Guimbal Cabri G2

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Cabri G2
Cabri G2 in February 2006
Cabri G2 in February 2006
Type: Light helicopter
Design country:

FranceFrance France

Manufacturer:

Hélicoptères guimbal

First flight:

March 31, 2005

Production time:

In series production since 2008

Number of pieces:

210 (as of September 2017)

The Cabri G2 is a single-engine, two-seat helicopter made by the French manufacturer Hélicoptères Guimbal with a piston engine drive .

history

The idea and the development of the helicopter was initiated as a private project by the engineer Bruno Guimbal, who was then employed by Aérospatiale , in the 1980s. From the beginning of the 1990s, the development and testing of the project was officially supported by Aérospatiale (later Eurocopter ).

Guimbal Cabri explains the name as an acronym formed from C omfort in A utorotation B elongs to R otor I nertia . The prototype of the Cabri G2 had its maiden flight in April 1992. When Eurocopter decided against the certification and serial production of the model, Guimbal reached an agreement with the group and in 2000 founded his own company, Hélicoptères Guimbal SA. From now on, Guimbal worked on the certification of the Cabri and received approval from the European approval authority EASA according to CS-27 on December 14, 2007 and approval from the FAA on February 3, 2015 . The Cabri is intended to compete with the Robinson R22 . The price quoted is EUR 275,000. The gmbh Baden-Baden motorflug , a subsidiary of Eurocopter , received her first helicopter (D-HETA), with the serial number 1007 on 24 November 2009. The machine is there the pilot training. The Cabri G2 also holds some world records in various categories in its class.

Orka-1200

Orka-1200 at the 2007 Paris Air Show

The UAV Orka-1200, which was developed by Hélicoptères Guimbal together with EADS Defense and Communications Systems , is also based on the Cabri G2 .

Helicopter trainer

The Heli Trainer at the ILA 2010

Together with the Max Planck Institute for Biological Cybernetics and a helicopter operator based in Augsburg , a flight simulator with the fuselage of the G2 was developed. The fuselage was mounted on a heavy duty robot KR 500 TÜV from the Augsburg company KUKA Roboter and is able to simulate all movements of a helicopter. The Heli Trainer was presented to the public at the International Aerospace Exhibition Berlin 2010.

technology

The conventionally constructed helicopter is made of composite materials , with the fuselage being manufactured by Composites Aquitaine ( Sogerma ). It has an empty weight of less than 500 kg and is equipped with a three-bladed main rotor with blades made of carbon fiber reinforced plastic with a lead core, flapping and swivel joints with elastomer bearings and dampers, and a seven- bladed Fenestron rear rotor. The main rotor turns clockwise when viewed from above.

The G2 is powered by a 107 kW (145 PS) Lycoming O-360 -J2A four-cylinder boxer engine . The engine is the same as that of the Robinson R22, but has an additional Plasma II + ignition system from the US company Light Speed ​​Engineering, which increases the output from 131 HP to 145 HP. This drives an intermediate shaft via a belt with a reduction ratio of i = 0.855, which in turn drives the main rotor shaft via a bevel gear with i = 0.234 (11:47). Thanks to the 170 liter tank, flights of 930 km or up to five hours are possible. Particular emphasis was placed on the helicopter's crash safety and low operating costs (for example due to the long idle times of the drive train). The cockpit is equipped with a modern multifunctional display. A noise level of 75.7 decibels is reached in the flyby .

Incidents

The machine of motorflug baden-baden gmbh (see above) crashed on April 19, 2010 during a flight at Karlsruhe / Baden-Baden airport from a height of about three meters. The pilot and the passenger of the helicopter were uninjured. In spring 2014 there were two more accidents with this helicopter type in connection with uncontrolled turning around the vertical axis.

Technical specifications

(Manufacturer information for the Cabri G2)

Parameter Data (metric) at ISA
crew 2
Hull length 6.31 m
Width over runners 1.6 m
height 2.5 m
Main rotor diameter 7.2 m
Tail rotor diameter 0.6 m
Empty mass 425 kg
Maximum take-off mass 700 kg
drive a Lycoming O-360 -J2A
fuel 170 liters, (100 octane )
Starting power 108 kW (145 hp) at 2650 min -1
HIGE 1,500 m (5,000 ft)
Service ceiling 4000 m (13,000 ft)
Cruising speed 167 km / h
Top speed 245 km / h
Range 700 km

Comparable helicopter types

literature

  • The big little one. In: aerokurier No. 5/2018, pp. 22-26

Web links

Commons : Guimbal Cabri G2  - Collection of pictures, videos and audio files

Individual evidence

  1. FlightInternational, September 25 - October 1, 1991, page 22
  2. Website for the Cabri G2 (English)
  3. "Rotor", April 2014 ( Memento from May 9, 2015 in the Internet Archive )
  4. Guimbal Cabri Gets FAA Certification
  5. FliegerRevue 4/2008, p. 8.
  6. ^ First Cabri G2 delivered to Eurocopter, FlugRevue, December 9, 2009
  7. ^ Website of the Fédération Aéronautique Internationale: Database ID 11842, 11843, 11844 of the FAI record database
  8. mpg.de: Heli Trainer sets new standards in pilot training , press release from May 18, 2010
  9. Technical description of the rotor head of the Cabri G2
  10. ka-news: Helicopter crashed at Karlsruhe-Baden Airport
  11. Federal Office for Aircraft Accident Investigation: Investigation report file number BFU 3X036-10
  12. Federal Office for Aircraft Accident Investigation: Investigation report file number BFU 3X002-14
  13. Federal Office for Aircraft Accident Investigation: Investigation report file number BFU 3X003-14