Berger BX-110

Berger BX-110

__NOTOC__ Infobox Aircraft
name=BX-110


caption=
type=Utility helicopter
manufacturer=Hans Berger
designer=
first flight=3 June 1974
introduced=
retired=
status=
primary user=
more users=
produced=
number built=1
variants with their own articles=
The Berger BX-110 was a prototype light helicopter built in Switzerland in the early 1970s. The single example (registration "HB-YAK") was built by Hans Berger, a Swiss inventor and helicopter dealer. It was powered by a Wankel automotive engine and remained on the Swiss civil register until 1994. It was of conventional light helicopter configuration, with pilot and passenger sitting side-by-side under a large perspex bubble canopy, with the tail rotor carried on a tubular boom. The powerplant and fuel tanks were located behind the cabin, and the three-bladed main rotor had foldable blades. Landing gear was originally of skid type.

Originally powered by a converted NSU Ro 80 Wankel-type automotive engine, Berger later fitted a BMW 6012 turbine to the aircraft, and later still another adapted automotive Wankel engine, this time from a Mazda RX-7. At the time of the latter conversion, the undercarriage was changed to tricycle configuration.

pecifications (final configuration)

aerospecs
met or eng?= met

crew=one pilot
capacity=1 passenger
length m=6.05
length ft=19
length in=10
span m=
span ft=
span in=
rot number=1
rot dia m= 7.40
rot dia ft= 24
rot dia in= 3
height m=2.57
height ft=8
height in=5
wing area sqm=
wing area sqft=
rot area sqm= 43.0
rot area sqft= 463
aspect ratio=
empty weight kg=400
empty weight lb=880
gross weight kg=720
gross weight lb=1,590

eng1 number=1
eng1 type=Mazda RX-7 automotive engine
eng1 kw= 86
eng1 hp= 115
eng1 kn=
eng1 lbf=
eng1 kn-ab=
eng1 lbf-ab=
eng2 number=
eng2 type=
eng2 kw=
eng2 hp=
eng2 kn=
eng2 lbf=
eng2 kn-ab=
eng2 lbf-ab=

max speed kmh=175
max speed mph=109
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=
range miles=
endurance h=
endurance min=
ceiling m=2,800
ceiling ft=9,184
glide ratio=
climb rate ms=4.0
climb rate ftmin=790
sink rate ms=
sink rate ftmin=

armament1=
armament2=
armament3=
armament4=
armament5=
armament6=

References

*
* "Jane's All the World's Aircraft 1973-74" p. 188
* "Cockpit" (December 1989)

ee also

aircontent

related=

similar aircraft=

sequence=
* BX-50 - BX-110 - BX-111 - BX-200 - BX-300

lists=

see also=


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