Text

Revision a to Qualification Test Rept for Model 1801112-11 PSA-35 Shock Arrestor
	ML18025B862
Person / Time
Site:	Browns Ferry, Sequoyah, 05000000
Issue date:	02/07/1980
From:	Glauser J, Whitney R, Wright W; PACIFIC SCIENTIFIC
To:	;
Shared Package
ML18025B853	List: ML18025B852; ML18025B854; ML18025B855; ML18025B856; ML18025B857; ML18025B858; ML18025B859; ML18025B860; ML18025B861; ML18025B862; ML18025B865; ML18025B867; ML18025B868; ML20063B420;
References
	TR-845, TR-845-RA, TR-845-REV-A, NUDOCS 8208250437
	Download: ML18025B862 (45)
	v • d • e

REPORT NO.

TR 845 7 P'ebruary 1980 180lll2-11 PSA-35 QUAI XPXCATION TESTXNG BERGEN PATERSON II C. F.

BRAUN SPECIFXCATXON 400-20 TVA "STRIDE" PRO/)i PB Cl 1 It St IEllTIl It KIN-TECH DIVISION P

P D

auser Director of En ineering Chief D e

ment Engineer P. A. Hadna't o3 Mana ex REV.

DATE A

4-23.-80 BY APPD. BY 4)SQ C

PAGES AFFECTED Page 6

Page 9

Correct Acceleration Requirement Par.

1.1 aaoa2504w a2oasa PDR ADOCK 05000259 P

PDR PACIFIC SCIENTIFIC

~ KIN-TECH DIVISION

,1346 S. State College Blvd.

Araheim, Ca.

92803

{7t4) 774-82)7

REPORT NO.

- TR 845 PAGE 2

OF TABLE OF CONTENTS Administrative Data Equipment List Certification Testing 1.0 Acceptance Tests 2.0 Dynamic Load Cycling, Room Temperature

" 3.0 Abnormal Environment 4.0 Dynamic Load Cycling, 200 P

5.0 Additional Load Cycling 6.0 Summary and Conclusions Oscillogram - Load vs Travel Abnormal Environment Logs Appendix 1.

Initial Punctional Test Data Sheets and Material Traceability Record 2.

Spring Rate Calculations

~Pa e

3 5

10ll - 18 19 20 Enclosure l.

Acceptance Test Procedure I.T. 535 Photographs l.

Identification 2.

Acceleration Test Stand 3.

Dynamic Load Cycling at Room Temperature

4. "'Abnormal Environment Set-up 5.

Dynamic Load Cycling at 200 P.

PACIFIC SCIENTIFIC

~ KIN-TECH DIYISION 1346 S. State College Blvd.

Anaheim, Ca.

92803 (714) 774-5217

REPORT NO.

TR845 PAGE GP ADMINISTRATIVEDATA PURPOSE OF TEST To determine the ability of the 1801112-11 Shock Arrestor to meet the Qualification Test requirements.

MANUFACTURER PACIFIC SCIENTIFIC COMPANY, KIN-TECH DIVISION, 1346 S. State College Boulevard, Anaheim, California.

MANUFACTURER'S TYPE OR MODEL NO.

P/N 1801112-11 MODEL PSA-35 APPLICABLE DOCUMENTS C.F.

BRAUN Specification 400-20 Rev.

5'SCO Drawing 1801112-11 PSCO ~iFicMioh Test Procedure DR 1506 Rev.

3 PSCO Acceptance Test Procedure I.T. 534 Rev. 3 UANTITY OF XTEMS TESTED Two (2) P/N 1801112-11 Shock Arrestors S/N 5192 and 5193 were used for the test program.

They were selected at random from a production lot.

The test units were built in accordance with ASME Boiler and Pressure Vessel Code Section IXX, Subsection NF.

Summer 1977 Agenda and Code Case 1644-5.

Each of the test units were sub)ected to all of the required tests.

TEST COMPLETION DATE 1 February 1980 TEST CONDUCTED BY PACIFXC SCIENTIFIC COMPANY, KIN>>TECH DIVISION, ANAHEIM, CALIFORNIA SECURITY CLASSIFICATION OF ITEMS Unclassified PACIFIC SCIENTIFIC

~ KIN-TECH DIYISION 1346 S. State College Blvd.

Anaheim, Ca.

