OUTLINE
01–00–2
ENGINE FEATURES
CHU010002000S02
End Of Sie
ENGINE SPECIFICATIONS
CHU010002000S03
Improved power performance
•
A side intake and exhaust port system adopted
•
2-piece apex seals adopted
•
Keystone shaped side seals adopted
•
Cut-off seal adopted
•
A lightweight flywheel adopted
Improved driving performance
•
Advanced front mid-ship layout adopted
•
Drive-by-wire system, which opens and closes throttle valve by throttle actuator,
adopted
Improved engine torque and
output
•
Sequential dynamic air intake system (S-DAIS) adopted
Improved startability
•
A reduction type starter adopted
Reduced weight
•
Thin walls on the side housings adopted
•
Lightweight rotors adopted
•
Aluminum rotor housings adopted
•
Aluminum engine mount brackets adopted
•
A compact oil filter adopted
•
A thin oil pan made of steel adopted
•
An oil strainer made of plastic adopted
•
A down flow type radiator with aluminum core and plastic tank adopted
Miniaturization
•
A regulatorless generator with built-in power transistor adopted
•
A built-in type water pump adopted
Improved fuel economy
•
Bathtub shaped combustion chambers adopted
•
By-pass valve in the eccentric shaft adopted
•
Anti-wet port adopted
Improved idle fuel economy
•
Jet air fuel mixing system adopted
Reduced engine noise and
vibration
•
Oil-filled engine mount rubber adopted
•
A cooling fan with electric motor adopted
Improved reliability
•
A degassing type coolant reserve tank adopted
•
An independent ignition control system with distributorless ignition coil adopted
•
A battery duct adopted
Improved durability
•
A spark plug with an iridium tip adopted
Improved lubricity
•
A two-rotor type trochoid oil pump adopted
•
An electric type metering oil pump adopted
Improved safety
•
A starter interlock switch adopted (MT)
Improved serviceability
•
Nylon tubes adopted for fuel hoses in the engine compartment and around the fuel
tank, and quick release connectors adopted for joints
Wiring harness simplification
•
Controller area network (CAN) adopted
Reduction of evaporative gas
•
Returnless fuel system adopted
•
Evaporative purge control adopted
Improved exhaust purification
•
Secondary air injection (AIR) system with electric secondary air injection (AIR) pump
adopted
•
TWC system adopted
Item
Specifications
13B-MSP
(Standard power)
13B-MSP
(High power)
MECHANICAL
Engine type
Rotary
Rotor arrangement and number
In-line 2-rotor, longitudinal
Combustion chamber type
Bathtub
Displacement
(ml {cc, cu in})
654 {654, 40.0}
×
2
Compression ratio
10.0
Compression pressure
(kPa {kgf/cm
2
, psi} [rpm])
830 {8.5, 120}[250]
Содержание 2004 RX-8
Страница 11: ......
Страница 37: ...MECHANICAL 01 10 2 ENGINE STRUCTURAL VIEW CHU011001001S02 End Of Sie BHJ0110N002 ...
Страница 65: ......
Страница 91: ......
Страница 93: ......
Страница 113: ......
Страница 119: ......
Страница 189: ......
Страница 197: ......
Страница 201: ......
Страница 203: ......
Страница 205: ......
Страница 211: ......
Страница 213: ......
Страница 225: ......
Страница 231: ......
Страница 261: ......
Страница 265: ......
Страница 275: ......
Страница 279: ...MANUAL TRANSMISSION Y16M D 05 11 2 MANUAL TRANSMISSION POWER FLOW CHU051101025S03 1st 2nd 4th 3rd 5th 6th CHU0511S102 ...
Страница 291: ......
Страница 343: ......
Страница 349: ......
Страница 361: ......
Страница 371: ......
Страница 379: ......
Страница 381: ......
Страница 389: ......
Страница 403: ......
Страница 413: ......
Страница 417: ......
Страница 427: ......
Страница 450: ......
Страница 466: ......
Страница 516: ......
Страница 530: ......
Страница 540: ......