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词条 Chasle YC-100 Hirondelle
释义

  1. Design and development

  2. Variants

  3. Specifications (YC-100 prototype)

  4. References

name=YC-100 Hirondelle image= caption=

}}{{Infobox Aircraft Type

type=Single seat microlight national origin=France manufacturer= from plans designer=Yves Chasle first flight=1 May 1985 introduced= retired= status= primary user= more users= produced= number built= program cost= unit cost= developed from= variants with their own articles=
}}

The Chasle YC-100 Hirondelle ({{lang|en|Swallow}}) is a French single seat microlight designed in the 1980s.

Design and development

Yves Chasle worked as an Aérospatiale stress engineer and independently designed several light aircraft, starting with the Chasle YC-12 Tourbillon. His YC-100 Hirondelle is a largely wooden framed and fabric covered single-seat sports aircraft of conventional pusher layout. It has a strut braced high wing of constant chord with styrofoam ribs. The fuselage of the Hirondelle is a slender, rectangular cross-sectioned beam with the pilot's seat upon it ahead of the wing leading edge. Behind the pilot a central structure supports the wing just above head level; on its trailing edge, one of several types of small piston engine, with power outputs typically around {{convert|20|kW|hp|abbr=on|0}}, drives a pusher propeller. The fin is broad and straight-tapered and the horizontal tail is attached to the fuselage underside. The Hirondelle has a short, fixed tricycle undercarriage.

Its first flight was on 1 May 1985, powered by a {{convert|18|kW|hp|abbr=on|0}} König SC 430 engine, a 430 cc (26.2 cu in), air-cooled, three-cylinder radial. The second prototype, built in Brazil, had a {{convert|22|hp|kW|abbr=on|order=flip|0}} JPX PUL 425/503 engine, a 212 cc (12.9 cu in) air-cooled flat-twin two stroke.[3]

The number built is uncertain; in 2009 two examples, both YC-100s, appeared on European civil registers, one in Spain and one in France.[4]

Variants

Plans for these were available but only the YC-100 is known to have been built.

YC-100
As described below but could also be fitted with a {{convert|22|hp|kW|abbr=on|order=flip|0}} JPX PUL 425/503.
YC-101
As YC-100 but span increased to {{convert|9.35|m|ftin|abbr=on|0}}. Recommended engines were the JPX PUL 865, the {{convert|28|hp|kW|abbr=on|order=flip|0}} König SD 570 or the {{convert|30|hp|kW|abbr=on|order=flip|0}} KFM 107ER.
YC-110
Shorter span ({{convert|8.25|m|ftin|abbr=on|0}} wings with NACA 23015 section and Junkers type, two part, full span auxiliary airfoil ailerons or flaperons. Recommended engines as YC-100 and also the König SD 570.
YC-111
Longer span ({{convert|9.35|m|ftin|abbr=on|0}}) YC-110. Recommended engines were the König SD 570, KFM 107ER, JPX PUL 865 and also the Rotax 377 or 447, respectively {{convert|26|kW|hp|abbr=on|0}} and {{convert|29.4|kW|hp|abbr=on|1}}.

Specifications (YC-100 prototype)

{{Aircraft specs
|ref=Jane's All the World's Aircraft 1988/89
|prime units?=met


|crew=one
|length m=5.43
|length note=
|span m=8.30
|span note=
|height m=1.71
|height note=
|wing area sqm=11.25
|wing area note=
|aspect ratio=
|airfoil=3.20.16Y (an Aérospatiale V.16F variant)
|empty weight kg=110
|empty weight note=
|gross weight kg=
|gross weight lb=
|gross weight note=
|max takeoff weight kg=210
|max takeoff weight note=
|fuel capacity=24 l (6.3 US gal; 5.3 Imp gal)
|more general=


|eng1 number=1
|eng1 name=König SC 430
|eng1 type=air-cooled three cylinder 430 cc (26.24 cu in) radial engine[3]
|eng1 kw=18
|eng1 note=
|more power=
|prop blade number=
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=


|perfhide=
|max speed kmh=130
|max speed note=
|cruise speed kmh=100
|cruise speed note=
|stall speed kmh=45
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|minimum control speed kmh=
|minimum control speed mph=
|minimum control speed kts=
|minimum control 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=
|climb rate ftmin=
|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=
|wing loading note=
|power/mass=
|more performance=

  • Take-off run, grass: less than {{convert|100|m|ft|abbr=on|-1}}
  • Landing run, grass: about {{convert|27|m|ft|abbr=on|-1}}

}}{{aircontent
|see also=
|related=
|similar aircraft=
|lists=
}}

References

1. ^{{cite book |title= Jane's All the World's Aircraft 1988-1989|last= Taylor|pages=684, 689}}
2. ^{{cite book |title=European registers handbook 2010 |last= Partington |first=Dave |edition= |year=2010|publisher= Air Britain (Historians) Ltd|location= |isbn=978-0-85130-425-0|pages=691, 1171}}
[1][2]
}}{{Chasle aircraft}}

6 : Ultralight aircraft|French sport aircraft 1980–1989|Chasle aircraft|High-wing aircraft|Single-engined pusher aircraft|Aircraft first flown in 1985

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