92803 (714) 774-5217

V

>J Ef

TEST Dimensional Examination E UIPMENT LIST Standard Micrometers Height Gages, etc.

CALIBRATION CALIBRATION TOLERANCE DATE PERIOD (Data on pile in Quality Control Dept.)

CO 'g p n o

O 0

m M

O W z ITl CL l2

~~~ n 3

A Ql O

Pl U

c M

V 0 V

Acceleration/Load Breahaway Friction Force Lost Motion Dynamic Load Abnormal Environment 1801-TF-2 Fixture Meylan Digital Timer Model 112 1801-TF-2 Fixture Pressure Gauge Dial Indicator -.001/Div.

Mts. Load Cycling Machine Model 311;31 S/N 416 Lebow Load Cell Model 661.023A-02 S/N 999 C. L. Collins Linear Motion Transducer Model LMT 12911, S/N 19447 Omega Digital Thermometer Model 2175A With Thermocouple B.T.C. Steam Chamber 0-100 PSI Pressure Gage Omega Digital Thermometer Model 2175A Pith Thermocouple

+.01 sec.

+. 1Z

+ 1/2 de

+ 0.5X 9/24/79 a 1/24/79 1 /11/80 11/21/79 6/19/79 9/5/79 1 /7/80 9/5/79 4 months 3 months 6 months 12 months Daily 3 months 12 months D

Zlfll m~

O z

12 months 0

REPORT NO, TR 845 PAGE~

OF CERTIFICATION I, the undersigned, being a registered Professional Engineer in the Stat:e of California, competent in the testing and evaluation of Mechanical Shock Arrestors, certify that this report truly and accurately presents results of tests performed in accordance with the approved test procedures.

Certified by Quality Engineer State of California Registration No. 1919 Date 7 February 1980 PACIFIC SCIENTIFIC

~ KIN-TECH DIVISION 1346 S. State College Blvd.

Anaheim, Ca.

92803 (714) 774-5217

Bi

REPORT NO.

TR 845 PAGE~

QF 20 TESTING 1.0 Acce tance Tests 1

The test units were examined and tested to the requirements of I.T. 534, enclosure 1.

Photograph 1 identifies the test units.

Photograph 2

shows the acceleration test fixture.

The breakaway friction must not O

A exceed 5001bs.

and the snubber must limit the acceleration to.015 G

maximum (.59 seconds for 1 inch travel).

The calculations are as follows:

a~

2S

+

2x 1

.015 G

386'86 x (.59) 1.2 Procedure 1.2.1 Breakawa Friction The breakaway friction was measured with the unit extending and retracting.

The measurements were made at mid position and approx-imately 1/2 inch away from the fully retracted and fully extended position.

1.2.2 Acceleration A constant load was applied to the snubber and the time required for the unit to travel 1 inch was recorded.

The test was made with tension and compression

loads, 1.3 Results Both snubbers met, the requirements.

S/N Friction-Lbs.

(500 lbs. max.)

Acceleration (0.59 sec. Min.)

Ext.

1.99 sec. 5192 5193 425 lbs.

485 lbs.

1. 54 Refer to Appendix 1 for actual data sheets X.T. 534, Page 4.

Retr 1.83 sec.

1.52 PACIFIC SCIENTIFIC

~ KIN-TECH DIYISION 1346 S. State College Blvd.

Anaheim, Ca.

92803 (714) 774-5217

REPORT NO.

TR 845 PAGE~

QF

>0 2.0 ic Load C clin Room Tem erature

2. 1-2.2 Rated load (50Eppplbs) shall be applied for ten seconds at-each step in both tension and compression between 3 and 33 Hs in 5 Hs steps.

The lost motion during dynamic cycling shall not exceed

