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词条 Hanriot LH.10
释义

  1. Variants

  2. Operators

  3. Specifications (LH.16)

  4. References

name=LH.10-LH.16image=Hanriot LH.10 Annuaire de L'Aéronautique 1931.jpgcaption=LH.10

}}{{Infobox Aircraft Type

type=Civil trainer aircraftnational origin=Francemanufacturer=Hanriotdesigner=1930}}introduced=retired=status=primary user=Armée de l'Airmore users=produced=number built=54variants with their own articles=
}}

The Lorraine-Hanriot LH.10 was a family of training monoplanes built in France in the early 1930s, the most widely produced and well-known member of which was the LH.16, later known simply as the Hanriot H.16. It was a conventional parasol-wing monoplane with fixed tailskid undercarriage, the main units of which were mounted on outriggers attached to the wing struts. The pilot and instructor sat in tandem open cockpits.

Early members of the family all had radial engines, but the definitive LH.16 of 1933 had an inline engine within a neat cowling. This type was evaluated by the Armée de l'Air and an initial order for 60 machines was placed. This was soon amended to just 15 in the original trainer configuration, plus another 29 modified as observation aircraft with a mounting for a trainable machine gun in the rear cockpit. Following a brief career in military service, the H.16s were turned over to the Aviation Populaire for use as trainers.

Variants

  • LH.10 - initial version with Lorraine 5Pa engine (2 built)
  • LH.11 - version with Lorraine 5Pb engine (2 built)
    • LH.11bis
  • LH.12 - version with Salmson 9Ac engine (1 built)
  • LH.13 - version with Lorraine 5Pb engine (5 built)
  • LH.16 - definitive version with Renault 4Pdi engine (15 built)
    • H.16/1 - armed observation version of H.16 (29 built)

Operators

{{FRA}}
  • French Air Force

Specifications (LH.16)

{{aerospecs
|ref=
|met or eng?=met
|crew=Two, pilot and instructor
|capacity=
|length m=8.28
|length ft=26
|length in=3
|span m=11.90
|span ft=39
|span in=1
|swept m=
|swept ft=
|swept in=
|rot number=
|rot dia m=
|rot dia ft=
|rot dia in=
|dia m=
|dia ft=
|dia in=
|width m=
|width ft=
|width in=
|height m=2.62
|height ft=8
|height in=8
|wing area sqm=22.0
|wing area sqft=237
|swept area sqm=
|swept area sqft=
|rot area sqm=
|rot area sqft=
|volume m3=
|volume ft3=
|aspect ratio=
|empty weight kg=547
|empty weight lb=1,206
|gross weight kg=886
|gross weight lb=1,953
|lift kg=
|lift lb=
|eng1 number=1
|eng1 type=Renault 4Pdi
|eng1 kw=90
|eng1 hp=120
|eng1 kn=
|eng1 lbf=
|eng1 kn-ab=
|eng1 lbf-ab=
|eng2 number=
|eng2 type=
|eng2 kw=
|eng2 hp=
|eng2 kn=
|eng2 lbf=
|eng2 kn-ab=
|eng2 lbf-ab=
|max speed kmh=155
|max speed mph=96
|max speed mach=
|cruise speed kmh=
|cruise speed mph=
|range km=375
|range miles=233
|endurance h=
|endurance min=
|ceiling m=4,200
|ceiling ft=13,800
|glide ratio=
|climb rate ms=
|climb rate ftmin=
|sink rate ms=
|sink rate ftmin=
|armament1=
|armament2=
|armament3=
|armament4=
|armament5=
|armament6=
}}{{aircontent
|see also=
|related=
|similar aircraft=
|lists=
}}

References

  • {{cite book |last= Taylor |first= Michael J. H. |title=Jane's Encyclopedia of Aviation |year=1989 |publisher=Studio Editions |location=London |pages=470 }}
  • {{cite book |title=World Aircraft Information Files |publisher=Bright Star Publishing|location=London |pages=File 896 Sheet 09 }}
{{Hanriot aircraft}}

4 : French civil trainer aircraft 1920–1929|Hanriot aircraft|Parasol-wing aircraft|Aircraft first flown in 1930

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