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Aeromarine B-90

The Aeromarine B-90 is an aircraft engine built by the Aeromarine Plane and Motor Company in 1915. Aeromarine made two series of V-8 engines. The B series was developed by Joseph Boland and the L series by Charles F. Willard.[1][2][3]

B-90
Aeromarine B-90
Type V-8 piston engine
National origin United States
Manufacturer Aeromarine
First run 1915
Variants Aeromarine B-45

Specifications edit

Data from Airplane Engine Encyclopedia[3]

General characteristics

Components

  • Valvetrain: 2 intake and 2 exhaust valves per cylinder, single DOHC camshaft operating rockers
  • Fuel system: Single 1.75 in. duplex Zenith carburetor
  • Fuel type: gasoline
  • Oil system: triple gear pump pressure system; HP to crankshaft; LP to camshaft; LP to oil cooler in radiator
  • Cooling system: Water
  • Reduction gear: .571:1
  • Ignition: 2 Dixie magnetos

Performance

References edit

  1. ^ "Motors". www.aerofiles.com. Retrieved 2018-03-23.
  2. ^ Faurote, Fay Leone (1919). Aircraft Year Book. American Aviation Publications.
  3. ^ a b Angle, Glenn D. (1921). Airplane Engine Encyclopedia. Dayton, Ohio: THE OTTERBEIN PRESS. pp. 23–24.

aeromarine, aircraft, engine, built, aeromarine, plane, motor, company, 1915, aeromarine, made, series, engines, series, developed, joseph, boland, series, charles, willard, 90type, piston, enginenational, origin, united, statesmanufacturer, aeromarinefirst, 1. The Aeromarine B 90 is an aircraft engine built by the Aeromarine Plane and Motor Company in 1915 Aeromarine made two series of V 8 engines The B series was developed by Joseph Boland and the L series by Charles F Willard 1 2 3 B 90Aeromarine B 90Type V 8 piston engineNational origin United StatesManufacturer AeromarineFirst run 1915Variants Aeromarine B 45 Contents 1 Specifications 1 1 General characteristics 1 2 Components 1 3 Performance 2 ReferencesSpecifications editData from Airplane Engine Encyclopedia 3 General characteristics Type 8 cylinder 90 Vee piston engine Bore 3 625 in 92 08 mm Stroke 5 125 in 130 18 mm Displacement 423 2 cu in 6 94 L Dry weight 460 lb 210 kg Designer Joseph BolandComponents Valvetrain 2 intake and 2 exhaust valves per cylinder single DOHC camshaft operating rockers Fuel system Single 1 75 in duplex Zenith carburetor Fuel type gasoline Oil system triple gear pump pressure system HP to crankshaft LP to camshaft LP to oil cooler in radiator Cooling system Water Reduction gear 571 1 Ignition 2 Dixie magnetosPerformance Power output maximum 166 hp 124 kW nominal at 2 635 rpm Compression ratio 5 to 1 Power to weight ratio 0 3226 hp lb 0 5304 kW kg References edit Motors www aerofiles com Retrieved 2018 03 23 Faurote Fay Leone 1919 Aircraft Year Book American Aviation Publications a b Angle Glenn D 1921 Airplane Engine Encyclopedia Dayton Ohio THE OTTERBEIN PRESS pp 23 24 nbsp Wikimedia Commons has media related to Aeromarine B 90 Retrieved from https en wikipedia org w index php title Aeromarine B 90 amp oldid 1125780561, wikipedia, wiki, book, books, library,

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