fbpx
Wikipedia

Franklin O-265

The Franklin O-265 (company designation 6AC-264) was an American air-cooled aircraft engine of the early 1940s. The engine was of six-cylinder, horizontally-opposed layout and displaced 265 cu in (4 L). The power output ranged between 120 hp (89 kW) and 140 hp (104 kW) depending on variant. The 6ACG-264 featured a geared propeller drive.

O-265/6AC-264
Type Piston aircraft engine
National origin United States
Manufacturer Franklin Engine Company
First run 1940

Variants edit

6AC-264
110 hp (82 kW) at 2,600 rpm
6ACG-264
138 hp (103 kW) at 3,100 rpm

Applications edit

Specifications (6AC-264) edit

Data from[citation needed]

General characteristics

Components

  • Cooling system: Air-cooled

Performance

  • Power output: 120 hp (89 kW) at 2,600 rpm

See also edit

Comparable engines

Related lists

References edit

Notes
Bibliography
  • Gunston, Bill. (1986) World Encyclopedia of Aero Engines. Patrick Stephens: Wellingborough. p. 57

franklin, company, designation, american, cooled, aircraft, engine, early, 1940s, engine, cylinder, horizontally, opposed, layout, displaced, power, output, ranged, between, depending, variant, 6acg, featured, geared, propeller, drive, 264type, piston, aircraf. The Franklin O 265 company designation 6AC 264 was an American air cooled aircraft engine of the early 1940s The engine was of six cylinder horizontally opposed layout and displaced 265 cu in 4 L The power output ranged between 120 hp 89 kW and 140 hp 104 kW depending on variant The 6ACG 264 featured a geared propeller drive O 265 6AC 264Type Piston aircraft engineNational origin United StatesManufacturer Franklin Engine CompanyFirst run 1940 Contents 1 Variants 2 Applications 3 Specifications 6AC 264 3 1 General characteristics 3 2 Components 3 3 Performance 4 See also 5 ReferencesVariants edit6AC 264 110 hp 82 kW at 2 600 rpm6ACG 264 138 hp 103 kW at 3 100 rpmApplications editBellanca Cruisair Northrop N 1M Vultee Stinson Model 75Specifications 6AC 264 editData from citation needed General characteristics Type 6 cylinder air cooled horizontally opposed aircraft piston engine Bore 4 0 in 101 6 mm Stroke 3 5 in 88 9 mm Displacement 263 9 in 4 32 L Dry weight 248 lb 112 kg Components Cooling system Air cooledPerformance Power output 120 hp 89 kW at 2 600 rpmSee also editComparable engines Continental O 280Related lists List of aircraft enginesReferences editNotes BibliographyGunston Bill 1986 World Encyclopedia of Aero Engines Patrick Stephens Wellingborough p 57 Retrieved from https en wikipedia org w index php title Franklin O 265 amp oldid 1166941722, wikipedia, wiki, book, books, library,

article

, read, download, free, free download, mp3, video, mp4, 3gp, jpg, jpeg, gif, png, picture, music, song, movie, book, game, games.