.040 inch.

The unit spring rate shall be calculated from the load/deflection photographs between 8 and 1S Hs.

The average value shall be equal to or greater than 600 x 10 lbs./inch less 10X.

3 Spring Rate ~ Full Rated Load eak to eak)

Total deflection less lost motion Procedure The snubber was installed in an MTS load cycling machine and positioned to approximately mid-position of travel.

A 1inear motion transducer t

was installed to measure unit travel or displacement.

A load cell was in line with the unit centerline to measure axial load.

Refer to set-up in Photograph 3. The displacement and axial load were monitored on an oscilloscope with the displacement on the vertical axis and the load on the horizontal axis.

Refer to the photographs on pages 11 thru 14'he input motion was a displacement that varied as a sine wave which resulted in a load being developed in both tension and compression.

Rated load was applied for 10 seconds at each of the seven frequency steps.

2.3 Results The unit met the requirements.

Refer to oscilloscope photos and Appendix 2.

S/N 5192 5193 Data Summa Lost Notion - Inches

.040 inch max.)

. 037

.032 Spring Rate Lbs/Inch (540 X lo> Lbs/Inch Min.)

1150 x 103 1210 x 103 PACIFIC SCIENTIFIC

~ KIN-TECH DIVISION 1346 S. State Coltege Slvd.

Anaheim, Ca.

92803 (714) 774-52>7

REPORT NO.

TR 845 PAGE~

OF 20 3.0 Abnormal Ambient Environment 3.1 The shock arrestors at room ambient condition shall be placed in a chamber capable of maintaining pressure and temperature.

The chamber conditions shall then be ad5usted to the Phase I Condition and then alloved to decay gradually through Phase II, III and CV as outlined.

(1)

Phase I:

330F, (-)2 to (+)15 psig, all steam for 3 hours3.472222e-5 days 8.333333e-4 hours 4.960317e-6 weeks 1.1415e-6 months

330F,

(+)30 psig, all steam for 45 seconds (2)

Phase II:

310F,

(<<)2 to (+)15 psig, all steam for 6 hours6.944444e-5 days 0.00167 hours 9.920635e-6 weeks 2.283e-6 months (3)

Phase III:

250F, 0 to 15 psig, 100 percent relative humidity (RH) for 24 hours2.777778e-4 days 0.00667 hours 3.968254e-5 weeks 9.132e-6 months (4)

Phase IV:

250F to 100F, 0 to 15 psig, 100 percent relative hum-idity for 1 day (24 hours2.777778e-4 days 0.00667 hours 3.968254e-5 weeks 9.132e-6 months ) 0 Following the steam test the unit shall be stabilized at 200 F and sub)ected to the breakaway friction and acceleration test.

3 ~ 2 Procedure The PSA 35 snubbers were placed in the Steam Chamber.

Refer to photograph 4.

The chamber was sealed and a quantity of water vas introduced into the chamber.

Heat was applied to the chamber and the temperature was monitored vith a thermocouple.

The chamber conditions vere ad)usted to 330 F and + 15 psig (Phase I).

0 The air was vented from the chamber vhich resulted in the-units being sub5ected to "all steam".

The temperature was maintained at 330 F minimum and the pressure was alloved to vary between 0 and 15 psig.

