NSN 2835-00-930-7132
Part Details | NONAIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR
2835-00-930-7132 A single or multistage assembly designed to receive thermal energy from the combustion section and convert it to mechanical energy to drive the ROTOR, COMPRESSOR, NONAIRCRAFT GAS TURBINE ENGINE and/or the ROTOR, FAN, NONAIRCRAFT GAS TURBINE ENGINE through a SHAFT, TURBINE, NONAIRCRAFT GAS TURBINE ENGINE. It consists of disks, blades, hubs, and the like. It is the moving part of a TURBINE ASSEMBLY, NONAIRCRAFT GAS TURBINE ENGINE. It has facilities for attaching to a SHAFT, TURBINE, NONAIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 6956521, 695652-1, 2835-00-930-7132, 00-930-7132, 2835009307132, 009307132
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUN 29, 1966 | 00-930-7132 | 50592 ( ROTOR, TURBINE, NONAIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2835-00-930-7132
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 695652-1 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 2835-00-930-7132
| Characteristic | Specifications |
|---|---|
| SPECIAL FEATURES | MATL TITANIUM ALLOY PER EMS 491; 1.690 IN. MIN AND 1.696 IN. MAX LONG; 5.747 IN. MIN AND 5.753. MAX OD TAPERED TO 3.22 IN DIA; BORE 0.7917 IN MIN AND 0.7932 IN MAX DIA; COUNTER BORE 0.9010 IN. MIN AND 0.9013 MAX DIA BY 0.27 |
