Opener BlackFly / BlackFly International BlackFly

The Opener BlackFly is an American electric-powered VTOL personal air vehicle designed by Canadian Marcus Leng and under development by his company, Opener, Inc of Palo Alto, California. It was publicly introduced on 12 July 2018, after nine years of development.

The first proof-of-concept version was flown on 5 October 2011, in Warkworth, Ontario, Canada, by Leng. He flew the next model, named the BlackFly, in August 2014 and then relocated the company to Palo Alto, California in September 2014. In February 2016, the second BlackFly prototype was first flown. By September 2017, the prototype had flown 10,000 mi (16,093 km) in a series of flights of at least 30 mi (48 km) each. The first pre-production aircraft was flown in October 2017.

The design is intended for the FAR 103 Ultralight Vehicles category in the US and the Basic Ultralight Aeroplane category in Canada. The US version and international versions were to have different ranges, speeds and weights to comply with national regulations. The aircraft is intended to be supplied complete and ready-to-fly.

The aircraft is made from carbon-fiber reinforced epoxy with all-electric battery-powered propulsion. It has two 13.6 ft (4.15 m) cantilevered tandem wings, on the front and rear of a short fuselage. The fuselage has a single-seat cockpit under a bubble canopy. The forward wing is low, and the rear wing high, giving the cockpit good forward visibility. Each wing has four tractor configuration contrarotating propellers powered by electric motors. The tractor configuration prevents the flexible propellers from contacting the airframe. Each wingtip has winglets to improve lateral stability and reduce vortex drag. The aircraft weighs 313 lb (142 kg) empty and can carry a pilot and baggage totaling 250 lb (113 kg). It can accommodate a pilot of up to 6.5 ft (1.98 m) in height. A ballistic parachute is optional.

The aircraft is not a tiltwing, tiltrotor or ducted-fan design. Instead, the entire aircraft changes pitch. When the aircraft is parked, both wings and their motors are canted up at about 45 degrees. To ascend vertically, the aircraft pitches up 45 degrees, so that the propellers pull vertically. The wing-mounted tractor propellers move air over the wings, reducing stall speeds. So, at pitch angles near zero degrees, the aircraft can fly slowly with high angles of attack. For efficient horizontal flight, the aircraft pitches down 45 degrees, canting the wings and propellors to an optimal angle of attack. The forward wing has a slightly lower angle of attack to aid stall recovery. At low speeds the forward wing will stall first, causing the nose to fall, increasing air speed and exiting a stall.

The take-off and landing distances are 36 inches. The landing gear consists of a rub-strip on the bottom of an amphibious hull and a small rubber bumper on the rear of the fuselage. The lower edge of the winglets are skids that limit the vehicle’s roll when parked. The vehicle is designed to fly from a grass surface, but can also be flown from fresh water, asphalt, snow and ice.

Pilot controls are a joystick with a thumb control for altitude. Flight controls are triple-redundant fly-by-wire controlling the motors and dual elevons on the outer edge of both wings. Differential motor speeds provide control authority in pitch, roll and yaw. Elevons also permit control in an efficient unpowered glide mode. The elevons are in the prop-wash of the outer propellers, enhancing their roll and pitch authority at low speeds. Flight stability is software-controlled, with modes for cruise-control, “return-home,” auto-land and geo-fencing.

Most flight testing was unmanned, operated by software with a test weight in place of a pilot. Each motor weighs 4 lb (2 kg) and produces 130 lb (59 kg) of thrust. There are two batteries per motor, located in the wing, behind each motor. Adjacent batteries can be cross-connected for redundancy. The batteries are software-monitored. Avionic include Full authority autopilot, Remote controls, and VHF airband radio.

The manufacturer claims that the design is the world’s first ultralight fixed-wing, all-electric, vertical take-off and landing aircraft. Investors in the company include Google co-founder Larry Page.

The craft was still under development in 2018.

Opener has donated a first-generation BlackFly personal ultralight aircraft to the EAA Aviation Museum in Oshkosh, Wisconsin. According to Opener, BlackFly vehicles have flown over 2,300 flights, including 900 made on preproduction models since the aircraft appeared at Oshkosh in 2018.

Opener was displaying the production version of BlackFly at the AirVenture Innovation Showcase from July 22 to July 28, 2019.

Powerplant: 8 × 112 lb thrust/engine electric motors, 42.0 hp (31.3 kW) each
Propellers: 2-bladed, 3 ft (0.91 m) diameter
Wingspan: 13 ft 7 in (4.14 m)
Length: 13 ft 5 in (4.09 m)
Height: 5 ft (1.5 m)
Empty weight: 313 lb (142 kg)
Gross weight: 563 lb (255 kg)
Fuel capacity: 12KWh
Cruise speed: 80 mph (130 km/h, 70 kn)
Range: 40 mi (64 km, 35 nmi) plus reserves
Rate of climb: 1,000 ft/min (5.1 m/s)
Rate of sink: 1,000 ft/min (5.1 m/s)
Crew: one

MSW Aviation Votec Evolaris

The steel tube hull with carbon fiber covering is for the first time a divisible, also made of carbon fiber, wing. The plug-in wing halves allow for rapid assembly and dismantling, as well as the simple transport of the aircraft in a specially designed transport trailer.

