Borgward hummingbird

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Borgward hummingbird
Large model (s) of the Borgward-Focke BFK-1 Kolibri in the scale 1: 4.6 in the helicopter museum in Bückeburg
Large model (s) of the Borgward-Focke BFK-1 Kolibri in the scale 1: 4.6 in the helicopter museum in Bückeburg
Type: Multipurpose helicopter
Design country:

Federal Republic of Germany

Manufacturer:

Borgward

First flight:

July 8, 1958

Number of pieces:

2 prototypes

The Borgward-Focke BFK-1 "Kolibri" was a three-seat multi-purpose helicopter made by Carl FW Borgward GmbH Automobil- und Motoren-Werke in Bremen-Sebaldsbrück.

history

The Kolibri was designed by Professor Henrich Focke and was the first type of helicopter developed independently in Germany after the Second World War . The first flight of the prototype known as Kolibri I took place on July 8, 1958. A second airworthy copy was built, which already had the full fairing of the fuselage intended for series production. However, it cannot be proven whether this machine actually flown. Only two prototypes were built and development was abandoned after Borgward went bankrupt in 1961.

construction

The structural design of the Kolibri with a tubular steel lattice hull was conventional. The fuselage of the prototype was not disguised, but this should be changed in the series version. The tail boom carried a V-tail unit at the end, at the two tips of which a propeller should produce the torque compensation. The main rotor had three blades with a steel tube as a core, which was clad with plywood for shaping.

The drive consisted of an air-cooled 6-cylinder boxer engine Lycoming VO-435-A1B with an output of 191 kW (260 hp). The fuel tank with a capacity of 180 l was located behind a firewall.

Instead of two passengers, it should alternatively be possible to transport a stretcher outside and inside. It was also planned to use the machine for spraying in agriculture. The external load capacity was 300 kg.

Technical specifications

Parameter Data
crew 1
Passengers 2
Hull length 8.30 m
Main rotor diameter 9.40 m
Tail rotor diameter 1.66 m
height 3.05 m
Empty mass 800 kg
Max. Takeoff mass 1200 kg
Cruising speed 140 km / h
Top speed 160 km / h
Service ceiling 4500 m
Max. Floating height 600 m
Engine an air-cooled six - cylinder boxer
Lycoming VO-435-A1B ; 191 kW (260 hp)

Whereabouts

The two helicopters were used by the Bremen airport fire brigade for training purposes and were largely destroyed in the process. Parts of the two machines are exhibited in the helicopter museum in Bückeburg .

See also

literature

  • Harald Focke: Borgwards helicopter . Carl B. - Car history (s), Volume 4. Verlag Peter Kurz, Bremen 2014, ISBN 978-3-927485-84-6 .
  • William Green: The Observer's World Aircraft Directory , 1961, 142
  • Henrich Focke: My way of life , 1977

Web links

Individual evidence

  1. Photo of the second prototype
  2. Use for fire brigade exercises (PDF; 3.4 MB)