Dyn'Aéro Twin-R: Difference between revisions
Content deleted Content added
Rescuing 1 sources and tagging 0 as dead.) #IABot (v2.0 |
m Apply Template:Convert and tidy as MOS:FOOT, typo(s) fixed: 2001-2 → 2001–2 |
||
| (4 intermediate revisions by 4 users not shown) | |||
| Line 1: | Line 1: | ||
{{Short description|Twin engine kit-built light aircraft}} |
|||
<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. --> |
<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. --> |
||
{|{{Infobox |
{|{{Infobox aircraft begin |
||
| name=Twin-R |
| name=Twin-R |
||
| image= |
| image= |
||
| caption= |
| caption= |
||
}}{{Infobox |
}}{{Infobox aircraft type |
||
| type=Four seat twin engine [[homebuilt aircraft|kitbuilt]] |
| type=Four seat twin engine [[homebuilt aircraft|kitbuilt]] |
||
| national origin=[[France]] |
| national origin=[[France]] |
||
| Line 26: | Line 27: | ||
==Design and development== |
==Design and development== |
||
The Dyn'Aéro Twin-R is a twin engine development of the four-seat, single-engine [[Dyn'Aéro MCR4S]], with a 580 |
The Dyn'Aéro Twin-R is a twin engine development of the four-seat, single-engine [[Dyn'Aéro MCR4S]], with a {{convert|580|mm|ftin|abbr=on}} greater span and increases in tail surface areas. It was originally intended that it should be built from drawings but changes to French multi-engine aircraft regulations led to plans for kit production.<ref name=JAWA11/><ref name="WDLA11"/><ref name="WDLA15"/> |
||
The Twin-R follows previous MCR series structural practice with much use of [[carbon fibre]], notably in the [[Spar (aviation)|spars]] and [[rib (aircraft)|ribs]] of the wings and control surfaces, which have pre-formed aluminium skins. |
The Twin-R follows previous MCR series structural practice with much use of [[carbon fibre]], notably in the [[Spar (aviation)|spars]] and [[rib (aircraft)|ribs]] of the wings and control surfaces, which have pre-formed aluminium skins. The [[fuselage]] is a carbon fibre [[monocoque]]. The wings have constant chord as on the MCR4S, though the increased span raises the aspect ratio to 10.8, and the Twin-R uses the [[winglet]]s of the early MCR4S versions (2001–2), with curved (in plan) trailing edges, rather than the later, straight edged ones. The [[aileron]] span is increased by 20% and the [[flaps (aircraft)|flaps]] are electrically operated. Like the MCR4S, the Twin-R has a swept [[fin]], [[ventral fin]] and [[T-tail]] but the fin is taller and the [[stabilator|all flying tailplane]] of greater span. The [[rudder]] area is almost doubled and the surface is double hinged to control [[yaw (rotation)|yaw]] when one engine is shut down.<ref name=JAWA11/><ref name="WDLA11"/><ref name="WDLA15"/> |
||
The cabin and rear fuselage of the Twin-R are similar to that of the MCR4S. The cabin has a large, forward hinged, one piece [[aircraft canopy|canopy]] with [[trapezoid]]al windows aft. It seats the pilot and three passengers in two side-by-side rows. |
The cabin and rear fuselage of the Twin-R are similar to that of the MCR4S. The cabin has a large, forward hinged, one piece [[aircraft canopy|canopy]] with [[trapezoid]]al windows aft. It seats the pilot and three passengers in two side-by-side rows. The twin {{convert|74|kW|hp|abbr=on}} [[Rotax 912ULS]] [[flat four engine]]s are wing mounted. The [[tricycle undercarriage]] has wing mounted, [[fairing (aircraft)|faired]] main legs and wheels.<ref name=JAWA11/><ref name="WDLA11"/><ref name="WDLA15"/> |
||
The Twin-R appeared in public for the first time at the [[AERO Friedrichshafen]] 2010 show.<ref name=JAWA11/> It flew for the first time on 3 March 2011 piloted by Christian Briand.<ref name=T-R/> |
The Twin-R appeared in public for the first time at the [[AERO Friedrichshafen]] 2010 show.<ref name=JAWA11/> It flew for the first time on 3 March 2011 piloted by Christian Briand.<ref name=T-R/> |
||
| Line 70: | Line 71: | ||
|max takeoff weight kg=950 |
|max takeoff weight kg=950 |
||
|max takeoff weight note= |
|max takeoff weight note= |
||
|fuel capacity=110 L (24.2 Imp gal, 29.1 US gal) standard. |
|fuel capacity=110 L (24.2 Imp gal, 29.1 US gal) standard. Can be increased to 200 L (44 Imp gal, 52.8 US gal) |
||
|more general= |
|more general= |
||
<!-- |
<!-- |
||
| Line 100: | Line 101: | ||
|cruise speed mph= |
|cruise speed mph= |
||
|cruise speed kts= |
|cruise speed kts= |
||
|cruise speed note=normal, at 75% power at 2,438 |
|cruise speed note=normal, at 75% power at {{convert|2,438|m|ft|abbr=on}} |
||
|stall speed kmh=92 |
|stall speed kmh=92 |
||
|stall speed note=flaps down |
|stall speed note=flaps down |
||
| Line 135: | Line 136: | ||
|sink rate note= |
|sink rate note= |
||
|lift to drag= |
|lift to drag= |
||
|wing loading kg/m2 |
|wing loading kg/m2= |
||
|wing loading lb/sqft= |
|wing loading lb/sqft= |
||
|wing loading note= |