The superheated steam condition was obtained by draining water from the chamber in order to keep the pressure from increasing above 15 psig.

A log vas maintained of the temperature and pressure.

Refer to pages 19 thru 21.

After 3 hours3.472222e-5 days 8.333333e-4 hours 4.960317e-6 weeks 1.1415e-6 months the pressure was increased to 30 psig for 45 secon s

y ds b adding more water, and then reduced to the condition of Phase II and maintained for 6 hours6.944444e-5 days 0.00167 hours 9.920635e-6 weeks 2.283e-6 months .

0 The temperature was then allowed to drop to 250 F and the pressure was maintained betveen 0 and 15 psig, Phase III. After 24 hours2.777778e-4 days 0.00667 hours 3.968254e-5 weeks 9.132e-6 months the cham-PACIFIC SCIENTIFIC

~ KIN-TECH DIVISION 1346 S. State College Blvd.

Anaheim, Ca.

92803 (714) 774-5217

PAGE 0

OF 20 ber temperature was ad3usted to between 250 F and 100 F while 0

0 maintaining the pressure betveen 0 and 15 psig.

(Phase IV).

These conditions were held for another 24 hour2.777778e-4 days 0.00667 hours 3.968254e-5 weeks 9.132e-6 months period.

The chamber vas then opened and the units vere visually examined.

The snubbers were stabilized at 200 F for 2 hours2.314815e-5 days 5.555556e-4 hours 3.306878e-6 weeks 7.61e-7 months and then sub5ected to the breakaway friction and acceleration tests.

3. 3 Results The exterior of the units displayed a darkening in color, but there was no base metal corrosion.

The friction and acceleration values vere met at 200 F.

QA S/N Friction - lbs.

.(~

Acceleration 5192 460 lbs.

5193 450 lbs.

4.0 amic Load C clin at 200 F Ext.

1.46 1.29 Rett.

1.43 1,28 Same as Paragraph 2 1 except the unit shall be at 200 F.

0 at each step, between 3 and 33 Hz in 5 Hz steps.)

(10 seconds 4.2 Procedure o

Same as Paragraph 2.2 except the unit shall be stabilized at 200 F for 2 hours2.314815e-5 days 5.555556e-4 hours 3.306878e-6 weeks 7.61e-7 months before load cycling.

A temperature chamber was placed around the snubber which was installed in the load cycling fixture.

Refer to Photograph 5.

4.3 Results The unit met the requirements.

Refer to Pages 15 thru 18 for the load cycling photographs.

The maximum lost motion during cycling vas:

S/N 5192

~ 040 inch (8 Hz)

S/8 5193

.037 inch (8 Hz) 5.0 Additional Load C clin Room Tem erature A total of 5,000 cycles is required 'for each snubber.

All cycles applied during testing of Paragraph 2.0 and 4.0 shall be subtracted from 5,000 PAClFlC SCIENTlFlC ~ KlN-TECH DlVlSION 1346 S. State College Blvd.

Anaheim, Ca.

92803 (714) 774-52)7

REPORT NO.

TR 845 PAGE

~G 'F and the remaining cycles shall be run at room temperature at rated load and at 3 Hz.

5.2 Procedure The procedure details vere the same as Paragraph 2.2, except all cycles were applied at 3 Hs.

The cycles were run as follows:

CZcles

~Pre ueue 3-33Hz 3-33 5.3 Results Tem erature 75 F 200 75 TOTAL S/N 5192 1430 1330 40 SOOO Cy S/N 5193 1260 1290 2450 5000 Cy There was no failure.

Each snubber vas'in good condition after the test.

