ARMY *TM 9-6115-464-34 AIR FORCE TO-35C2-3 ... - Igor Chudov

More documents

Recommendations

Info

ARMY TM 9-6115-464-34AIR FORCE 35C2-3-445-2NAVY NAVFAC P-8-624-34Figure 3-80. Electro-Hydraulic Governor Control Unit Parallel Winding Test Circuit(2) Position governor control unit to install threaded rod (6, figure 3-68), bracket (5), Iockwashers (4),nuts (3), Iockwashers (2) and nuts (1).(3) Connect electrical connectors to governor control unit and untag.NOTEDesired speeds must be obtained by trial and error adjustments of linkage, position ofcontrol arm and performing the alignment procedures in paragraph 3-64j.j. Alignment Procedure. See figure 3-83 for identification of controls and perform the following procedures.(1) Set R11, R14, R16 and R18 rheostats at mid-point.(2) Set R15 full counterclockwise.(3) Set R12 approximately 3/4 turn counterclockwise.(4) Refer to Unit Maintenance Manual and start engine. If engine oscillates rapidly, adjust R16 and R18until operation is stable.(5) Once set has been stabilized, adjust R1 rheostat on control panel to obtain 60 Hz or 400 Hz.(6) Connect a dc voltmeter with 0-10 volt range across test points 3 and 4. Test point 4 is positive.Adjust R14 until voltage across test points 3 and 4 is zero at no load.3-180
ARMY TM 9-6115-464-34AIR FORCE TO 35C2-3-445-2NAVY NAVFAC P-8-624-34(7) Connect dc voltmeter across test points 1 and 2. Test point 1 is positive. Adjust R11 for zero volts at60 Hz or 400 Hz at no load. Repeat adjustment until voltage across test points 1 and 2 and 3 and 4is zero and frequency is 60 Hz or 400 Hz.NOTEIf test points 1 and 2 cannot be zeroed, they must be reduced to a minimum,(8) Adjust R12 to give approximately 5 volts across test points A and B.(9) Adjust R15 for optimum transient performance. Fully clockwise position is maximum loadmeasurement gain.(10) Set R18 and R16 for stabilized performance at all load conditions. For optimum performance R18should be set as far counterclockwise as possible without causing an oscillation for any setting ofR15.(11) Increasing the load measurement gain R15 (turning in a clockwise direction) will improve transientperformance; therefore, it should be adjusted as high as possible. The adjustment of R18, R16, andR15 are interdependent. For any position of R18, there is an optimum position for R16. Therefore, toimprove transient performance, increase the frequency gain by turning R18 clockwise. If a huntdevelops, readjust R16 for stability. If no hunt develops, apply and reject load to check for stabilityunder transient conditions.3-181
Page 1:
ARMY *TM 9-6115-464-34AIR FORCETO-3
Page 4 and 5:
ARMY TM 9-6115-464-34AIR FORCE 35C2
Page 7:
ARMY TM 9-6115 464 34AIR FORCE TO 3
Page 11 and 12:
ARMY TM 9-6115-464-34AIR FORCE TO 3
Page 13 and 14:
Page 15 and 16:
Page 17 and 18:
Page 19 and 20:
Page 21 and 22:
Page 23 and 24:
Page 25 and 26:
Page 27 and 28:
Page 29 and 30:
Page 31 and 32:
Table 1-1. FITS AND TOLERANCES (CON
Page 33:
Table 1-1. FITS AND TOLERANCES (CON
Page 36 and 37:
Page 38 and 39:
Page 40 and 41:
Page 42 and 43:
Page 44 and 45:
Page 46 and 47:
Page 48 and 49:
Page 50 and 51:
Page 52 and 53:
Page 54 and 55:
Page 56 and 57:
Page 58 and 59:
Page 60 and 61:
Page 62 and 63:
Page 64 and 65:
Page 66 and 67:
Page 68 and 69:
Page 70 and 71:
Page 72 and 73:
Page 74 and 75:
Page 76 and 77:
Page 78 and 79:
Page 80 and 81:
Page 82 and 83:
Page 84 and 85:
Page 86 and 87:
Page 88 and 89:
Page 90 and 91:
Page 92 and 93:
Page 94 and 95:
Page 96 and 97:
Page 98 and 99:
Page 100 and 101:
Page 102 and 103:
Page 104 and 105:
Page 106 and 107:
Page 108 and 109:
Page 110 and 111:
Page 112 and 113:
Page 114 and 115:
Page 116 and 117:
Page 118 and 119:
Page 120 and 121:
Page 122 and 123:
Page 124 and 125:
Page 126 and 127:
Page 128 and 129:
Page 130 and 131:
Page 132 and 133:
Page 134 and 135:
Page 136 and 137:
Page 138 and 139:
Page 140 and 141:
Page 142 and 143:
Page 144 and 145:
Page 146 and 147:
Page 148 and 149:
Page 150 and 151:
Page 152 and 153:
Page 154 and 155:
Page 156 and 157:
Page 158 and 159:
Page 160 and 161:
Page 162 and 163:
Page 164 and 165:
Page 166 and 167:
Page 168 and 169:
Page 170 and 171:
Page 172 and 173:
Page 174 and 175:
Page 176 and 177:
Page 178 and 179:
Page 180 and 181:
Page 182 and 183:
Page 184 and 185: ARMY TM 9-6115-464-34AIR FORCE 35C2
Page 268 and 269: ARMY TM 9-6115-464—34AIR FORCE 35
Page 284 and 285:
Page 286 and 287:
Page 288 and 289:
Page 290 and 291:
Page 292 and 293:
Page 294 and 295:
Page 296 and 297:
Page 298 and 299:
Page 300 and 301:
Page 302 and 303:
Page 304 and 305:
Page 306 and 307:
Page 308 and 309:
Page 310 and 311:
Page 312 and 313:
Page 314 and 315:
Page 316 and 317:
Page 318 and 319:
Page 320 and 321:
Page 322 and 323:
Page 324 and 325:
Page 326 and 327:
Page 328 and 329:
Page 330 and 331:
Page 332 and 333:
Page 334 and 335:
Page 336 and 337:
Page 338 and 339:
Page 340 and 341:
Page 342 and 343:
Page 344 and 345:
Page 346 and 347:
Page 348 and 349:
Page 350 and 351:
Page 352 and 353:
Page 354 and 355:
Page 356 and 357:
Page 358 and 359:
Page 360 and 361:
ARMY TM 9-6115-464—34AIR FORCE 35
Page 362 and 363:
Page 364 and 365:
(c)(d)(e)Pull all slack from the le
Page 366 and 367:
Page 368 and 369:
Page 370 and 371:
Page 372 and 373:
Page 374 and 375:
Page 376:
Page 379 and 380:
Page 381 and 382:
Page 383 and 384:
Page 385 and 386:
Page 387 and 388:
Page 389 and 390:
Page 391 and 392:
Page 393 and 394:
Page 395 and 396:
Page 397 and 398:
Page 399 and 400:
Page 401 and 402:
Page 404 and 405:
REPAIR INSTRUCTIONSARMY TM 9-6115-4
Page 406 and 407:
Page 408 and 409:
Page 410 and 411:
Page 412 and 413:
Page 414 and 415:
Page 416 and 417:
Page 418 and 419:
Page 420 and 421:
Page 422 and 423:
Page 424 and 425:
Page 426 and 427:
Page 428 and 429:
Page 430 and 431:
Page 432 and 433:
Page 434 and 435:
Page 436 and 437:
Page 438 and 439:
Page 440 and 441:
Page 442 and 443:
Page 444 and 445:
Page 446 and 447:
Page 448 and 449:
Page 450 and 451:
Page 452 and 453:
Page 454 and 455:
Page 456 and 457:
Page 458 and 459:
Page 460 and 461:
Page 462 and 463:
Page 464 and 465:
Page 466 and 467:
Page 468 and 469:
Page 470 and 471:
Page 472 and 473:
Page 474 and 475:
Page 476 and 477:
Page 478 and 479:
Page 480 and 481:
Page 482 and 483:
ARMY TM 9-6115 464 34AIR FORCE TO 3
Page 484 and 485:
Page 487 and 488:
Page 489 and 490:
Page 491:
ARMY TM 9-6115-464-34AIR FORCE TO-3
show all

ARMY *TM 9-6115-464-34 AIR FORCE TO-35C2-3 ... - Igor Chudov

You also want an ePaper? Increase the reach of your titles

Delete template?

Save as template?