| 词条 | Hanriot H.180 | ||||||||||||||||
| 释义 |
The Hanriot H.170, H.180, and H.190 were a family of light utility aircraft produced in France in the 1930s. All introduced in 1934, they appeared side-by-side at the Paris Air Show that year, the model numbers distinguishing between versions powered by Salmson, Renault, and Régnier engines respectively. Design and developmentIn basic construction, the different variants were otherwise almost identical, as largely conventional monoplanes with high, strut-braced wings and fixed, tailskid undercarriage. The pilot and one or two passengers sat in an extensively-glazed, enclosed cabin. Although usually described as a monoplane, this family of aircraft all featured small, stub wings at the bottom of the fuselage. These carried the fuel tanks and served as a mounting point for the wing struts and undercarriage. An interesting feature was that the upper portion of the rear fuselage was a removable module, allowing it to be replaced with alternative modules for different roles, for example to carry a stretcher, or a second, open cockpit for pilot or gunnery training. Operational historyThe H.182 was the major production version, accounting for 346 out of the total of 392 aircraft built. Most of these were produced as part of a government order for machines to equip the Cercles Aériens Régionaux reserve flying units, with 172 aircraft still operational at the Fall of France in 1940. Ten more were purchased by the Second Spanish Republic for use in the Spanish Civil War, and 50 aircraft originally ordered by the French government were diverted to Turkey as part of a military aid agreement. VariantsH.170
H.180
H.190
Operators
Specifications (H.182){{aerospecs|ref= |met or eng?=met |crew=Two, pilot and instructor |capacity= |length m=7.22 |length ft=23 |length in=8 |span m=12.00 |span ft=39 |span in=5 |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=3.15 |height ft=10 |height in=4 |wing area sqm=19.0 |wing area sqft=204 |swept area sqm= |swept area sqft= |rot area sqm= |rot area sqft= |volume m3= |volume ft3= |aspect ratio= |empty weight kg=604 |empty weight lb=1,331 |gross weight kg=887 |gross weight lb=1,955 |lift kg= |lift lb= |eng1 number=1 |eng1 type=Renault 4Pei |eng1 kw=104 |eng1 hp=140 |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=190 |max speed mph=120 |max speed mach= |cruise speed kmh= |cruise speed mph= |range km=600 |range miles=370 |endurance h= |endurance min= |ceiling m=5,500 |ceiling ft=18,400 |glide ratio= |climb rate ms= |climb rate ftmin= |sink rate ms= |sink rate ftmin= |armament1= |armament2= |armament3= |armament4= |armament5= |armament6= }} See also{{aircontent||related= |similar aircraft= |sequence= |lists=
|see also= }} References
External links
6 : French civil utility aircraft 1930–1939|French military utility aircraft 1930–1939|Hanriot aircraft|High-wing aircraft|Single-engined tractor aircraft|Aircraft first flown in 1934 |
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