6.0 Summa and Conclusion The shock arrestors met all requirements of the test program.

There

'as no failure or damage to the units.

1.

Lost Motion

.040 inch-max.

2.

Breakaway Friction SOO lbs. max.

Acceleration Test 0.59 sec.-min.

S/N 5192

.040 inch 460 lbs.

1.43 sec.

S/N 5193

.037 inch 485 lbs.

1.52 sec.

3.

Dynamic Test Response 4.

Spring Constants 600 x10) -( 60x10) 3 3

540 x 10 lbs/inch 3

(Refer to load-displacement photo-graphs) 1260 x 10 lbs/in.

1365 xl0 lbs/in.

3 3

PACIFIC SCIENTIFIC ~ KIN"TECH DIVISION 1346 S. State College Blvd.

Anaheim, Ca.

92803 (714) 774-5217

P/W DATE 1801 2-1-24-80 s/m PSA-35 75 F PAGE~

OF 20 Ekkkk BALLL LR%

klhmkkkk kkk

. LLLIL Lkkiik k kkkLllk LLIINkk Lk l k LL Ilk LiIlkkk LkIkkkk

. LLL%lmkkk.:

kkkik k" kkkhl%

~Lk %

0 A Lkkl Lk 1%kk

~klIkkkk.

~RL%kkkk

, LLLOLkkk kkkklk L:

ilk M M P H Cd C4 41 0 PACIFIC SCIENTIFIC ~ KIN-TECH DIVISION 1346 S. State College Blvd.

Anaheim, Ca.

92803 (714) 774-5217

f'

DATE 1-24-80 S/N 192 PSA-35 75 P PAGE SLIER SRL%ii ~

aimjair iilII%lMR WllklILtlIi:

~55%5 iii%IWW SR RL%%85

~8 llRRSR' i i iii IS SSIiRRR iii%IIRRR:

RIIIRIW i-RS%

lamini aatii$55

RllHSRRR, RRI88888':

WRSLWWRW =

iSilli Sii ii RRIR~ ii PACIFIC SCIENTIFIC ~ KIN-TECH DIVISION 1346 S. State College Blvd.

Anaheim, Ca.

82803

{714) 774-5217

F/N 1-31-80 S/N 5192 FSA-35 200 F PAGE

~G OP DEERE 88%8888 Eai Iaaaa RRNEERE 8886%888 i

~Rakllaaa RRR Iar aaa taa lilIllaaaE ERl%8888 RRIL%8888 81%'%888 EELHERE -.

Eaailla IIRR llaaa

~8 MM A Cl

~Ra aa Iaa I ~

ISara

~%I%8888 RELIEREE RKLRRRRR ERR)IR 8:

ERR l18 tIiLllaaaa Rl'L'Iaaaar EE1%8888 8Iggaaaa EEL~i%8 8.*

~Ra)la 888, laa aa ar PACIFIC SCIENTIFIC ~ KIN-TECH DIYISION 1346 S. State College Blvd.

Anaheim, Ca.

92803 (714) 774-5217

P/N 3.-31-80 S/N 5192 PSA-35 200 F REPORT NO TR 845 PAGE i

OF lllEEEE EILrEEEEE ELINEEEE EIE'%EEE EEL%LIE E =

EEk>IlE EEE. IEE EE IEE H H 4 4 IISEEE EILIEEEE

>EEEE EIL EE%%EEE EEL>IE E:

EEET EEE 1EE EE l'RE O O H N P H c4 D4 X O EIL%EEE EEILIEEEE EEIIREEE EE)IL%EEE EEhlNE E:

-'ERIIE EEEllEE EE 1EE PACIFIC SCIENTIFIC ~ KIN-TECH DIVISION 1346 S. State College Blvd.

Anaheim, Ca.

92803 (714) 774-5217

P(N 1801112-11 DATE 1-24-80 S(N PBA-35 75 P REPORT NO.

PAGE

>5 OF R,%

RL I'I%

NLlR IRL%%

Il

~I ~

8 L 8

~i 55LISSUE ISSRS RRL68%88 8RR)%8%8 WIIRL%8 8 -.

RRRL)%

%SR lRE WR 8

PACIFIC SCIENTIFIC ~ KIN-TECH DIVISION

]346 S. State College Blvd.

Anaheim, Ca.

92803 (714) 774-5217

P/N 1801112-11 S/N 5193 PSA-35 75 P REPORT NO.

TR 845 PAGE

>E OF

~li%RRR WRRI$885 WRlL~R8$$

%II%%88%

Will)RWI 8-RWI',%IS awarder aa

> ~

IimSWIE RRLIRRSE l5~S

~S

~8%%

~SR l 8$

RRRSSSR 8%1)%8%8 WWR/hid 8-IL185WR WllimRERR

~Llh38$8$

RI1%8888 8%i(IS 8 -.

aaaair 55L'5 RR 8$

VO HN jE H PACIFIC SCIENTIFIC ~ KIN-TECH DIVISION 1346 S. State College Blvd.

Anaheim, Ca.

92803 (7th) 774-5217

1-31-80/~

DATE S/N PSA-35 200 P

PAGE

~7 OF LeEEL ILLLE' LIBELEE LL EEL%LEER EEENE E"

EEL%i~

~LL )RE LL

'1E

%LEE ILL EL

~Ekl%

EEI'EEi llIEEEE

~IL'EEEEE

~IlREEEE LRIL%EEEE EEL%

