NSN 2835-01-155-3188
Part Details | NONAIRCRAFT GAS TURBINE ENGINE TURBINE SHAFT
2835-01-155-3188 An item designed to transfer rotary motion from a ROTOR, TURBINE, NONAIRCRAFT GAS TURBINE ENGINE to a ROTOR, COMPRESSOR, NONAIRCRAFT GAS TURBINE ENGINE and/or a ROTOR, FAN, NONAIRCRAFT GAS TURBINE ENGINE. It may include the HUB, TURBINE, NONAIRCRAFT GAS TURBINE ENGINE. It may include provisions for mounting bearings and/or seals.
Alternate Parts: 723059, 723059, 723059, 2835-01-155-3188, 01-155-3188, 2835011553188, 011553188
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUN 07, 1983 | 01-155-3188 | 50602 ( SHAFT, TURBINE, NONAIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2835-01-155-3188
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 723059 | 99167 | HAMILTON SUNDSTRAND CORPORATION |
| 723059 | 58163 | MEGGITT (NORTH HOLLYWOOD), INC.DBA MEGGITT CONTROL SYSTEMS |
| 723059 | 55820 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
Technical Data | NSN 2835-01-155-3188
| Characteristic | Specifications |
|---|---|
| OVERALL LENGTH | 4.969 INCHES NOMINAL |
| SPECIAL FEATURES | ALL CHARACTERISTICS DATA PROPRIETARY; SURFACE FINISH 16.0 MICROINCH ON PLAIN END; 32.0 MICROINCH INTERNAL; 250.0 MICROINCH EXTERNAL; EXTERNAL FLANGE ON RIGHT END; 0.938 IN. DIA; 0.125 IN. THICK; 4 SHOULDERS 2 UNDERCUTS BETWEEN ENDS; SMALLEST DIA 0.625 IN.; LARGEST DIA 0.6692 MIN 0.6695 MAX IN.; ONE 0.664-32UNS 3A THREADED SHOULDER; FLAT KEYWAY LOCATED ON SHOULDER BEHIND FLANGE; 0.791 IN. LG; 0.1895 MIN 0.1915 MAX IN. W; 0.0822 MIN 0.0875 MAX IN. DEPTH; INTERNAL FLAT ROOT; SIDE FIT; INVOLUTE SPLINE DATA: 11 TEETH; 0.3438 IN. PITCH DIA; 0.5 IN. PITCH FRACTION; 0.2977 IN. BASE CIRCLE DIA; 30 DEG PRESSURE ANGLE; 0.375 IN. MIN FORM DIA; 0.045 IN. WIRE SIZE; 0.2955 IN. MAX LG BETWEEN 2 WIRES; 0.001 IN. MAX PROFILE VARIATION; 0.0003 IN. MAX LEAD VARIATION; ARMY COGNIZANT SERVICE |
| END ITEM IDENTIFICATION | 2350-01-061-2445 |