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词条 Brantly B-1
释义

  1. Design and development

  2. Specifications

  3. References

  4. External links

name = Brantly B-1image =caption =

}}{{Infobox Aircraft Type

type = light coaxial-rotor helicoptermanufacturer = Brantly Helicopter Corporationdesigner = Newby O. Brantlyfirst flight = 1946introduced =retired =status = abandonedprimary user =more users =produced =number built =unit cost =developed from =variants with their own articles =
}}

The Brantly B-1 was a 2-seat, coaxial-rotor helicopter designed by Newby O. Brantly and constructed by the Pennsylvania Elastic Company, Brantly's employer.

Design and development

In 1946, Brantly started flight testing the B-1 prototype (NX69125), which used a 150 hp Franklin O-335 engine in the fabric fuselage and two three-bladed rotors that rotated at 320 rpm and were fitted coaxially. The collective, cyclic, and differential controls were enclosed in the rotor hubs and ran in an oil-bath. Each rotor blade weighed 5.5 kilos. It also had a fixed wheel undercarriage with a tailwheel under the tailfin.[1]

Unfortunately, the design was too heavy and complex and was abandoned.

Specifications

{{Aircraft specs
|ref=[2]
|prime units?=imp


|genhide=
|crew=1
|capacity=1
|length m=5.33
|length ft=
|length in=
|dia m=
|dia ft=
|dia in=
|width m=
|width ft=
|width in=
|height m=2.36
|height ft=
|height in=
|empty weight kg=601
|empty weight lb=
|gross weight kg=907
|gross weight lb=
|max takeoff weight kg=
|max takeoff weight lb=
|more general=


|eng1 number=1
|eng1 name=Franklin O-335
|eng1 type=6-cyl. air-cooled horizontally=opposed piston engine
|eng1 kw=
|eng1 hp=150
|eng1 shp=
|eng1 kn=
|eng1 lbf=
|power original=
|thrust original=
|eng1 kn-ab=
|eng1 lbf-ab=
|more power=
|rot number=
|rot dia m=9
|rot dia ft=
|rot dia in=
|rot area sqm=
|rot area sqft=


|perfhide=
|max speed kmh=
|max speed mph=
|max speed kts=
|cruise speed kmh=182
|cruise speed mph=
|cruise speed kts=
|range km=640
|range miles=
|range nmi=
|endurance=
|ceiling m=
|ceiling ft=
|g limits=
|roll rate=
|climb rate ms=
|climb rate ftmin=
|lift to drag=
|disk loading kg/m2
|disk loading lb/sqft=
|more performance=
|avionics=
}}

References

1. ^{{cite book|last1=Simpson|first1=R.W.|title=Airlife's Helicopters and Rotorcraft|date=26 May 1998|publisher=The Crowood Press Ltd|isbn=978-1853109683}}
2. ^{{cite book|last1=Lambermont|first1=Paul Marcel|first2=Anthony|last2=Pirie|title=Helicopters and autogyros of the world|date=1970|publisher=Barnes|edition=Illustrated, revised}}

External links

{{commons category|Brantly International}}
  • Brantly Historical Photos
{{Brantly aircraft}}{{aero-1940s-stub}}

5 : United States civil utility aircraft 1940–1949|United States helicopters 1940–1949|Coaxial rotor helicopters|Brantly aircraft|Aircraft first flown in 1946

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