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词条 Caproni Ca.127
释义

  1. Design

  2. Specifications

  3. References

{{Underlinked|date=April 2019}}{{short description|1930s Italian aircraft}}
name=Ca.127image=caption=

}}{{Infobox aircraft type

type=Reconnaissancemanufacturer=Capronidesigner=first flight=1935introduced=retired=status=prototype onlyprimary user=more users=produced=number built=1variants with their own articles=
}}

The Caproni Ca.127 was a single-engine reconnaissance monoplane built by Caproni in the mid-1930s.

Design

The Ca.127 was a single engine for distant reconnaissance; it was built with a metal structure and a fuselage, with a rectangular section, built in welded steel tubes covered in canvas. The empennages are single-celled, made of steel tube covered with painted canvas. The drift and fixed altitude plan were adjustable in flight. The partially cantilever wings rested each to a metal strut that anchored to a knot in the fuselage; they were built in a light-alloy metal structure of the monospar type covered in cloth.[1]

The landing gear was of the double axle type; the shock absorber was connected to the side member of the wing at the stiffening strut of the same. The wheels were equipped with aerodynamic fairings and used medium pressure tires with expanding brakes. The tail pad was sprung, with a swiveling wheel.[1]

The cabin was dual-controlled, with side-by-side seats, and the glazed hood was connected to the rear with the median section of the wing. In the cockpit there was a telegraphic transceiver, a camera, and a front-firing machine gun.[1]

Based on results of flight tests, the Ca.127 was judged unfit to perform its intended role and did not enter production.

Specifications

{{Aircraft specs
|ref=,[2] Aeroplani Caproni dal 1908 al 1935[1]
|prime units?=met


|genhide=
|crew=
|capacity={{cvt|1000|kg}} payload
|length m=12.82
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|span m=16.9
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|wing area sqm=40
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|aspect ratio=
|airfoil=
|empty weight kg=2200
|empty weight lb=
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|gross weight kg=3200
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|fuel capacity=
|lift kg=
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|more general=


|eng1 number=1
|eng1 name=Isotta Fraschini XII R.
|eng1 type=V-12 water-cooled piston engine
|eng1 kw=
|eng1 hp=750
|eng1 shp=
|eng1 kn=
|eng1 lbf=
|eng1 note={{clarify|should this be ASSO XI R.?|date=February 2019}}
|power original=
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|eng3 number=
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|eng3 shp=
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|eng3 lbf=
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|eng3 kn-ab=
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|more power=
|prop blade number=2
|prop name=fixed pitch wooden propeller or 3-bladedground-adjustable metal propeller
|prop dia m=
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|prop dia note=
|rot number=
|rot dia m=
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|rot dia in=
|rot area sqm=
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|rot area note=


|perfhide=
|max speed kmh=305
|max speed mph=
|max speed kts=
|max speed note=
|max speed mach=
|cruise speed kmh=
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=
|stall speed kts=
|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=1000
|range miles=
|range nmi=
|range note=
|combat range km=
|combat range miles=
|combat range nmi=
|combat range note=
|ferry range km=
|ferry range miles=
|ferry range nmi=
|ferry 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={{cvt|8000|m}} in 46 minutes 25 seconds
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=
|wing loading note=
|disk loading kg/m2=
|disk loading lb/sqft=
|disk loading note=
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass=
|thrust/weight=
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|guns= 5 × {{cvt|7.7|mm|3}} machine guns
|bombs=
}}

References

1. ^{{cite book |last1=Caproni |first1=Gianni |title=Aeroplani Caproni dal 1908 al 1935 |publisher=Edizioni d'arte Emilio Bestetti |location=Milan |date=1937 |pages=337–339 |language=Italian}}
2. ^{{cite web|url=http://www.airwar.ru/enc/other1/ca127.html|title=Caproni Ca.127|website=www.airwar.ru}}
{{Caproni aircraft}}

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