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Packard 1A-1500

The Packard 1A-1500 was an American 12-cylinder liquid-cooled 60-degree Vee piston aircraft engine designed in 1924.[1] Test flown in the second prototype Douglas XO-2 it proved to be unreliable. Only 29 engines were built.

1A-1500
Type Liquid-cooled V-12 piston engine
Manufacturer Packard
First run 1924
Number built 29

Applications

Specifications (1A-1500)

Data from STATISTICS OF ALL THE AERO ENGINES OF PACKARD[2]

General characteristics

  • Type: V-12 liquid-cooled piston aircraft engine
  • Bore: 5+38 in (136.5 mm)
  • Stroke: 5+12 in (140 mm)
  • Displacement: 1,498 in3 (24.5 L)
  • Dry weight: 720 lb (326.5 kg)

Components

Performance

  • Power output: 500 hp (370 kW) at 2,000 rpm maximum continuous;520 hp (390 kW) at 2,200 rpm for takeoff
  • Specific power: 0.347 hp/cu in (15.8 kW/L)
  • Power-to-weight ratio: 0.722 hp/lb (1.187 kW/kg)

See also

Comparable engines

Related lists

References

Notes

  1. ^ Gunston 1989, p.109.
  2. ^ Neal, Bob. "STATISTICS OF ALL THE AERO ENGINES OF PACKARD" (pdf). Aircrqaft Engine Historical Society. Washington D.C. Retrieved 20 January 2018.

Bibliography

  • Gunston, Bill. World Encyclopedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. ISBN 1-85260-163-9

packard, 1500, american, cylinder, liquid, cooled, degree, piston, aircraft, engine, designed, 1924, test, flown, second, prototype, douglas, proved, unreliable, only, engines, were, built, 1500type, liquid, cooled, piston, enginemanufacturer, packardfirst, 19. The Packard 1A 1500 was an American 12 cylinder liquid cooled 60 degree Vee piston aircraft engine designed in 1924 1 Test flown in the second prototype Douglas XO 2 it proved to be unreliable Only 29 engines were built 1A 1500Type Liquid cooled V 12 piston engineManufacturer PackardFirst run 1924Number built 29 Contents 1 Applications 2 Specifications 1A 1500 2 1 General characteristics 2 2 Components 2 3 Performance 3 See also 4 References 4 1 Notes 4 2 BibliographyApplications EditBoeing Model 15 Boeing XP 4 Curtiss Falcon Douglas XO 2 Loening OLSpecifications 1A 1500 EditData from STATISTICS OF ALL THE AERO ENGINES OF PACKARD 2 General characteristics Type V 12 liquid cooled piston aircraft engine Bore 5 3 8 in 136 5 mm Stroke 5 1 2 in 140 mm Displacement 1 498 in3 24 5 L Dry weight 720 lb 326 5 kg Components Valvetrain Four valves per cylinder overhead camshaft Cooling system Liquid cooledPerformance Power output 500 hp 370 kW at 2 000 rpm maximum continuous 520 hp 390 kW at 2 200 rpm for takeoff Specific power 0 347 hp cu in 15 8 kW L Power to weight ratio 0 722 hp lb 1 187 kW kg See also EditPackard 1A 2500Comparable engines Curtiss D 12 Fairey Prince V 12 Rolls Royce KestrelRelated lists List of aircraft enginesReferences EditNotes Edit Gunston 1989 p 109 Neal Bob STATISTICS OF ALL THE AERO ENGINES OF PACKARD pdf Aircrqaft Engine Historical Society Washington D C Retrieved 20 January 2018 Bibliography Edit Gunston Bill World Encyclopedia of Aero Engines Cambridge England Patrick Stephens Limited 1989 ISBN 1 85260 163 9 Aircraft Engine Historical Society Retrieved from https en wikipedia org w index php title Packard 1A 1500 amp oldid 1111462244, wikipedia, wiki, book, books, library,

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