Drive System Flashcards
General
Consists of:
- Engine transmissions
- Combining transmission
- Forward transmission
- Aft transmission
Primary function is to transmit engine output to rotor system. Secondary function is to drive AC generators, hydraulic pumps, transmission oil pumps, tach gen, and transmission oil cooler fan
Engine shafts to c box, 7 sync shafts from c box to forward transmission, 2 sync shaft from c box to aft transmission, vert shaft from aft transmission to aft rotor head, fan drive shaft, cooling fan, and rotor brake near c box
Each transmission has a separate primary and auxiliary lube system with sensors to detect temp, pressure, and metallic chips
Engine Drive Shafting
Connects output of engine to input pinion of c box
Each shaft made of aluminum tubing with each end connected with a flex coupling to compensate for minor misalignment
Both shafts are serial numbered and dynamically balanced
Aft Synch Drive Shafting
Connects aft output of c box to input pinion of aft transmission
2 shafts connecting with Thomas couplings and mounted to fuselage with lord mounts
Aft sync shafting is supported by a single bearing
Forward Synch Drive Shafting
7 shafts connecting forward output of c box to input pinion of forward transmission
Forward 6 Synch shafts are identical and interchangeable, 7th shaft is unique in that it doesn’t have a bearing and support assembly attached to it
All 7 shafts are interconnected with Thomas couplings and aluminum adaptors mounted to each end
Fan Drive Shafting
Transmits torque from aft transmission to transmission oil cooling fan
Extends diagonally up and forward from aft transmission at approximately a 45* angle
Aft Vertical Drive Shaft
Extends upward from aft transmission through aft pylon to aft rotor head. Shaft is splined to aft transmission output and is secured to airframe via thrust bearing
Each end of shaft is made of steel and pinned to carbon fiber center section
Center of rotor head is splined to aft vert shaft on the top
Aft Vert Shaft Thrust Bearing
Connects aft vert shaft with aft pylon structure
Distributes lift force from aft rotor system to airframe instead of aft transmission
Bearing assembly is pressure lubricated with oil from aft transmission lube system, and the oil return line contains a screen and chip detector
Transmission Oil Temp Indicating System
Consists of 5 temp bulbs, selector switch, and gauge
Each temp sensor from its corresponding input transistor is applied to logic circuit which is controlled by the selector switch. When switch is set to TEST, the output of the logic circuit is 0 volts, resulting in a 0 degree indication
When selector is set to SCAN the logic circuit compares the 5 temp signals and selects the highest reading
Transmission Oil Temp Warning System
5 thermal switches warn pilot of overtemp condition when transmission oil temp increases above 140*C, illuminating common XMSN OIL HOT. The switch is located in line just prior to their respective coolers
2 thermal switches monitor oil temp in sumps of No. 1 and 2 engine transmissions. They closes on temp above 207*C and light their associated annunciator (ENG # XMSN HOT)
Transmission Oil Pressure Indicating System
Consists of 5 transmission pressure transducers, switch assemblies, selector switch, and indicator dial
Logic circuit controlled by selector switch indicates pressure of transmission selected, and when set to SCAN it compares 5 pressure signals and selects the lowest pressure
Transmission Oil Pressure Warning System
5 identical oil pressure switches provide warning for underpressure condition. Contacts close on decreasing oil pressure below 18psig
When oil pressure drops below 18psig the associated pressure switch illuminates XMSN OIL PRESS light
Engine Transmissions
Mounted on front of engine, takes N2 output power from quill shaft and changes its direction 90 degrees to go into c box
Sprag clutch on output shaft permits freewheeling if Nr exceeds N2
Engine is lubricated from main and auxiliary oil pumps located in c box. Scavenge pump located on c box returns oil to its reservoir
Combining Transmission
Combines torque from both engine transmissions and changes its direction 90 degrees, distributing the power to output shafts to drive forward and aft transmissions.
3 section oil tank with common filler port provides primary and auxiliary lubrication for c box and engine transmissions. Accessory drive spur gear on forward output shaft provides drive for 6 element pump for 3 main oil pumps and 3 scavenge oil pumps. Auxiliary lube pumps for c box and engine transmissions are punted on same accessory drive and are visible on exterior of c box
Caliber assembly for rotor brake is on rear cover of c box, with calipers working against disc mounted on splined adapter to aft output shaft
Engine and Combining Transmission Primary Lubrication
3 compartment tank on top of c box supplies oil to engine transmissions and c box. Tank is approx 10 gallons
Within c box main oil pumps for each transmission provide pressure to their respective engine, passing oil through an oil filter, 2 oil coolers, and in line jet protection screen before passing onto lube jets. Scavenge oil pump is provided for each transmission to return oil to reservoir
Chip detectors located in transmission sump with burn off system, to prevent minute metallic particles. These illuminate XMSN CHIP DET and ENG CHIP DET lights, and to determine which transmission has chips the maintenance panel in aft fuselage area must be consulted
Engine/C Box Reservoir
1 big tank with 2 walls inside tank divide it into 3 separate chambers. Common filler and breather aperture is on top.
At the base of each compartment is combined temp bulb and overlay switch
Engine/C Box Pressure Pumps
3 pressure pump are housed within c box, and are driven from common shaft and each draws oil from its own section of reservoir
Extreme pressure is released by a relief valve for protection of system
Engine/C Box Filter
Filter mounted on rear side of c box, fitted to its respective pump outlet
Bypass indicator pops out to indicate blockage in element and oil will bypass filter to the system
Engine/C Box Oil Coolers
2 coolers attached to rear pylon and each is made of 3 separate sections. Each pump delivers oil to section of one then the other cooler
Bypass valve attached to each cooler inlet acts as thermal control valve and opens at temps below approx 70*C. Valve also acts as safety bypass should cooler becomes blocked