请输入您要查询的百科知识:

 

词条 North American Rotorwerks Pitbull Ultralight
释义

  1. Design and development

  2. Operational history

  3. Variants

  4. Specifications (Pitbull Ultralight)

  5. References

  6. External links

name=Pitbull Ultralight image= caption=

}}{{Infobox Aircraft Type

type=Autogyro national origin=United States manufacturer=North American Rotorwerks designer= first flight= introduced= retired= status=Production suspended (2013) primary user= more users= produced= number built= program cost= unit cost= US$12,500 (ultralight kit, 2011) developed from= variants with their own articles=North American Rotorwerks Pitbull II
}}

The North American Rotorwerks Pitbull Ultralight is an American autogyro, designed and produced by North American Rotorwerks of Tukwila, Washington. When it was available the aircraft was supplied as a kit for amateur construction, but by 2013 production had been suspended.[1][2][3]

Design and development

The Pitbull Ultralight was designed to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of {{convert|254|lb|kg|0|abbr=on}}, although the aircraft has a standard empty weight of {{convert|260|lb|kg|0|abbr=on}}. It features a single main rotor, a single-seat open cockpit with a windshield, conventional landing gear and a twin cylinder, air-cooled, two-stroke, single-ignition {{convert|40|hp|kW|0|abbr=on}} Rotax 447 engine in tractor configuration. The dual ignition {{convert|50|hp|kW|0|abbr=on}} Rotax 503 and the Subaru EA81 automotive conversion are both optional.[1][3]

The aircraft fuselage is made from bolted-together square aluminum tubing, with the engine mount made from 6061-T6 aluminium. The down-struts are made from 4130 steel tubing. Its {{convert|23.6|ft|m|1|abbr=on}} diameter Fleck rotor has a chord of {{convert|7|in|cm|1|abbr=on}} and is made from extruded aluminum. The landing gear is made from 4130 steel tubing and the tailplane is strut-braced. An electric pre-rotator is standard, while a bubble canopy for year-round flying is optional. With its empty weight of {{convert|260|lb|kg|0|abbr=on}} and a gross weight of {{convert|500|lb|kg|0|abbr=on}}, the useful load is {{convert|240|lb|kg|0|abbr=on}}.[1][3]

The aircraft is intended to resemble the autogyros of the 1930s and as such it uses a radial engine-style round cowling, rounded rudder, barrel-shaped fuselage and other antique styling details.[1][2]

Operational history

By January 2013 five examples had been registered in the United States with the Federal Aviation Administration.[4]

Variants

Pitbull Ultralight

Base model with {{convert|40|hp|kW|0|abbr=on}} Rotax 447 or the {{convert|50|hp|kW|0|abbr=on}} Rotax 503 engine. Installed power can be from {{convert|38|to|52|hp|kW|0|abbr=on}}. Estimated construction time from the factory-supplied assembly kit is 50 hours.[1][2]

Pitbull SS

Higher powered model for the Experimental - amateur-built category, with {{convert|64|hp|kW|0|abbr=on}} Rotax 582 or an {{convert|85|hp|kW|0|abbr=on}} Subaru engine. Installed power can be from {{convert|50|to|85|hp|kW|0|abbr=on}}. Empty weight of {{convert|290|lb|kg|0|abbr=on}} and a gross weight of {{convert|610|lb|kg|0|abbr=on}}, the useful load is {{convert|320|lb|kg|0|abbr=on}}. Estimated construction time from the factory-supplied assembly kit is 80 hours.[1][2]

Specifications (Pitbull Ultralight)

{{Aircraft specs
|ref=Bayerl and North American Rotorwerks[1][2]
|prime units?=imp


|genhide=
|crew=one
|capacity=
|length m=
|length ft=13
|length in=5
|length note=
|width m=
|width ft=5
|width in=10
|width note=
|height m=
|height ft=8
|height in=0
|height note=
|airfoil=
|empty weight kg=
|empty weight lb=260
|empty weight note=
|gross weight kg=
|gross weight lb=500
|gross weight note=
|fuel capacity={{convert|6|u.s.gal}}
|more general=


|eng1 number=1
|eng1 name=Rotax 447
|eng1 type=twin cylinder, air-cooled, two stroke aircraft engine
|eng1 kw=
|eng1 hp=40
|prop blade number=2
|prop name=wooden
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=
|rot number=1
|rot dia m=
|rot dia ft=23
|rot dia in=6
|rot area sqm=
|rot area sqft=
|rot area note=


|perfhide=
|max speed kmh=
|max speed mph=80
|max speed kts=
|max speed note=
|cruise speed kmh=
|cruise speed mph=65
|cruise speed kts=
|cruise speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|range km=
|range miles=
|range nmi=
|range note=
|endurance=
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=4.5
|climb rate ftmin=
|climb rate note=
|time to altitude=
|disk loading kg/m2=
|disk loading lb/sqft=
|disk loading note=
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}

References

1. ^Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 184. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
2. ^{{cite web|url = http://www.pitbullrotorcraft.com/|title = North American Rotorwerks presents the Pitbull|accessdate = 12 January 2013|last = North American Rotorwerks|date = n.d.}}
3. ^Purdy, Don: AeroCrafter - Homebuilt Aircraft Sourcebook, Fifth Edition, page 327. BAI Communications, 15 July 1998. {{ISBN|0-9636409-4-1}}
4. ^{{cite web|url = http://registry.faa.gov/aircraftinquiry/AcftRef_Results.aspx?Mfrtxt=&Modeltxt=PITBULL&PageNo=1|title = Make / Model Inquiry Results|accessdate = 12 January 2013|last = Federal Aviation Administration|date = 12 January 2013}}

External links

  • {{Official website|http://www.pitbullrotorcraft.com/}}
{{North American Rotorwerks aircraft}}

3 : United States sport aircraft 2000–2009|Homebuilt aircraft|Single-engined tractor autogyro

随便看

 

开放百科全书收录14589846条英语、德语、日语等多语种百科知识,基本涵盖了大多数领域的百科知识,是一部内容自由、开放的电子版国际百科全书。

 

Copyright © 2023 OENC.NET All Rights Reserved
京ICP备2021023879号 更新时间:2024/9/21 13:36:03