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词条 Hanriot H.41
释义

  1. Variants

  2. Operators

  3. Specifications (variant)

  4. References

  5. Further reading

name=H.41frameless|centercaption=

}}{{Infobox Aircraft Type

type=Trainernational origin=Francemanufacturer=Hanriotdesigner=1925}}introduced=retired=status=primary user=more users=produced=number built=variants with their own articles=
}}

The Hanriot H.41 was a military trainer aircraft produced in France in the 1920s. It was a further development in the family of aircraft that had commenced with the HD.14 in 1920, and incorporated a number of design features that had been developed for other members of that family. Like those other aircraft, however, it was a conventional, two-bay biplane with unstaggered wings of equal span.

The H.41 used the modern engine and mixed construction developed for the HD.40 air ambulance and used them in a new design for a military trainer. The design did not prove a success, however, and only eleven were built, with three different engine types. A floatplane variant based on the HD.17 was slightly more successful, with twelve examples exported to Greece and Portugal.

Variants

H.41
Two-seat training aircraft.
H.410
version with Lorraine 5Pa engine (5 built)
H.411
version with Salmson 7Ac engine (2 built)
LH.412
version with Lorraine 5Pb engine (4 built, plus 3 converted from H.410)
HD.41H
:(Hydro) - floatplane with Salmson 9Ac engine (12 built)+ (10 built in Yugoslav Aircraft factory "Zmaj" Zemun)

Operators

{{GRE}}
  • Hellenic Air Force
  • Hellenic Navy
{{POR}}
  • Portuguese Navy
{{flagcountry|Kingdom of Yugoslavia}}
  • Yugoslav Royal Navy

Specifications (variant)

{{Aircraft specs
|ref=Jane's all the World's Aircraft 1928[1]
|prime units?=met


|crew=2
|length m=7.25
|span m=10.26
|height m=3.13
|wing area sqm=34.9
|aspect ratio=
|airfoil=
|empty weight kg=625
|gross weight kg=900
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|more general=


|eng1 number=1
|eng1 name=Lorraine 5P
|eng1 type=5-cylinder air-cooled radial piston engine
|eng1 hp=100
|prop blade number=2
|prop name=fixed pitch propeller
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=


|perfhide=
|max speed kmh=185
|max speed note=

  • Landing speed: {{cvt|50|km/h|mph kn}}

|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=
|range km=400
|ferry range km=
|ferry range miles=
|ferry range nmi=
|ferry range note=
|endurance=
|ceiling m=3500
|g limits=
|roll rate=
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude={{cvt|1000|m}} in 13 minutes
|wing loading kg/m2=25.8
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass={{cvt|0.0505|hp/lb|kW/kg|order=flip}}
|thrust/weight=
|more performance=
}}

References

{{Commons category|Hanriot HD.41}}
1. ^{{cite book |title=Jane's all the World's Aircraft 1928 |editor1-last=Grey |editor1-first=C.G. |year=1928 |publisher=Sampson Low, Marston & company, ltd |location=London |page=104c}}

Further reading

  • {{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 11 }}
  • {{cite book |title= Short History of Aviation in Serbia|last= Janić |first= Čedomir |author2=O. Petrović |edition= |year=2011|publisher= Aerokomunikacije|location= Beograd|isbn=978-86-913973-2-6|ref=harv }}
{{Hanriot aircraft}}

5 : French military trainer aircraft 1920–1929|Hanriot aircraft|Biplanes|Single-engined tractor aircraft|Aircraft first flown in 1925

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