Lycoming O-235

from Wikipedia, the free encyclopedia
Lycoming
A Lycoming O-235-C2C

A Lycoming O-235-C2C

Lycoming O-235
Production period: since 1940
Manufacturer: Lycoming
Working principle: Otto
Motor design: Four - cylinder boxer engine
Displacement: 3816 cm 3
Mixture preparation: Carburetor
Engine charging: no
Power: 75 - 93 kW
Dimensions: 110-115 kg
Previous model: none
Successor: none

The Lycoming O-235 , originally called the Lycoming O-233, is a piston aircraft engine from the US manufacturer Lycoming .

construction

It is an air-cooled 4-stroke boxer engine with four cylinders. The bore is 111.1 mm and the stroke is 98.4 mm. This results in a displacement of 3816 cm³ (235 cubic inches). The propeller is driven directly. The compression is 6.75: 1 to 9.7: 1, depending on the variant. The engine was approved on August 26, 1940 and is still in production today.

The O 235 provides between 75 kW (100 hp) at 2450 min -1 and 93 kW (125 hp) at 2800 min -1 . Tens of thousands of examples of this engine have been built to date. It is one of the most widely used aerospace engines. Among other things, he came to the Beechcraft 77 , the Cessna 152 , Robin R3000 , Piper J-5 , Piper PA-12 and Piper PA-38 are used. In Germany it used z. B. Heini Dittmar to drive his Motor-Möwe HD-156 B and there are also two conversions to this motor on the Sokol M-1C and Sokol M-1D.

O-290

The Lycoming O-290 has the same dimensions as the O-235, but has an enlarged bore from 111 mm to 123.7 mm. The power increases to 135 hp (140 hp take-off power) at a speed of 2800 min −1 . The compression is 7.0: 1, the weight 120 kg.

Another engine from the manufacturer with the same bore and stroke is the Lycoming O-350 with six instead of four cylinders.

Web links

Commons : Lycoming O-235  - collection of images, videos and audio files

Individual evidence

  1. http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/c7bf8c45a9443a6686256e4d005e73c3/$FILE/E-223.pdf
  2. www.airweb.faa.gov (accessed December 11, 2012) (PDF; 538 kB)
  3. ^ Leonard Bridgman (ed.): Jane's All The World's Aircraft - 1959-60 , Sampson Low, Marston & Company Ltd., London, 1959, pp. 532 ff.