

NWC TH 3358

INTRODUCTION

The contents of this report are the results of a stress analysisconducted on the critical areas of the DP Ejection Launcher Inner TubeSubsystem. It was determined that the hardware and/or assembliesexperiencing the critical load conditions were the tube, power cylinderassembly, detent assembly, warm cable cutter assembly, plumbing fittingsand tubing. The stress analyses on these components and subsystems arepresented on the following pages in the form of mathematical calculationsand accompanying sketches without explanatory text. The drawings inFigures 1-5 (pages 50-54) show how the components relate to the overallsystem and give more detail on the items tested.

Equations and other data used in this analysis were obtained fromthe Machiner j 's Hanalook' and Formulas for Stress and Strain.2

The materials used throughout this analysis are 304, 316, and 17-4Phcorrosion resistant steel, AlIS5700 series steel, and 6061-T6 aluminumalloy. The mechanical properties for all material used in this analysisare shown in Table 8.1, page 46. In all cases the lowest specifiedvalues were used to insure a conservative design.

Each area has been analyzed for worst case under the followingconditions:

Maximum Internal Pressure (P x) ... ......... 5,000 psi

Internal Operating Pressure (P y) ......... ... 2,000 psi

Maximum External Pressure (Pz) ......... ........ 700 psi

Maximum Handling Load (PH) ........ ......... 25,000 lb

Where worst case load conditions differ from those listed above, theyare so noted at the specific point of analysis.

The final result is the safety factor (SF) achieved or in somecases, deflection. These values are listed in the Summary Table 8.2,page 47.

1 ,lachinery'a Handbook, 20th ed. New York, Industrial Press, Inc.,1976.

2 Raymond J. Roark. Formulas for Stress and Strain, 3rd ed. New

York, McGraw-Hill, 1971.

3

NWC TM 3358

ABBREVIATIONS AND SYMBOLS

A area (in )

Al aluminum

ALY alloy

B A bearing area (in )

BL maximum bearing load (ibs)

BS bearing stress (psi)

* CRES corrosion resistant steel

D outside diameter (in.)

d inside diameter (in.)

E modulus of elasticity (psi)

I moment of inertia

IN. inches

Z moment arm (in.)

LBS pounds

M moment (in.lbs)

m I/V

n number of threads

P external collapsing pressure (psi)

P, pitch diameter (in.)DPE ejection load (lbs)

P handling load (lbs)

P maximum internal pressure (psi)xP internal operating pressure (psi)

P maximum external pressure (psi)

P thread pitch

PSI pounds per square inch (lbs/in2 )

R radius (in.)

SA shear area (in.)

SB maximum bending stress (psi)

SL shear load (lbs)

. S shear stress (psi)

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y deflection (in.)

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