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Aeronca E-107

The Aeronca E-107 was one of the first low-cost reliable engines of the post-World War I era.[1]

E-107
E107 on display
Type Flat-twin aircraft engine
National origin United States of America
Manufacturer Aeronautical Corporation of America
Designer Ray Poole and Robert Galloway
First run 1929
Major applications Aeronca C-2
Number built 115
Variants Aeronca E-113

Design and development

 
An Aeronca C-2, with the E-107 "flathead" engine

The E-107A was a production aviation flathead engine designed to replace a Morehouse engine on the first prototype of the Aeronca C-2. The first five were produced without cooling fins on the crankcase, but with all versions having air-cooling fins atop the cylinder heads, similar to many air-cooled two-stroke engines in appearance. A Winfleld Model 5 carburetor was standard for the engine.[2] The E-107 was replaced by the uprated, overhead valvetrain E-113 engine based on the same design.[3]

Variants

E-107
Standard production engine
E-107A
The E-107A was produced for Aeronca by the Govro-Nelson Company of Detroit, Michigan.[2]
O-107
Designation given to engines fitted to impressed aircraft

Applications

Engines on display

Specifications (E-107)

Data from [5]

General characteristics

Components

  • Valvetrain: One inlet and one exhaust valve per cylinder, operated by tappets directly from the camshaft
  • Oil system: scavenged pressure feed.
  • Cooling system: air-cooled

Performance

  • Power output: 30 hp (22 kW) maximum at 2,500 rpm, (cruising at 2000 rpm)
  • Compression ratio: 4:1
  • Specific fuel consumption: 0.55 lb/hp (0.33 kg/kW)/hr at 2,000 rpm
  • Oil consumption: 0.21 lb/hp (0.13 kg/kW)/hr

See also

Comparable engines

Related lists

References

  1. ^ Janet Rose Daly Bednarek, Michael H. Bednarek. Dreams of flight: general aviation in the United States.
  2. ^ a b . Archived from the original on 4 July 2011. Retrieved 20 January 2012.
  3. ^ Kenneth M. Molson, National Aviation Museum (Canada). Canada's National Aviation Museum: its history and collections. p. 100.
  4. ^ "Aeronca C-2". Retrieved 20 January 2012.
  5. ^ Grey, C.G., ed. (1931). Jane's all the World's Aircraft 1931. London: Sampson Low, Marston & company, ltd. pp. 64d–65d.

aeronca, first, cost, reliable, engines, post, world, 107e107, displaytype, flat, twin, aircraft, enginenational, origin, united, states, americamanufacturer, aeronautical, corporation, americadesigner, poole, robert, gallowayfirst, 1929major, applications, ae. The Aeronca E 107 was one of the first low cost reliable engines of the post World War I era 1 E 107E107 on displayType Flat twin aircraft engineNational origin United States of AmericaManufacturer Aeronautical Corporation of AmericaDesigner Ray Poole and Robert GallowayFirst run 1929Major applications Aeronca C 2Number built 115Variants Aeronca E 113 Contents 1 Design and development 2 Variants 3 Applications 4 Engines on display 5 Specifications E 107 5 1 General characteristics 5 2 Components 5 3 Performance 6 See also 7 ReferencesDesign and development Edit An Aeronca C 2 with the E 107 flathead engine The E 107A was a production aviation flathead engine designed to replace a Morehouse engine on the first prototype of the Aeronca C 2 The first five were produced without cooling fins on the crankcase but with all versions having air cooling fins atop the cylinder heads similar to many air cooled two stroke engines in appearance A Winfleld Model 5 carburetor was standard for the engine 2 The E 107 was replaced by the uprated overhead valvetrain E 113 engine based on the same design 3 Variants EditE 107 Standard production engine E 107A The E 107A was produced for Aeronca by the Govro Nelson Company of Detroit Michigan 2 O 107 Designation given to engines fitted to impressed aircraftApplications EditAeronca C 2 Pickering Pearson KP 2Engines on display EditAn E 107 is on display at the EAA Airventure Museum in Oshkosh Wisconsin The restored first prototype Aeronca C 2 registration NC 626N fitted with an E 107 is on display at the Udvar Hazy building of the Smithsonian s National Air and Space Museum 4 Specifications E 107 EditData from 5 General characteristics Type 2 cyl air cooled horizontally opposed flathead engine Bore 4 5 in 110 mm Stroke 4 in 100 mm Displacement 107 cubic inches Dry weight 114 lb 52 kg Components Valvetrain One inlet and one exhaust valve per cylinder operated by tappets directly from the camshaft Oil system scavenged pressure feed Cooling system air cooledPerformance Power output 30 hp 22 kW maximum at 2 500 rpm cruising at 2000 rpm Compression ratio 4 1 Specific fuel consumption 0 55 lb hp 0 33 kg kW hr at 2 000 rpm Oil consumption 0 21 lb hp 0 13 kg kW hrSee also EditComparable engines Bristol Cherub Lawrance A 3Related lists List of aircraft enginesReferences Edit Wikimedia Commons has media related to Aeronca E 107 Janet Rose Daly Bednarek Michael H Bednarek Dreams of flight general aviation in the United States a b Aeronca E107A 39 Archived from the original on 4 July 2011 Retrieved 20 January 2012 Kenneth M Molson National Aviation Museum Canada Canada s National Aviation Museum its history and collections p 100 Aeronca C 2 Retrieved 20 January 2012 Grey C G ed 1931 Jane s all the World s Aircraft 1931 London Sampson Low Marston amp company ltd pp 64d 65d Retrieved from https en wikipedia org w index php title Aeronca E 107 amp oldid 1109077055, wikipedia, wiki, book, books, library,

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