Ri%EEE LEILLLE EEIIEELL LEk3EEEE ELEVE L.-

EEELIEE

~EE IIL

~ %EIIE

~ELIELLL EEIEEEE ELLE%LEE.

LEENE L',:

~EER1E ELE 'iRE

~L SE PACIFIC SCIENTIFIC ~ KIN-TECH DIYISION 1346 S. State College Blvd.

Anaheim, Ca.

92803 (714) 774-5217

8 z->z-8o I"~

DATE s/m PSA-35 200 F PAGE

>E OF

~i

~iilMS

$8lLtSRRR

~SlILWSSS

88LINRRR, WWR%% 8:

~8RLllI RRR ILM aa lIr W M A A IL'RORY

~Rll%8$$R Smlk%8REE

. RIAL'%8%8 RSL>hW 8 SSRIIR 888 llRE 55 kS

~1i%ME SRlk%115$5 555555i RL%888

~551$ 5 RS

) ~

V O

~ M 4 O PACIFIC SCIENTIFIC ~ KIN-TECH DIVISION 1346 S. State College Blvd.

Anaheim, Ca.

92803 (714) 774-5217

~

MKHIIR~

RiQ%8%%%ISERR ERSRRSS%

Ei886i55%

ERWRSE%

EN888%M EKR885%%M ERFSIR%%%

EIBI555IRM E5l8%5%%~

E88@8%M E58i%58i%~

E5888%M E58i5RRM E%9555%%%

8%N855M~

~SKHSR~

I8RRSS @%i%

E885RRM ERR%58%~

EPR558%%

E88f555ESR EN855fEM ERSSRlmKW EI5NRSM ERliSRI%

El8%88%~

EIHf588%~

ERN5i%$%

ERNBERM ERRCSEM ER%58R~

%iRR RRRSSRE~

EBSI5515~

EF8i%58$W E8858!%5%

E88@%8RRM:

ERR%58%~

E58%RWNE E88%I8%~

%8%8%5%

E8%%%M ERSRRiSNE E6538%INE ER85RRNE

%88%$8%5$%

IRR85IHRRR%

mreawam RQR8i5BESM ERi%58%RM ENRSSIRNE E88%l$%M E8%88W Ei5%REK&

'I8$

%8%

EiHWIR%

EHRNESM ERSRNEM E%88%5%

E8i85585M E85585iSM ER%8%%~

8%%iSKHR~

REPORT NO.

TR 845 ABNORMAL ENVIRONMENT LOG P/N 1801112-11 8/N 5192 6

5193 PAGE 20 PF 20

-2540 i2

~

I20j I

~ 0 JIX

/000 Idl2 IGNIS 2 $1 2

2C2 I'20 dj 2000 Qd IS Jddv 50 jjjC'l jIO LI50 Zl 93 L&0 2250 55+5 550 d 53IS Ljd ZI3 2I

~ 2 I7 Ljj/

5 I2 LI LLI Ll 2 Ia/

5 IC LI)

/CvI

/clr ld JO

/C /C

/7)d

/

I/Jd

/5C

/fdd

/C 5.

239 25 25S

'@5 0 J.I 5'.I 7 Lid LIS LI5 dj2 0 0 /JI 2 552 2900 0dl dd 50 0050 dido 0 III ol 0

0 I4r Otj20 o 24$

O5jf OS3+

2IV LI4 2 lg 2 I4 LIg 2.I4 LI OJOF 0400 0 ~

oodr OO ZI3 IIJO

//0$

/20d 2/S

/330 2 I '5 0rj$

0 JO LI3

%. I 2,(Q t I odor 0 7oo Odjr LIS

/300

/3'330

/~0 C

/430 OOIS'7 O

O74$

0 5'i 0 PIO 0 O'CC'%00 09IS 0930 lord

/030~

//00

/id Ll5 5IL

/$00

/bd j0

/b/C

/C 30 Bud PS rj55r PAClFIC SClENTIFIC

~ Klhl-TECH DlVlSlON 1346 S. State College Blvd.

Anaheim, Ca.

92803 (714) 774-5217

APPENDIX 1 INITIALFUNCTIONAL'EST DATA SHEETS AND MATERIAL TRACEABILITYRECORD, I.T. 534 PAGES 4, 5 and 5A TOTAL OF 6 PAGES PACIFIC SCIENTIFIC KIN-TECH DIYISION 1346 S. State College Blvd.

Anaheim, Ca.

92803

(?14) 774-5217

V lj

TR 8P5 APPENDIX 1 6 PAGES ADDENDUM Final Inspection Check List PSCo 1801112 Shock Arrestor AEPORT NO.

pAGE A

op 6

Rev.

J Date Ref. paragraphs refer to paragraphs from this procedure, I.T. 534 Part No. ~

/ (

Serial No.

PSCo P.O.

No.

Ehop Qrder No.

I 0 ZS %38 Customer &

Pdemn I.

Visual Examination (para.

5.1)

(a)

Dimensional....'..........

(b)

Workmanship......,.......

II.

Final Functional Tests W+-"c,

~

+I~

~

e

~

~ce ~

QAOE

( )

OG (b)

Breakaway Friction Force (500 lbs. max.)

{para. 6. 1)........................Actual~2.s Lost Motion (.040 max.) (para. 6e2).........Actual

. e'~

QH (c)

Acceleration/Load Test {.59 sec. min.}(para. 6.3)....

Actual Time Extending~sf g Retracting~/.

