ML17053A855

Rept of Test on Philadelphia Gear Corp SMBO-15 Limitorque. Prepared by Lockheed Electronics Co

ML17053A855
Person / Time
Site:	Nine Mile Point
Issue date:	07/31/1968
From:	FRANKLIN INSTITUTE
To:
Shared Package
ML17053A854	List: ML17053A853 ML17053A855 ML17053A857 ML17053A858 ML18037A184
References
2120-4594, NUDOCS 7907300166
Download: ML17053A855 (12)

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e PHXLADELPHXA GEAR CORPORATION

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SMBO-15 LEIIXTORQUE

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PLAINI'I LDe NQYf JKAGQY C

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Approved by:

N. Johnson, Sup rvisor Environmental. mboratory C

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CC LEG 197P

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~ '-. '::,":.: i'.;.".,,'.'..', ':..."-'i'..).: Tes t Report No ~ 2120- 559 PURPOSE-OF TEST: '..

':. '.. 'o 'subject the test specimen to the

';:.. Vibration Test r'eferenced in. Philad.elphla

.'..'Gear Corporation Purchase Order No.

600198.

KQfUFACTURER:

.:.'..':.;, '.Philadelphia Gear Corporation I

l,'..=.:.:;.:::,.;: King of Prussia, Pa.

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. SPECIiIENS TESTD:

-'.': SIIBO-15 Limigorque (Reliance Motor S/N 435571-MS)

J APPLICABLE DOCUiIENTS:

Philadelphia Gear Corporation

..:Purchase Order No.

600198

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CASE 'UMBER:, ; '" 24-8001-0594

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One (1,)

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SECURITY CLASSIFICATlON OF SPECIMEifS TESTED: 'nclassif led.

DgTE TEST COMPLETED:

7/30/68 TEST CONDUCTED BY:

LOCKHEED ELECTRONICS COiIPANY ZNVIRONiIENTAZ LABORATORY ISPOSITION OF SPECIMENS TESTED:

...Returned. t'o.'ranklin Institute, Applied Mechanics Laboratory pe r the rea ue st of

".'..."Philadelphia Gear Corooraiion per Lockheed Electronics Company Packing Silo No.

41775

.':::;"..':.::-".-::., dated. 7/31/68.

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TEST APPARATUS:

" :.-...':Reaction-Type Vibration Machine, LAB Company i!odel RVH-72-5000, S/N 51401

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Vibration Meter, MB Company

'odel M-6, S/N 539 J

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, ,.:;Vibration Pickups, MB Company Type 120,

.',', 'S/N 14187 (vertical).and S/N 11263

".. (horizontal)

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J TEST PROCEDURE:

..":The test soecimen was secured to the vibration machine, as sho>>n in Figures 1

.'and. 2, and sub]

cted. to five (5) cycles of

. vibration in 'ooth the vertical axis and

.:'-..:the horizontal axis rrith the mounting flange

.:.. -',"-in the horizontal plane.

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TEST PROCEDURE:

=.;:.':. Each: cycle consisted of two (2) minutes (Cont'd.)....: '..""'::.'".'.";"-: ':.of.vibration at a freauency of twenty (20}

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and. a acceleration level of 'one (1}

followed, by. one (1.) m1nute of no vibration.

.'.Visual inspections for evidence of any

-.-;-.::..'::":external 'physical damage were conducted.

'::.'":;.:: throughout v bration testing.

TEST RESULTS::

".'.":The Vibration Test was completed with no

.'visible evidence of any external physical

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RECOtPilEÃ3ATIONS:

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Data merely submitted..

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