Page 34 - Improving Machinery Reliability
P. 34

Requirements Specificatiori   7


                    CENTRIFUGAL COMPRESSOR                         P  A  G  E  3  OF b
                           DATA SHEET           JOB NO.         ITEM NO.
                                                REVlSlON
                        CUSTOMARY UNITS   CONSTRUCTION  FEATURES   DATE
                I *            RPM   FPS  TRIP   RPM   TYPE (OPEN. ENCLOSED, ETC.)
                 1
                 2  0 SPEEDS:
                                                    TYPE FABRICATION
                    MAX. CONT.
                 3
                 4
                                                    MATERIAL
                                        RATE0 SPEED
                    MAX  np SPEEDS:
                                                    MAX.  YIELD STRENGTH (PSI)
                                    FPS a MAX CONT.  SPEEC
                      TERAL CRITICAL SPEEDS (DAMPED)
                                                    SMALLEST TIP INTERNAL WIDTH (IN, 1
                    FIRST CRITICAL
                    SECOND CRITICAL,   RPM   MODE   BRINNEL HARDNESS:   MAX-   MIN.
                                             MODE
                                                    MAX.  MACH.  NO. a IMPELLER EVE
                                   RPM
                 e   THIRD cRincAL   RPM     MODE   MAX. IMPELLER  HEAD a RATED sm (FT-LBsILB)-
                 10   FOURTH CRITICAL   RPM   MODE   0 SHAFT:
                 11  0 TRAIN LATERAL ANALYSIS REQUIRED (2.0.2.3)   MATERIAL
                 12  0 UNOAMPEO STIFFNESS MAP REOUIREO (2.8.2.401   OIA  @  IMPELLERS (IN)-   OIA a COUPLING (IN.)-
                 13  0 TRAIN TORSIONAL ANALYSIS REQUIRED   SHAFT END:   TAPERED   CYLINDRICAL
                 I4   (WRBINE ORNEN TRAIN)  12.0.4.6)   MAX. YIELD STRENGTH (PSI)
                 15  0 TORSIONAL CRITICAL SPEEDS:   SHAFT HARDNESS IBNH) (Re)
                 16   FIRST cRincAL          RPM    STRESS AT COURING  (PSI)
                 17   SECOND CRITICAL        RPM   0 BALANCE PISTON:
                 16   THlRO CRITICN          RPM    MATERIAL       AREA       (IN  !
                    FOURTH CRITICAL          RPM    FIXATION METHOD
                  )VIBRATION:                      0 SHAFT SLEEVES  (2.8.2):
                !  ALLOWABLE TEST LEVEL.     MILS      AT INTERSTG. CLOSE   MATL
                                                       CLEARANCE POINTS
                     (PEAK TO PEAK1                    ATSHAFT  SEALS   MATL
                 23  0 ROTATION, VIEWED  FROM DRIVEN END
                 24  0 MATERIALS INSPECTION REQUIREMENTS (4.2.3)   0 LABYRINTHS:
                 21   0 SPECIAL CHARPV TESTING 12.11.3)   INTERSTAGE
                 2(   0 RADIOGRNWY REQUIRED FOR        TYPE       MATERIAL
                 21   0 MAGNETIC PARTICLE REOUIRED FOR   BALANCE FiSTON
                 21   0 LIQUID PENETRANT REQUIRED FOR   TYPE      MATERIAL
                 2(  0 CASING:                      SHAFT SEALS:
                 3(   MODEL                        0 SEAL TYPE (2.8.3
                 31   CASING Sfti7                 0 SETTLING OUT PRESSURE (PSIGJ
                 3;   MATERIAL                     0 SPECIAL OPERATtON (2.8.1)
                 3:   THICKNESS (IN.)   CORR.  ALLOW.  (IN.)   0 SUPREMENTAL DEVICE REOUIREO FOR CONTACT
                 3r   MAX. WORIUNG PRESS       PSlG   SEALS (2.8.3.2)   TYPE
                 3!   MAX DESIGN PRESS         PSI0   0 BUFFER GAS SYSTEM REQUIREO (2.8.71
                 24   TEST PRESS (PSIG):  HELIUM   HYDRO   0 TYPE BUFFER GAS
                 3i   MAX. OPER.  TEMP.OF MIN.  OPER.  TEMP.*   0 BUFFER QAS CONTROL SYSTEM SCHEMATIC BY VENDOR
                 31   MAX NO.  OF IMPELLERS FOR CASING   0 PRESSURIZING GAS FOR SUBATMOSPHERIC SEALS 12.8.61
                 31   Mu(. CASING CAPACITY (ICFM)   0 TYPE SEAL
                 41   RADIOGRAPH QUALrTy   0 YES   0 NO   ‘I  0 INNER OIL LEAKAGE GUAR.  (GALfDAY/SEAL)
                 4   CASING SRlT SEALING          )PBUFFER  GAS REQUIRED FOR:
                 4;   STEM RELIEF VALVE SET PT.  (2.2.3)   PSlG   0 AIR RUN-IN   0 OTHER
                 4   IAPHRAQMS:                    0 BUFFER GAS FLOW (PER SEAL):
                                                                          A
                                                                        PSI
                      MATERIAL                         NORM:-   LBSIMIN @ - P-
                 4!  0 IMPELLERS:                      MU(.:-   LBSlMlN a __  PSI A P-
                 41   NO.     DIAMETERS            O BEARINQ HOUSINQ CONSTRUCTION:
                 4    NO,  VANES EA.  IMPELLER         TYPE (SEPARATE. 1NTEGRAL)~SUlT
                 4                                     MATERIAL
                  I_
                  PAINTED IN U.S.A.  DS-617-3                                 REV.  1.
                    Figure 1-3. API 617, data sheet page 3. (Courtesy American Petroleum Institute.)
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