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ULPower
ULPower Aero Engines is a Belgium, Belgian company which manufactures engines specifically designed for light aircraft/rotorcraft use. History In 2001 the founding partners of ULPower were asked to fix an issue with a Jabiru 2200, Jabiru engine fitted into a helicopter. By examining the setup they decided to build a new engine from scratch instead, because the particular Jabiru engine simply was too small for the application. The new engine should have the following aims and objectives: FADEC, simple, robust, easy to maintain, low parts count, high power to weight ratio and low cost of ownership. The founding partners had years of experience in the professional automotive rally industry. This included engine design, development and production for the Dakar Rally and a proprietary Electronic control unit, ECU Based on the years of engine experience from Rally, the prototype helicopter engine and the proprietary Electronic control unit, ECU, they decided to form a company producing ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
ULPower Logo
ULPower Aero Engines is a Belgium, Belgian company which manufactures engines specifically designed for light aircraft/rotorcraft use. History In 2001 the founding partners of ULPower were asked to fix an issue with a Jabiru 2200, Jabiru engine fitted into a helicopter. By examining the setup they decided to build a new engine from scratch instead, because the particular Jabiru engine simply was too small for the application. The new engine should have the following aims and objectives: FADEC, simple, robust, easy to maintain, low parts count, high power to weight ratio and low cost of ownership. The founding partners had years of experience in the professional automotive rally industry. This included engine design, development and production for the Dakar Rally and a proprietary Electronic control unit, ECU Based on the years of engine experience from Rally, the prototype helicopter engine and the proprietary Electronic control unit, ECU, they decided to form a company producing ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
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 * Pe ... [...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] |
UL260iSA
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] |
UL260iF
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] |
UL260iS
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] |
UL350iHPS
The ULPower UL350i is a Belgian aircraft engine, designed and produced by ULPower Aero Engines of Geluveld for use in ultralight and homebuilt aircraft.Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', pages 242-243. WDLA UK, Lancaster UK, 2011. Design and development The engine is a four-cylinder, four-stroke, horizontally-opposed, , air-cooled, direct drive, gasoline engine design. It employs dual electronic ignition, multi-point EFI and produces at 3300 rpm. Variants ;UL350i :Base model that produces at 3300 rpm. ;UL350iS :Higher compression model that produces at 3300 rpm. ;UL350iSA :Same as UL350iS but with inverted oil system for aerobatic use. ;UL350iHPS :Special version for helicopter use. It produces at 3500 rpm. Applications * BRM Aero Bristell *Rans S-20 Raven *Rokospol Via The Rokospol Via is a Czech ultralight and light-sport aircraft (LSA), designed and produced by Rokospol Aviation of Prague, introduced at the ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
UL350iSA
The ULPower UL350i is a Belgian aircraft engine, designed and produced by ULPower Aero Engines of Geluveld for use in ultralight and homebuilt aircraft.Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', pages 242-243. WDLA UK, Lancaster UK, 2011. Design and development The engine is a four-cylinder, four-stroke, horizontally-opposed, , air-cooled, direct drive, gasoline engine design. It employs dual electronic ignition, multi-point EFI and produces at 3300 rpm. Variants ;UL350i :Base model that produces at 3300 rpm. ;UL350iS :Higher compression model that produces at 3300 rpm. ;UL350iSA :Same as UL350iS but with inverted oil system for aerobatic use. ;UL350iHPS :Special version for helicopter use. It produces at 3500 rpm. Applications * BRM Aero Bristell *Rans S-20 Raven *Rokospol Via The Rokospol Via is a Czech ultralight and light-sport aircraft (LSA), designed and produced by Rokospol Aviation of Prague, introduced at the ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
UL350i
The ULPower UL350i is a Belgian aircraft engine, designed and produced by ULPower Aero Engines of Geluveld for use in ultralight and homebuilt aircraft.Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', pages 242-243. WDLA UK, Lancaster UK, 2011. Design and development The engine is a four-cylinder, four-stroke, horizontally-opposed, , air-cooled, direct drive, gasoline engine design. It employs dual electronic ignition, multi-point EFI and produces at 3300 rpm. Variants ;UL350i :Base model that produces at 3300 rpm. ;UL350iS :Higher compression model that produces at 3300 rpm. ;UL350iSA :Same as UL350iS but with inverted oil system for aerobatic use. ;UL350iHPS :Special version for helicopter use. It produces at 3500 rpm. Applications * BRM Aero Bristell *Rans S-20 Raven *Rokospol Via The Rokospol Via is a Czech ultralight and light-sport aircraft (LSA), designed and produced by Rokospol Aviation of Prague, introduced at the ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
UL390i
The ULPower UL390i is a Belgian aircraft engine, designed and produced by ULPower Aero Engines of Geluveld for use in homebuilt aircraft.Tacke, Willi; Marino Boric; et al: ''World Directory of Light Aviation 2015-16'', pages 262-263. Flying Pages Europe SARL, 2015. Design and development The engine is a six-cylinder four-stroke, horizontally-opposed, displacement, air-cooled, direct-drive, gasoline engine design. It employs dual electronic ignition and produces at 3300 rpm. Variants ;UL390i :Base model with fuel injection and a compression ratio The compression ratio is the ratio between the volume of the cylinder and combustion chamber in an internal combustion engine at their maximum and minimum values. A fundamental specification for such engines, it is measured two ways: the stati ... of 8.2:1, producing at 3300 rpm ;UL390iS :Model with fuel injection and a 9.1:1 compression ratio, producing at 3300 rpm ;UL390iA :Inverted oil system version of the UL390iS, produ ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
UL350iS
The ULPower UL350i is a Belgian aircraft engine, designed and produced by ULPower Aero Engines of Geluveld for use in ultralight and homebuilt aircraft.Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', pages 242-243. WDLA UK, Lancaster UK, 2011. Design and development The engine is a four-cylinder, four-stroke, horizontally-opposed, , air-cooled, direct drive, gasoline engine design. It employs dual electronic ignition, multi-point EFI and produces at 3300 rpm. Variants ;UL350i :Base model that produces at 3300 rpm. ;UL350iS :Higher compression model that produces at 3300 rpm. ;UL350iSA :Same as UL350iS but with inverted oil system for aerobatic use. ;UL350iHPS :Special version for helicopter use. It produces at 3500 rpm. Applications * BRM Aero Bristell *Rans S-20 Raven *Rokospol Via The Rokospol Via is a Czech ultralight and light-sport aircraft (LSA), designed and produced by Rokospol Aviation of Prague, introduced at the ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
AMD Zodiac
The Zodiac is a family of Canadian all-metal, two-seat, fixed landing gear airplanes that first flew in 1984. The aircraft have been produced as kits and completed aircraft by Zenair in Canada and Zenith Aircraft Company in the US.Vandermeullen, Richard: ''2011 Kit Aircraft Buyer's Guide'', Kitplanes, Volume 28, Number 12, December 2011, page 77. Belvoir Publications. ISSN 0891-1851 The latest models in the Zodiac family are the ready-to-fly AMD Zodiac LS and LSi produced by Aircraft Manufacturing and Design. The design has a single-piece bubble canopy. Development The Zodiac was developed by Avions Pierre Robin engineer Chris Heintz in the early 1970s. The Zenair CH 200 kit plane was developed as a Homebuilt aircraft, meaning that consumers can purchase the plane as components to assemble it themselves. Variants of the Zodiac have since been manufactured in Canada, Europe, the United States and South America as a factory-assembled, ready-to-fly aircraft. The original Zo ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
