- Source: Walter Major
Walter Major was a family of Czechoslovak aircraft inline engines developed by Walter Aircraft Engines in the 1930s.
Design and development
Available in either four or six cylinder configuration, with identical bore and stroke of 118 mm (4.6 in) and 140 mm (5.5 in), respectively, the Walter Majors were primarily used in light aircraft. License-built in Poland by the state-owned Państwowe Zakłady Inżynieryjne (as the PZInż. Major 4), the engine was used in, among others, Zlin Z-XIII, RWD-11 and one of the PWS-35 Ogar prototypes.
Applications
= Walter Major 4
=Beneš-Mráz Be-50 Beta-Minor
Beneš-Mráz Be-52
Beneš-Mráz Be-56
Beneš-Mráz Be-250
Beneš-Mráz Be-251
González Gil-Pazó GP-4
PWS-35 Ogar
RWD 13
RWD 20
Spartan Cruiser
Zlin Z-XIII
Rubik R-18 Kánya
= Walter Major 6
=Breda Ba.44
Caproni Ca.308 Borea
RWD 11
Rogožarski SIM-XII-H
Specifications (Major 4)
Data from [1]
= General characteristics
=Type: 4-cylinder inverted inline engine
Bore: 118 mm
Stroke: 140 mm
Dry weight: 140 kg
= Components
=Cooling system: Air-cooled
= Performance
=Power output: 130 hp
Compression ratio: 5.2:1
See also
Comparable engines
de Havilland Gipsy Major
de Havilland Gipsy Six
Related lists
List of aircraft engines
External links
Oldengine.org
valka.cz
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