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Weslake A80
The Weslake A80 is a liquid cooled, two-stroke, opposed piston, 1332 cc Diesel aircraft engine An aircraft engine, often referred to as an aero engine, is the power component of an aircraft propulsion system. Most aircraft engines are either piston engines or gas turbines, although a few have been rocket powered and in recent years many ..., produced by Weslake.Weslake factsheet August 2104Tacke, Willi; Marino Boric; et al: ''World Directory of Light Aviation 2015-16'', pages 262-263. Flying Pages Europe SARL, 2015. Design and development This opposed piston aero-engine appears superficially similar to a true flat-four "boxer" engine, but is actually significantly different. It has two ported cylinders with a crankshaft at each end and four pistons in total. This engine is similar to the prototype Diesel Air engine, which was built for Diesel Air by Weslake, but which has to date failed to reach volume production. Each crankshaft is linked by an idler gear to a ce ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Opposed-piston Engine
An opposed-piston engine is a piston engine in which each cylinder has a piston at both ends, and no cylinder head. Petrol and diesel opposed-piston engines have been used mostly in large-scale applications such as ships, military tanks, and factories. Current manufacturers of opposed-piston engines include Fairbanks-Morse, Cummins and Achates Power. Design Compared to contemporary two-stroke engines, which used a conventional design of one piston per cylinder, the advantages of the opposed-piston engine have been recognized as: * Eliminating the cylinder head and valvetrain, which reduces weight, complexity, cost, heat loss, and friction loss of the engine. * Creating a uniflow-scavenged movement of gas through the combustion chamber, which avoided the drawbacks associated with the contemporary crossflow-scavenged designs (however later advancements have provided methods for achieving uniflow scavenging in conventional piston engine designs). * A reduced height of the e ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
KFM 112M
The KFM 112M is a four-cylinder, four-stroke, dual ignition, horizontally opposed aircraft engine designed for ultralight aircraft and motor gliders. The engine was designed and produced by the KFM (Komet Flight Motor) Aircraft Motors Division of Italian American Motor Engineering of Italy as a follow-on engine to their KFM 107 series and has been out of production since 1990. Development The KFM 112 is a conventional four-cylinder engine that is very compact and lightweight at only , including the starter, alternator and carburetor. The engine features dual electronic ignition, a single OVC carburetor, hydraulic valve lifters, nickel-silicon treated cylinders and bi-metallic valves with chromed stems. It was offered without a reduction system. Starting is electric starter only. The engine produces at 3400 rpm for three minutes for take-off, at 3200 rpm for five minutes and at 3090 rpm continuous. Applications *Partenavia P.86 Mosquito Specifications (112 ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Two-stroke Diesel Engines
A two-stroke (or two-stroke cycle) engine is a type of internal combustion engine that completes a power cycle with two strokes (up and down movements) of the piston during one power cycle, this power cycle being completed in one revolution of the crankshaft. A four-stroke engine requires four strokes of the piston to complete a power cycle during two crankshaft revolutions. In a two-stroke engine, the end of the combustion stroke and the beginning of the compression stroke happen simultaneously, with the intake and exhaust (or scavenging) functions occurring at the same time. Two-stroke engines often have a high power-to-weight ratio, power being available in a narrow range of rotational speeds called the power band. Two-stroke engines have fewer moving parts than four-stroke engines. History The first commercial two-stroke engine involving cylinder compression is attributed to Scottish engineer Dugald Clerk, who patented his design in 1881. However, unlike most later two-st ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Verner 133M
The Verner VM 133 is a family of Czech two cylinder, horizontally opposed, four stroke aircraft engines, designed and built by Verner Motor of Šumperk.Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 22. WDLA UK, Lancaster UK, 2011. Design and development The 133M is based on the earlier Verner 1400 and uses a 12 volt 1000W electric starter and has a 12 volt 160W generator. It runs on 95 octane automobile fuel or 100LL Avgas. The recommended time between overhauls is 1000 hours. The engine was still advertised for sale on the company website in 2013, but by 2015 was no longer listed as available and it is likely that production has ended. Variants ;VM 133M :Original model ;VM 133MK :Improved model Applications * Airflow Twinbee *Airkraft Sunny *Aquilair Swing *Avid Catalina * Flitzer Z-21 * Rainbow Cheetah *SlipStream Genesis The SlipStream Genesis is a family of American, strut-braced, high wing, pusher configuration, t ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
ULPower UL260i