S Inspector S

p

~F'ACtRC ICtENTtRC CONPAKY Aircratt Products Dirisiort 1346 South State Cotteye Soutevard

~ Anaheim. Cattfornia 92fO3 ~ (f)l) TN-5217

APPENDIX 1 6 PAGES ADDENDUM Final Inspection Check List PSCo 1801112 Shock Arrestor REPORT NO.

L'AGE OF Rev.

J Part No.

Ref. paragraphs refer to paragraphs from this procedure, I.T. 534 Serial No.

5 I ~ 5 PSCo P.O.

No.

Shop Order No. + ~ES~'6 Date f- ~w WO Cua tomar Br'n Pa'rrSOn I.

Visual Examination (para.

5.1)

(a)

Dimensional..................

a

{b) Workmanship..................

II.

Final Functional Tests SCg

~

P6 Ca~

~

OAO

~

OG (a)

Breakaway Friction Force (500 lbs

. max. )

(para. 6.1)........................Actual~@>

Lost Motion (.040 max.) (para. 6a2).........Actual~~o QH (c)

Acceleration/Load Test (.59 sec. min.)(para. 6.3)....

Actual Time Ea tan ding~>+

Ratrattinge Ins pec to Stamp 4;

Date I-~~- ~

~'ACIRC ICffNTlRC COMPANY Aircraft Products Dltiahn 1346 South Stale Colleen Soufevard

~ Anaheim. California 925N G p14) 774-5217

TR 845 APPENDIX 1 6 PACES ASiiIE SECTION III, DIVISION I SUBSECTION NF Rev.

J I.T. 534 5LPTERIALS TRACE-ABILITYTABULATION PSCO P/N Pof l f~- t Serial No.

Owner1Agenr r

jc ~e Date Part No.

1801506 1801480 1801529 1801474 1801470 1801458 1801457 1801456 1801453 1801451 1801450 1801407 QD 1801467 1801464 Description End Cap (For l80L~ro W~

Cap A~sv.)

Hub, Inertia Mass Kcy, Capsthn Kcy, Anti-Rotation Nut, Adapter Tube, Transition Sbell, Torque Carrier Shell, 'Inertia Nass Hub, Torque Carrier Ca DS tQXL Cvlinder Su ort Cjrlinder Teleeconinz Housina

Nut, End Cap Naterial Code Number A'/alp

/Y Ng2

~'/48]

Nazis A(/zt C.

Al!HJ<

S tamp e-.d z'te Cd e

Qi.

1801635 l801465 Inertia >Iass Gear, Planctarf

.dd pAcIFIc sclENTIFlc cclMpANY Aircrott Products Division

%46 SOulh State COIIege SOuleVard

~ Anahe>N, CSI<<Or~>I 926CS

~ P'l4) 77'.$ 2)7 0 As e

TR 845 APPENDIX 1 6 PAGES REPORT tvv.

PAGE EA OF E

Rev.

J ASME SECTION III, DIVISION I SUBSECTION iP MATERIALS TRACEABILITYTABULATION PSCO P/N Serial No.

Pc/] 2- /

Owner/Agent 5 r o.~e <

- Po OJ OJ Pare No.

1801466 1801471 Description

Pear, Ring Gear, Pinion Material Code Number

Stamp, PACIFIC SCIENTIFIC COMPANY Aircraft Products Division 1346 SOuth State COffege BOuleVara

~ Anaheim. CalifOrnia 92803 G (?)a) 77<-5217

OB APPENDIX 1 6 PAGES AS~itE SECTION III, DIVISION I SUBSECTION NF

.I.T. 534

~ %

WLATERIA1$ TRACEABIT,ITY TABULATION PSCO P/N

/

S IN.~f Owner/Agent Bc I Date Part No.

~ 1801506 1801'0 1801529 1801474 1801470

~

1801488 1801457 1801456 1801453 1801451 18014 5O 1801407 QD 1801467 1801464 Description Hous inn

Nut, End Cap End Cap (For lSOx~ev W~

Cap A sy.)

Hub, Inertia Hass Kcy, Capsthn Key, Anti-Rotation Nut, A'dapter Tube, Transition Shell, Torque Carrier Shell, Inertia Nass Hub, Torque Carrier Ca os tan Cvlinder Su ort Cylinder Teleeennine Naterial Code Number

]V/8/7 g/Og O'@74 Stamp 0

Q+0

'go

'I ~

O>

