“Hinz BLT-ARA”的意思、由来-开放百科全书

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Hinz BLT-ARA

释义

Design and development
Operational history
Specifications (BLT-ARA)
References

name= BLT-ARA

image=

caption=

}}{{Infobox Aircraft Type

type=Homebuilt aircraft

national origin=Germany

manufacturer=L and B Hinz

designer=

first flight=

introduced=

retired=

status= Production completed

primary user=

more users=

produced=

number built=

program cost=

unit cost= US$1,000 (plans and construction manual only, 1998)

developed from= Hinz BL1-KEA

variants with their own articles=
}}

The Hinz BLT-ARA is a German homebuilt aircraft that was designed and produced by L and B Hinz of Filderstadt. When it was available the aircraft was supplied as in the form of plans and a 300-page builder's manual for amateur construction.^[1]

Design and development

The BLT-ARA is a development of the earlier Hinz BL1-KEA which was first flown in 1989.^[1]

The BLT-ARA features a cantilever low-wing, a two-seats-in-side-by-side configuration enclosed cockpit under a bubble canopy, T-tail, retractable conventional landing gear and a single engine in tractor configuration.^[1]

The aircraft is made from fibreglass, using a moldless construction technique. Its {{convert|10.1|m|ft|1|abbr=on}} span wing has a wing area of {{convert|12.0|m2|sqft|abbr=on}}. The wings and tailplane are detachable, similar to a glider's to allow ground transport or storage in a trailer. The cabin width is {{convert|101|cm|in|abbr=on}}. The acceptable power range is {{convert|90|to|110|hp|kW|0|abbr=on}} and the standard engine used is the {{convert|95|hp|kW|0|abbr=on}} Limbach L2400 powerplant.^[1]

The BLT-ARA has a typical empty weight of {{convert|454|kg|lb|abbr=on}} and a gross weight of {{convert|726|kg|lb|abbr=on}}, giving a useful load of {{convert|272|kg|lb|abbr=on}}. With full fuel of {{convert|100|l}} the payload for the pilot, passenger and baggage is {{convert|201|kg|lb|abbr=on}}.^[1]

The manufacturer estimated the construction time from the supplied plans as 3000 hours.^[1]

Operational history

By 1998 the company reported that 13 sets of plans had been sold.^[1]

Specifications (BLT-ARA)

{{Aircraft specs
|ref=AeroCrafter^[1]
|prime units?=met

|genhide=
|crew=one
|capacity=one passenger
|length m=
|length ft=22
|length in=0
|length note=
|span m=
|span ft=33
|span in=0
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=
|wing area sqft=129
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=
|empty weight lb=1000
|empty weight note=
|gross weight kg=
|gross weight lb=1600
|gross weight note=
|fuel capacity={{convert|100|l}}
|more general=

|perfhide=
|max speed kmh=
|max speed mph=168
|max speed kts=
|max speed note=
|cruise speed kmh=
|cruise speed mph=158
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=53
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|range km=
|range miles=1000
|range nmi=
|range note=
|endurance=
|ceiling m=
|ceiling ft=18000
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=800
|climb rate note=
|time to altitude=
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=12.4
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}

References

1. ^¹²³⁴⁵⁶⁷Purdy, Don: AeroCrafter - Homebuilt Aircraft Sourcebook, Fifth Edition, page 175. BAI Communications, 15 July 1998. {{ISBN|0-9636409-4-1}}

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