WinGD X62DF-S2.0 - Page 12

Marine Installation Manual 2022-03 ix
List of Figures
X62DF-S2.0
List of Figures
0-1 GTD screenshot . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 0-4
1-1 Power/speed range of the WinGD X-DF engines . . . . . . . . . . . . . . . . . . 1-5
1-2 Principal engine dimensions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-7
1-3 Operating modes of the X-DF2.0 engine with iCER gas mode . . . . . . . 1-8
1-4 Operating modes of the X-DF2.0 engine with iCER gas and diesel
Tier III mode . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-9
1-5 Gas mode operation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-10
1-6 The iCER system with one turbocharger. . . . . . . . . . . . . . . . . . . . . . . . . 1-12
1-7 The iCER system with two turbochargers . . . . . . . . . . . . . . . . . . . . . . . . 1-12
1-8 The Flex system parts . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-13
1-9 Diesel fuel ratio during active CSM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-14
1-10 Fuel sharing mode — available operating window. . . . . . . . . . . . . . . . . 1-15
1-11 Fuel sharing mode — energy amount of different ratios of fuel . . . . . . 1-16
1-12 Fuel transfers and gas trips . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-17
2-1 Rating field for the X62DF-S2.0. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-1
2-2 Propeller curves and operational points . . . . . . . . . . . . . . . . . . . . . . . . . 2-4
2-3 Power range limits . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-6
2-4 Power range diagram of an engine with a PTO. . . . . . . . . . . . . . . . . . . . 2-10
2-5 Power range limits for PTO operation — Method 1 . . . . . . . . . . . . . . . . 2-11
2-6 Power range limits for PTO operation — Method 2 . . . . . . . . . . . . . . . . 2-12
2-7 The prohibited operation area (CMCR speed = R1—R2) . . . . . . . . . . . . 2-13
2-8 Calculating the prohibited operation area for the CMCR speed . . . . . . 2-15
2-9 The prohibited operation area (CMCR speed = 85% of R1—R2) . . . . . 2-16
2-10 The prohibited operation area (CMCR speed = R3—R4) . . . . . . . . . . . . 2-17
3-1 Engine dimensions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-1
3-2 Thermal expansion, dim. X, Y, Z . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-3
3-3 Minimum requirements for headroom . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-9
3-4 Force transmission to the engine foundation . . . . . . . . . . . . . . . . . . . . . 3-10