MOTORSTAR ENGINES
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9 Condorilor Street, Bacau, Romania Tel./ Fax. : +40234550510 e-mail: [email protected] M-14P AIRCRAFT ENGINE TECHNICAL SPECIFICATION MOTORSTAR ENGINES M-14PF AIRCRAFT ENGINE TECHNICAL SPECIFICATION Ø dry engine weight___________236 kg with all the accessories Ø number of cylinders___________9 radial cylinder Ø piston diameter______________105 mm Ø piston travel________________130 mm Ø total displacement____________10.16 l Ø compression ratio_____________6.3:1 Ø sense of rotation_________ clockwise (looking from front) Ø starting system_______________ compressed air Ø ignition system_______________ dual magnetos M-9F Ø sequence of ignition____________1-3-5-7-9-2-4-6-8 Ø ignition timing ________________23 0 BTC Ø carburetor type_______________ AK-14P fully inverted Ø fuel pump___________________ rotary type Ø oil system___________________ pressure & scavenge pump Ø power______________________360 HP at 2900 r.p.m Ø dry engine weight______________236 kg with all the accessories Ø number of cylinders_________9 radial cylinder Ø piston diameter____________105 mm Ø piston travel______________130 mm Ø total displacement__________10.16 l Ø power__________________400 HP at 2900 r.p.m Ø sense of rotation_________ clockwise (looking from front) Ø starting system____________ compressed air Ø ignition system____________ dual magnetos M-9F Ø sequence of ignition_________1-3-5-7-9-2-4-6-8 Ø ignition timing _____________23 0 BTC Ø carburetor type____________ AK-14P fully inverted Ø fuel pump________________ rotary type Ø oil system_________________pressure & scavengepump
Transcript of MOTORSTAR ENGINES
9 Condorilor Street, Bacau, RomaniaTel./ Fax. : +40234550510e-mail: [email protected]
M-14P AIRCRAFT ENGINE
TECHNICAL SPECIFICATION
MOTORSTAR ENGINES
M-14PF AIRCRAFT ENGINE
TECHNICAL SPECIFICATION
Ø dry engine weight___________236 kg with all the accessories
Ø number of cylinders___________9 radial cylinder Ø piston diameter______________105 mm Ø piston travel________________130 mm Ø total displacement____________10.16 l Ø compression ratio_____________6.3:1 Ø sense of rotation_________ clockwise (looking from front) Ø starting system_______________ compressed air Ø ignition system_______________ dual magnetos M-9F Ø sequence of ignition____________1-3-5-7-9-2-4-6-8 Ø ignition timing ________________230BTC Ø carburetor type_______________ AK-14P fully inverted Ø fuel pump___________________ rotary type Ø oil system___________________ pressure & scavenge pump Ø power______________________360 HP at 2900 r.p.m Ø dry engine weight______________236 kg with all the accessories
Ø number of cylinders_________9 radial cylinder Ø piston diameter____________105 mm Ø piston travel______________130 mm Ø total displacement__________10.16 l Ø power__________________400 HP at 2900 r.p.m Ø sense of rotation_________ clockwise (looking from front) Ø starting system____________ compressed air Ø ignition system____________ dual magnetos M-9F Ø sequence of ignition_________1-3-5-7-9-2-4-6-8 Ø ignition timing _____________230BTC Ø carburetor type____________ AK-14P fully inverted Ø fuel pump________________ rotary type Ø oil system_________________pressure & scavengepump
M-14D AIRCRAFT ENGINE
TECHNICAL SPECIFICATION
ELECTRIC START OPTION FOR M-14P
AND M-14PF AIRCRAFT ENGINES
9 Condorilor Street, Bacau, RomaniaTel./ Fax. : +40234550510e-mail: [email protected]
Ø number of cylinders______9 radial cylinder Ø piston diameter_________105 mm Ø piston travel____________130 mm Ø total displacement_______10.16 l Ø compression ratio________6.3:1 Ø sense of rotation_________ clockwise (looking from front) Ø starting system_________ compressed air Ø ignition system_________ dual magnetos M9-35M Ø sequence of ignition______1-3-5-7-9-2-4-6-8 Ø ignition timing __________230BTC Ø carburetor type_________ AK-14V fully inverted Ø fuel pump_____________ rotary type Ø oil system_____________ pressure & scavenge pump Ø power________________220 HP at 2000 r.p.m Ø dry engine weight________216 kg with all the accessories