Oa 1801635 180146m Inertia >fass Gear, Planetary OWg PACIFIC SCIENTIFIC COMPANY Aircrott Products Division 4S'6 Scuth Stele COIIeOe BOuIeVird ~ Ank'Ilei.

C4<<IO<>>4 926CS

~ P'I') 774N52t7

EN~A APPENDXZ 1 6 PAGES PAGE ENN PP~

Rev.

J I.T. 534 ASME SECTION III, DIVISION I SUBSECTION NF MATERIALS TRACEABILITYTABULATION PSCO P/N Rw Il~- (

N N1N Owner/Agent %r e

F~4r.

o I,~P Part No.

Description Material Code Number St mp, OJ OJ 1801'471 Gear, Pinion 1801466

Pear, Ring 4/z7/]g E ~ ~

't C

PAC1FIC SCtENTIFIC COMPANY Aircfatt Pfoduct5 Division

@46 South State College 9outevafd

~ Aneheitn, Catiiofnla 92803

~ tf14) 77l Qt7

REPORT NO.

TR 845 APPENDIX 2 SPRING RATE CALCULATIONS PACIFIC SCIENTIFIC ~ KIN-TECH DIVISION 1346 S. State College Blvd.

Anaheim, Ca." 92803 (714) 774-5217

V

REPORT NO.

TR 845 APPENDIX 2 PSA - 35 SPRING RATE CALCULATIONS AVERAGE ALLIABLERATE ~ 600 << 60 ~ 540 x 10 Lbs/Inch 3

S/N Temp OF Freq.

Hz Peak-Peak Load Lbs.

Dynamic Displ.

Inch Lost Motion Spring Rate Inch 1'x 103 lbs/Inch 5192 75 97000

.108

.037 1366 18 98000

.110

.025 1153 AVERAGE ~

1260 x 10 Lbs/Inch 5193 75 88000

.090

. 032 1517 18 98000

.'102

.021 1210 AVERAGE ~

1364 x 10 Lbs/Inch SAMPLE CALCULATION Dynamic Spring Rate

~

97000 lbs.

(,108-,037 inch) 1366 x 10 Lbs/Inch PACIFIC SCIENTIFIC

~ KIN-TECH DIVISION 1346 S. State College Blvd.

Anaheim, Ca.

92803 (714) 774-5217

REPORT NO FAGF~GF

. ~

~ l. 0 PURPOSE 1.1 To assure compliance of production units of the Shock Arrestor Assembly with referenced drawings.

2.0 SCOPE 2.1 This test establishes both visual and functional charac-teristics which could be expected to vary through dimen-s iona 1 varia tion or improper assembly and adjustment.

3.0 REFERENCE DOCUMENTS 4.0 3.1 PSCo Drawing 1801112

~U1P T

.1 1801 TF-2 Universal Shock Arrestor Tester 4.2

.0001 Dial Indicator

5. 0 INDIVIDUALTESTS

5. 1 Examination of Product 5.1.1 Each unit shall be subjected to a dimensional examination to determine compliance with appli-cable final assembly drawing.

5.1.2 Each unit shall be visually inspected to assure completeness of assembly, freedom from burrs and sharp

edges, alignment of parts, security of fasteners, and dimensional integrity.

5.1.3 5.1.4 Units shall be visually inspected for general appearance of plating, painting, freedom from nicks and damage of finishes.

Units shall be inspected to assure the accuracy and legibility of marking and identification.

6. 0 FINAL FUNCTIONAL TESTS QA 6.1 Breakawa Friction Force (500 lbs. max.)

6.1.1 The unit sh,"ll extend and retract when subjected to a maximu;ei force of 590 lbs.

Unit shall be in-stalled in the 1801 TF-2 Test Fixture and the starting force in both the extension and retrac-tion modes measured at three places, Measurements shall be taken at the approxi-mate mid position and approximately

.5 inch from both extreme positions.

Load measured shall not exceed 500 lbs.

PACIRC SClENTIRC COMPANY Aircraft Products lÃviaion

~346 South Slate Collepe Boulevard

~ Anaheim. California 82803

~ (714) 774-5217

ML18025B862

Text

Navigation menu

Search