Verhees D-Plane 1

The D- Plane 1 is developed in Belgium by Bart Verhees Delta Wing Aircraft Class Ultralight. The machine is designed for Amateurbau.

Description

The D- Plane 1 is a cantilever mid-wing monoplane with a single-seat enclosed cockpit. The fuselage and the wing are made ​​of aluminum tubing and aluminum sheet ( Aerospace Aluminum ) made ​​. The span is 4.5 meters and has a wing area of ​​10 m². The D-1 has a retractable nose wheel and a motor with a tractor propeller.

The first flight of the prototype took place in 2004. In the first flight available to the D- 1 through a Subaru EA -71 four-cylinder four -stroke engine with 1.6 liter displacement and 50 hp ( 37 kW).

The test pilot Captain Peter Kuypers conducted with the D -1 Features: F- PDHV, on 6 May 2010, a detailed test flight through the entire flight characteristics of the aircraft were recorded.

Specifications (2010)

  • Crew: 1 pilot
  • Wingspan: 4.5 m
  • Length: 3.3 m
  • Wing area: 10 m²
  • Motor: 1 Subaru EA -71 four-cylinder, water-cooled four -stroke engine, 50 hp ( 37 kW), no electric starter
  • Propellers: two-blade, fixed
  • Empty weight: 210 kg
  • Start Weight: 340 kg max.
  • Cruising speed: 220 km / h
  • Maximum speed: 270 km / h
  • Stall speed: 85 km / h
  • Struckturbelastung: / - 6 g
  • Fuel tank capacity: 60 liters
  • Fuel: Mogas, Super plus ( ROZ98 )
  • Fuel pump 2, a mechanically and electrically switchable pump
  • Consumption: 13 L / h at cruising speed
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