|
|
National Stock Number: 4820-00-692-0041
Federal Supply Class: 4820
National Item Identification Number: 006920041
Description: VALVE,GLOBE
Detail: A valve with one inlet and one outlet connection with outlet flow parallel to inlet flow. The flow is controlled by the action of a stem which lifts the disk perpendicularly off the center axis of its seat. The stem is at a 90 degree (1.5708 radians) angle to axis of flow. Excludes VALVE, STOP-CHECK; COCK, SHUTOFF, SCREW STEM; and VALVE, SOLENOID.
|
Manufacturer Information:
276343 | 0KDP7 | KIDDE-FENWAL, INC. | 276343 | 16004 | DAVEY COMPRESSOR CO DIV OF KECO INDUSTRIES INC | 40438 | 16004 | DAVEY COMPRESSOR CO DIV OF KECO INDUSTRIES INC | 5669 | 28510 | GENERAL AVIATION INDUSTRIES, INC. | 5669 | 58553 | SUPERIOR VALVE CO |
|
Techincal Specification:
BONNET ATTACHMENT METHOD | THREADED | BONNET TYPE | INSIDE SCREW | CONNECTION TYPE | THREADED EXTERNAL TUBE 2ND END | CONNECTION TYPE | THREADED EXTERNAL TUBE 1ST END | CONNECTION STYLE | FLARED (TUBE) 1ST END | CONNECTION STYLE | FLARED (TUBE) 2ND END | FLOW CONTROL DEVICE | STEM | MATERIAL | COPPER ALLOY OVERALL | MAXIMUM OPERATING PRESSURE | 4000.0 POUNDS PER SQUARE INCH SINGLE RESPONSE | MEDIA FOR WHICH DESIGNED | OXYGEN, GASEOUS SINGLE RESPONSE | NOMINAL THREAD SIZE | 0.375 INCHES 2ND END | NOMINAL THREAD SIZE | 0.500 INCHES 1ST END | NONDEFINITIVE SPEC/STD DATA | II TYPE | SEAT ANGLE | 37.0 DEGREES 1ST END | SEAT ANGLE | 45.0 DEGREES 2ND END | SPECIAL FEATURES | GRUMMAN A10 AIRCRAFT | STYLE DESIGNATOR | STRAIGHT THRU | THREAD CLASS | 3A 1ST END | THREAD CLASS | 3A 2ND END | THREAD DIRECTION | RIGHT-HAND 1ST END | THREAD DIRECTION | RIGHT-HAND 2ND END | THREAD SERIES DESIGNATOR | UNF 1ST END | THREAD SERIES DESIGNATOR | UNF 2ND END | VALVE OPERATION METHOD | MANUAL |
|
|