NSN 2835-00-918-4223
Part Details | NONAIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2835-00-918-4223 A single stationary item designed for the purpose of directing air at the proper angle and velocity to a ROTOR, TURBINE, NONAIRCRAFT GAS TURBINE ENGINE. It has provisions for attaching to a CASE (3), TURBINE, NONAIRCRAFT GAS TURBINE ENGINE. It may have an inner support shroud.
Alternate Parts: 377330, 37733-0, 2835-00-918-4223, 00-918-4223, 2835009184223, 009184223
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 01, 1960 | 00-918-4223 | 50586 ( NOZZLE, TURBINE, NONAIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2835-00-918-4223
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 37733-0 | 55820 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
Technical Data | NSN 2835-00-918-4223
| Characteristic | Specifications |
|---|---|
| SPECIAL FEATURES | OUTER SHROUD CRES,AMS5576,INNER SUPPORT CRES,AMS5768 OR CRES,AMS5532,2.331 IN.MIN,2.366 IN.MAX O/A LG,10.330 IN. MIN,10.390 IN.MAX OD SHROUD,4.160 IN.NOM ID SUPPORT,17 VANES EQUALLY SPACED,17 BOLTS,NO.10-0.190 IN.-32 UNF CLASS 2A THD,W/NUTS,THROUGH SHROUD AND SUPPORT,EQUALLY SPACED ON PLUS .692 IN.NOM BOLT CIRCLE DIA,66 HOLES,0.124 IN.MIN,0.129 IN.MAX DIA THROUGH SHROUD PERIPHERY EQUALLY SPACED 1.094 IN.NOM DISTANCE FROM VANE LEADING EDGE,6 SLOTS,0.156 IN.MIN,0.158 IN.MAX W SLOTS,THROUGH SHROUD PERIPHERY EQUALLY SPACED 0.732 IN.MIN,0.736 IN.MAX DISTANCE FROM VANE LEADING EDGE; |