|wing loading note= |
||
| Line 157: | Line 158: | ||
==References== |
==References== |
||
{{commons category|Dyn'Aéro}} |
|||
{{reflist|refs= |
{{reflist|refs= |
||
<ref name=JAWA11>{{cite book |title= Jane's All the World's Aircraft 2011-12|last= Jackson |first=Paul |
<ref name=JAWA11>{{cite book |title= Jane's All the World's Aircraft 2011-12|last= Jackson |first=Paul |year=2011|publisher= IHS Jane's|location=Redhill, UK|isbn=978-0-7106-2955-5|page=201}}</ref> |
||
<ref name=T-R>{{cite web|url=http://www.love4aviation.com/Aircraft/Twin-R/First+flights.html|title=Dyn'Aéro Twin-R - First flight| |
<ref name=T-R>{{cite web|url=http://www.love4aviation.com/Aircraft/Twin-R/First+flights.html|title=Dyn'Aéro Twin-R - First flight|access-date=2011-07-18|archive-url=https://web.archive.org/web/20110625051353/http://www.love4aviation.com/Aircraft/Twin-R/First+flights.html|archive-date=2011-06-25|url-status=dead}}</ref> |
||
<ref name="WDLA11">Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 100. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X</ref> |
<ref name="WDLA11">Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 100. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X</ref> |
||
Latest revision as of 14:26, 22 July 2024
| Twin-R | |
|---|---|
| Role | Four seat twin engine kitbuilt |
| National origin | France |
| Manufacturer | Dyn'Aéro |
| Designer | Pierre and Christophe Robin |
| First flight | 3 March 2011 |
| Developed from | Dyn'Aéro MCR4S |
The Dyn'Aéro Twin-R is a twin engine kit-built light aircraft based on the single-engine Dyn'Aéro MCR4S, designed and built in France. Its first flight was in March 2011.
Design and development
[edit]The Dyn'Aéro Twin-R is a twin engine development of the four-seat, single-engine Dyn'Aéro MCR4S, with a 580 mm (1 ft 11 in) greater span and increases in tail surface areas. It was originally intended that it should be built from drawings but changes to French multi-engine aircraft regulations led to plans for kit production.[1][2][3]
The Twin-R follows previous MCR series structural practice with much use of carbon fibre, notably in the spars and ribs of the wings and control surfaces, which have pre-formed aluminium skins. The fuselage is a carbon fibre monocoque. The wings have constant chord as on the MCR4S, though the increased span raises the aspect ratio to 10.8, and the Twin-R uses the winglets of the early MCR4S versions (2001–2), with curved (in plan) trailing edges, rather than the later, straight edged ones. The aileron span is increased by 20% and the flaps are electrically operated. Like the MCR4S, the Twin-R has a swept fin, ventral fin and T-tail but the fin is taller and the all flying tailplane of greater span. The rudder area is almost doubled and the surface is double hinged to control yaw when one engine is shut down.[1][2][3]
The cabin and rear fuselage of the Twin-R are similar to that of the MCR4S. The cabin has a large, forward hinged, one piece canopy with trapezoidal windows aft. It seats the pilot and three passengers in two side-by-side rows. The twin 74 kW (99 hp) Rotax 912ULS flat four engines are wing mounted. The tricycle undercarriage has wing mounted, faired main legs and wheels.[1][2][3]
The Twin-R appeared in public for the first time at the AERO Friedrichshafen 2010 show.[1] It flew for the first time on 3 March 2011 piloted by Christian Briand.[4]
Variants
[edit]- Twin-R
- Kit built.
- ELA1
- Proposed certificated aircraft.
Specifications (kitbuilt)
[edit]Data from Jane's All the World's Aircraft 2011/12[1]
General characteristics
- Capacity: 4
- Length: 7.10 m (23 ft 4 in)
- Wingspan: 9.24 m (30 ft 4 in)
- Height: 1.90 m (6 ft 3 in)
- Wing area: 8.60 m2 (92.6 sq ft)
- Empty weight: 425 kg (937 lb)
- Max takeoff weight: 950 kg (2,094 lb)
- Fuel capacity: 110 L (24.2 Imp gal, 29.1 US gal) standard. Can be increased to 200 L (44 Imp gal, 52.8 US gal)
- Powerplant: 2 × Rotax 912ULS flat four, air- and water-cooled piston, 73.5 kW (98.6 hp) each
- Propellers: 2-bladed
Performance
- Maximum speed: 335 km/h (208 mph, 181 kn)
- Cruise speed: 326 km/h (203 mph, 176 kn) normal, at 75% power at 2,438 m (7,999 ft)
- Stall speed: 92 km/h (57 mph, 50 kn) flaps down
- Range: 2,129 km (1,323 mi, 1,150 nmi) with maximum fuel
- Rate of climb: 7.6 m/s (1,500 ft/min)
Avionics
- Dynon Skyview 3-screen EFIS recommended
References
[edit]- ^ a b c d e Jackson, Paul (2011). Jane's All the World's Aircraft 2011-12. Redhill, UK: IHS Jane's. p. 201. ISBN 978-0-7106-2955-5.
- ^ a b c Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 100. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
- ^ a b c Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 97. Flying Pages Europe SARL, 2015. ISSN 1368-485X
- ^ "Dyn'Aéro Twin-R - First flight". Archived from the original on 2011-06-25. Retrieved 2011-07-18.