The ULPower UL260i is a family of aircraft engines, produced by ULPower in Belgium. Design The UL260i series are all lightweight, four-cylinder, four-stroke, horizontally-opposed, air-cooled, direct drive engine designs that feature FADEC with multipoint fuel injection and dual ignition systems.Tacke, Willi; Marino Boric; et al: ''World Directory of Light Aviation 2015-16'', pages 262-263. Flying Pages Europe SARL, 2015. Variants ;UL260i :Base model, fuel injection, compression ratio of 8.16:1, producing ;UL260iS :Model with a higher compression ratio of 9.10:1, fuel injection, producing ;UL260iSA :Aerobatic model with a higher compression ratio of 9.10:1, fuel injection, producing ;UL260iF :Model with a higher compression ratio of 9.10:1, fuel injection, producing , due to French regulatory requirements. Applications Specifications See also ;Related development * ULPower UL350i ;Lists * List of aircraft engines ;Comparable engines * HKS 700E * Jabiru 2200 * KFM 112M * P ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Sauer S 2100 ULT
The Sauer S 2100 ULT is a turbocharged four-stroke aircraft engine for homebuilt and ultralight aircraft. Sauer Flugmotorenbau GmbH Design and development The engine is based on the . It is extensively modified for aircraft use and all the parts are custom made. The engine is derived from the certified engines produced by the same manufacturer and used in several s and |
Sauer S 2400 UL
The Sauer S 2400 UL is a 4 stroke aircraft engine for Homebuilt aircraft, homebuilt and ultralight aircraft. Sauer Flugmotorenbau GmbH Design and development The engine is based on the Volkswagen air-cooled engine or the Wasserboxer. It is extensively modified for aircraft use and all the parts are custom made. The engine is derived from the certified engines produced by the same manufacturer and used in several motorgliders and small aircraft. The engine can be delivered with aluminium or magnesium casing (Wasserboxer-casing or the casing from the Volkswagen air-cooled engine, beetle engine), where the aluminium casing weighs 7 kg more.Applications *Groppo Trial Specifications (variant) |
Sauer S 2200 UL
The Sauer (German and Luxembourgish, , ) or Sûre (French, ) is a river in Belgium, Luxembourg and Germany. A left tributary of the Moselle, its total length is . Rising near Vaux-sur-Sûre in the Ardennes in southeastern Belgium, the Sauer flows eastwards and becomes the border with Luxembourg near Martelange. It forms the border between Belgium and Luxembourg for north of Martelange. West of Esch-sur-Sûre it flows into an artificial lake, the Upper Sûre Lake created by the Esch-sur-Sûre Dam, which gives its (French) name to the Luxembourgian commune of Lac de la Haute-Sûre. After flowing through Ettelbruck and Diekirch, the Sauer forms the border between Luxembourg and Germany for the last of its course, passing Echternach before emptying into the Moselle in Wasserbillig. The rivers Wiltz, Alzette, White Ernz, Black Ernz, Our, and Prüm Prüm () is a town in the Westeifel (Rhineland-Palatinate), Germany. Formerly a district capital, today it is the administrati ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Rotax 912
The Rotax 912 is a horizontally-opposed four-cylinder, naturally aspirated, four-stroke aircraft engine with a reduction gearbox. It features liquid-cooled cylinder heads and air-cooled cylinders. Originally equipped with carburetors, later versions are fuel injected. Dominating the market for small aircraft and kitplanes, Rotax produced its 50,000th 912-series engine in 2014. Originally available only for light sport aircraft, ultralight aircraft, autogyros and drones, the 912-series engine was approved for certified aircraft in 1995. Design and development The Rotax 912 was first sold in 1989 in non- certificated form for use in ultralights and motorgliders. The original 912 UL engine has a capacity of and a compression ratio of 9.1:1. The engine differs from previous generation aircraft engines (such as the Lycoming O-235) in that it has air-cooled cylinders with liquid-cooled heads and uses a 2.43:1 PSRU reduction gearbox to reduce the engine's relatively high 5 ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Revmaster R-2300
The Revmaster R-2300 is a 4 stroke aircraft engine for Homebuilt aircraft Design and development The engine is based on the Volkswagen air-cooled engine. It is extensively modified for aircraft use. This modification consists of a quad CDI ignition (8 coils), new and enlarged #4 bearing, custom made crank shaft and cam shaft, custom made cylinder heads and other modifications.EAA Experimenter EAA Experimenter The engine is delivered completely assembled and test run from the factory (it is not delivered as a kit). Applications * Thatcher CX5[...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Jabiru 2200
The Jabiru 2200 is a lightweight naturally aspirated, pushrod four-stroke, flat four, air-cooled aircraft engine produced by Jabiru Aircraft. Design and development The conventional direct-drive engine is fitted with an alternator, silencers, vacuum pump drives and dual ignition systems as standard. The engine generates up to 80 bhp at 3,300 rpm. In Europe the engine competes with the Rotax 912, another flat four four-stroke engine, but one that has water-cooled cylinder heads and a geared reduction drive to the propeller. Jabiru Aircraft began as a builder of small two-seater aircraft in Bundaberg, Australia. It turned to producing its own engines when supplies of the Italian-sourced engines previously used dried up. Jabiru engines are designed to be manufactured in small batch quantities, so the firm uses CNC machines to mill major engine parts such as cylinder blocks and heads, rather than using cast items. A larger variant of this engine is the flat-six Jabiru 3300 w ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
