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National Stock Number:
2840-01-039-3369
Federal Supply Class:
2840
National Item Identification Number:
010393369
Description:
CHAMBER,COMBUSTION,AIRCRAFT GAS
Detail:
THE PORTION OF AN ENGINE, GAS TURBINE, AIRCRAFT IN WHICH FUEL IS BURNED. IT MAY BE AN ANNULAR TYPE IN WHICH THE SPACE BETWEEN THE CIRCULAR INNER AND OUTER CYLINDERS FORM THE BURNING CHAMBER OR IT MAY BE THE MULTI-ARRANGEMENT CAN TYPE IN WHICH SEPARATE CAN LIKE BURN CYLINDERS ARE POSITIONED IN A CIRCULAR ARRANGEMENT WITHIN AN INNER AND OUTER CASE.
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Manufacturer Information:
| 23056130 | 63005 | ROLLS-ROYCE CORPORATION | | 23056130 | 73342 | ALLISON TRANSMISSION INC | | 6871486 | 63005 | ROLLS-ROYCE CORPORATION | | 6871486 | 73342 | ALLISON TRANSMISSION INC |
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Techincal Specification:
| SPECIAL FEATURES | CRES, AMS5521, 9.560 IN. NOM. O/A LG.; 6.524 IN. MIN.,6.536 IN. MAX. O/A OD; 1ST END FLANGE, 12 SLOTS EQUALLY SPACED ON OUTER PERIPHERY, 0.500 IN. NOM. DISTANCE FROM 1ST END TO SLOTS; 22 SLOTS EQUALLY SPACED ON OUTER PERIPHERY, 3.310 IN. NOM. DISTANCE FROM 2ND END TO SLOTS; 22 SLOTS EQUALLY SPACED ON OUTER PERIPHERY, 1.411 IN. NOM. DISTANCE FROM 2ND END TO SLOTS; 14 HOLES 0.375 IN. NOM. DIA. EQUALLY SPACED ON OUTER PERIPHERY; 2.090 IN. NOM. DISTANCE FROM 2ND END TO HOLE CENTERS, 6 HOLES 0.500 IN. NOM. DIA. AND 6 HOLES 0.562 IN. NOM. DIA. THROUGH BODY ALTERNATELY SPACED IN GROUPS OF 3 ON OUTER PERIPHERY, 2.720 IN. NOM. DISTANCE FROM 2ND END TO HOLE CENTERS |
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