At the AERO 2017 MSW presented the project Evolaris, an electric aerobatic plane with an empty weight of 500kg and 221Kw electric motor power.

Engine: Evo220, 221 kW / 300 hp
Wing span: 6.27m
Length: 6.0m
Wing area: 7.58 sq.m
Empty weight: 500kg
MTOW: 650kg
Roll rate: 460 ° / sec
Load: +/- 10g
Stall speed: 65mph
Never exceed speed: 270mph
Endurance: 20min + 5min reserve

Militky Brditschka MB-E1

Heinz W. Brditschka also converted an HB-3 airframe in 1973 to have electric power, in which form it was known as the Militky MB-E1; Fred Militky, who designed the installation of the 13hp Bosch electric motor that replaced the piston engine, was an engineer with the Graupner model-building company, and used his experience with electrically powered radio-controlled models to produce this first electric motor glider. This made what is claimed to be the first ever manned electric-powered flight on 21 October 1973.

The silent Militky Brditschka MB El made its 9 minute maiden flight on October 21 1973. Power was provided by a standard Bosch 10kw electric motor and Varta batteries, giving 13 hp.

Meteor F.L.53 / F.L.54

F.L.53 Continental A-65

The Meteor F.L.53 is an improved version of the Lombardi F.L.3 built by Meteor S.p.A. of Trieste under licence. The F.L.53 differs by having an all-round vision cockpit canopy and a cut-down rear fuselage.

Engines can include the 75 hp Praga D, the 65 hp Continental A-65, or the 60 hp CAN D-4. The F.L.53 is of mixed construction and the undercarriage is identical to that of the standard Piper Cub.

The F.L.54 is a three-seat model which can be powered by an 85 hp Continental C-85 or 90 hp Continental C-90.

F.L.53
Engine: 65 hp Continental A-65
Wingspan: 33 ft 9 in
Wing area: 152.85 sq.ft
Length: 21 ft 7.75 in
Empty weight: 772 lb
Normal loaded: 1157 lb
MTOW: 1378 lb
Max speed: 112 mph
Cruise: 97 mph
Cruise altitude: 13,120 – 18,700 ft
Seats: 2

F.L.53 CNA D-4

Mauro Solar Riser

First flown in April 1979 the converted Easy Riser hang-glider is powered by 500 solar cells mounted on the top wing. The 40V, 10A output powers a 3 hp electric motor driving a 41 inch propeller. 1½ hrs of sunshine accumulated in the battery provides around 5 minutes of still air flight. The biplane was mylar covered.

Engine: Electric, 3 hp
Wing span: 30 ft
Empty wt: 125 lb

Lilium Jet

On 4 May 2019, Lilium flew its first flight of an untethered and unmanned five seat Lilium Jet at the Special Airport Oberpfaffenhofen in Munich, Germany. The full-scale prototype was powered by 36 electric ducted fans in configuration inspired by the Eagle prototype aircraft. After the first flight, which consisted primarily of hover, the Lilium Jet has expanded its flight envelope to include conversion to forward flight using the wing for lift, and several safety tests.

LIFT Aircraft Hexa

A multicopter being developed by Texas company LIFT Aircraft circa 2020, the company advertises it as an ultralight, but legal ultralights must weigh less than 254 pounds – Hexa tips the scales at 432 pounds.

The craft looks marginally smooth in flight, and the pilot demonstrates only vertical flight, very slow forward flight and a little hovering.

It’s called Hexa, though Hexa has 18 rotors, which are, the company says, all individually controlled by a computer utilizing triple-redundant autopilots. There’s also a whole-airplane recovery parachute system (WARPS), airbags. and it’s said to be amphibious.

The United States Air Force witnessed a flight test of a new. The craft was flown by the company’s CEO and chief pilot for the Air Force at Camp Mabry. The USAF Chief of Staff even sat in it. USAF Secretary Barbara Barrett was there for the demonstration.

U.S. Air Force Secretary Barbara Barrett with LIFT CEO Matt Chasen

Lange EA 42

First run in 1995, the Lange EA 42 is an electrical aero engine designed for self launching gliders. It is produced in Germany by Lange Aviation for their Antares 20E glider.
Contents

The EA 42 combines an EM 42 brushless 42 kW electric external rotor motor with a related engine control system and power electronics. The motor drives a two-bladed composite fixed pitch propeller with a diameter of 2 m (7 ft). It is powered by a battery pack.

Applications:
Lange Antares 20E
Lange Antares 23E
Schempp-Hirth Arcus E

Specifications:
Power 38.5 kW

EM42 electrical engine
Diameter 25 cm (10 in)
Length 27.2 cm (11 in)
Mass 29.12 kg (64 lb)

LE 42 power electronics
Length 42.2 cm (17 in)
Width 16.9 cm (7 in)
Height 20.8 cm (8 in)
Mass 9.58 kg (21 lb)