Weller ULI NG
{{Short description|German ultralight aircraft}}
{{Use dmy dates|date=January 2022}}
{{Use British English|date=January 2022}}
{{Infobox aircraft begin
| name=ULI NG | image=File:D-MOHN - Weller ULI NG.jpg | caption= }}{{Infobox aircraft type | type=Ultralight aircraft | national origin=Germany | manufacturer=Weller Flugzeugbau | designer= | first flight= | introduced=2010 | retired= | status=In production (2012) | primary user= | more users= | produced= | number built= | developed from= Egon Scheibe Uli 1 | variants with their own articles= }} |
The Weller ULI NG (New Generation), sometimes called the Weller Uli NG, is a German ultralight aircraft, designed and produced by Weller Flugzeugbau of Bibersfeld. It was introduced at the Aero show held in Friedrichshafen in 2010. The aircraft is supplied as a complete ready-to-fly-aircraft.Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 84. WDLA UK, Lancaster UK, 2011. {{ISSN|1368-485X}}Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 88. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}
Design and development
The aircraft is derived from the Egon Scheibe Uli 1 and was re-designed to comply with the German {{convert|120|kg|lb|0|abbr=on}} class ultralight rules. It features a cable-braced high-wing, a single-seat open cockpit without a windshield, fixed conventional landing gear and a single engine in pusher configuration.{{cite web|url=http://www.weller-flugzeugbau.de/node/14/62 |title= Weller Uli NG |last=Weller Flugzeugbau |publisher=Weller-flugzeugbau.de |date= |accessdate=2012-09-13}}
The aircraft fuselage is made from welded steel tubing, the wing built from bolted-together aluminum tubing, with its flying surfaces covered in aircraft fabric. Its {{convert|9.68|m|ft|1|abbr=on}} span wing has an area of {{convert|12.78|m2|sqft|abbr=on}}, giving a very light wing loading of 17.0 kg/m2 (3.5 lb/sq ft). The standard engine available is the {{convert|30|hp|kW|0|abbr=on}} Briggs & Stratton industrial four-stroke powerplant with a V-belt reduction drive, powering a two bladed wooden propeller. The engine burns {{convert|5|L}} per hour at cruise. The aircraft's {{convert|18|L}} fuel tank is detachable for refueling and is filled with premium auto-fuel. The design incorporates a ballistic parachute whole-aircraft rescue system that includes an ignition cut-off upon firing.
Specifications (version)
{{Aircraft specs
|prime units?=met
|genhide=
|crew=one
|capacity=
|length m=5.92
|length ft=
|length in=
|length note=
|span m=9.68
|span ft=
|span in=
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=12.78
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=119.5
|empty weight lb=
|empty weight note=
|gross weight kg=220
|gross weight lb=
|gross weight note=
|fuel capacity={{convert|18|L}} removable tank
|more general=
|eng1 number=1
|eng1 name=Briggs & Stratton
|eng1 type=two cylinder, air-cooled, four stroke aircraft engine, with a V-belt reduction drive
|eng1 kw=
|eng1 hp=30
|prop blade number=2
|prop name=wooden
|prop dia m=
|prop dia ft=
|prop dia in=
|prop note=
|perfhide=
|max speed kmh=95
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=80
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=45
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|range km=150
|range miles=
|range nmi=
|range note=
|endurance=2:30 plus reserve
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=2
|climb rate ftmin=
|climb rate note=
|time to altitude=
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2=17.0
|wing loading lb/sqft=
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}
References
{{reflist}}
External links
- {{Official website|http://www.weller-flugzeugbau.de/node/14/62}}
{{Weller Flugzeugbau aircraft}}