Английская Википедия:Hennion two-seater

Материал из Онлайн справочника
Версия от 15:52, 20 марта 2024; EducationBot (обсуждение | вклад) (Новая страница: «{{Английская Википедия/Панель перехода}} <!-- This article is a part of Wikipedia:WikiProject Aircraft. Please see Wikipedia:WikiProject Aircraft/page content for recommended layout. --> {|{{Infobox aircraft begin | name=Hennion | image= | caption= }}{{Infobox aircraft type | type=Two seat sports aircraft | national origin=France | designer=Emile Hennion | first flight=28 August 1939 | introduced= | retir...»)
(разн.) ← Предыдущая версия | Текущая версия (разн.) | Следующая версия → (разн.)
Перейти к навигацииПерейти к поиску

The Hennion was a two-seat French training and touring aircraft, completed just before World War II began. It was flown again post-war and later fitted with a new engine; it survived into the early 1960s.

Design and development

Emile Hennion was the chief pilot at the Casablanca Aero Club in the 1930s. Just before the outbreak of World War II he designed, built and flew a side-by-side seat two seat aircraft, powered by a Train 4A 01 inverted four cylinder air-cooled engine which produced only Шаблон:Convert.[1][2] His goals were safety in the hands of a beginner, economy, comfort and true touring ability.[1] The first two features made it of some interest as an ab initio trainer after France had gone to war.[3]

In this pre-war form it was known as the Hennion 01. It was a low wing, cantilever monoplane, its wings straight tapered with blunt tips and of quite high aspect ratio (10). The wings were built around a single spar and fabric covered, though the ailerons were plywood skinned.[1]

The fuselage was flat sided and ply skinned, except behind the cockpit where rounded, raised decking was fabric covered. The Hennion's cockpit was fully enclosed under a two piece canopy with a sliding rear component. Its two seats were equipped with dual controls. Behind them there were luggage and light baggage/chart spaces, respectively Шаблон:Convert and Шаблон:Convert. The inverted Train engine in the nose drove a two blade propeller and its fuel tank held Шаблон:Convert.[1] At the rear the vertical tail was tall, with an unbalanced rudder which reached down to the keel and a fuselage mounted tailplane ahead of it.[3] The Hennion had a tail wheel undercarriage with a track of Шаблон:Convert, its spatted main wheels on vertical, streamlined legs.[1] The Hennion 01 flew for the first time on 28 September 1939 at Casablanca. Despite the low power, it had a maximum speed of Шаблон:Convert and cruised at Шаблон:Convert. Cruising, it used about Шаблон:Convert per hour, giving it a range around Шаблон:Convert. Landing speed was Шаблон:Convert.

The Hennion 01 survived the war and was flown again in 1949, now on the French civil register as F-WFOY.[2][4] After a period of disuse, it was re-engined in 1956 with a Шаблон:Convert Continental A65 air-cooled flat-four in a revised nose and redesignated the Hennion II.[2] The extra power gave a useful increase in speed despite an increase in empty weight of about 17%.[1][2] On 4 February 1962 it was destroyed at Meknes.[4]

Variants

Hennion 01
pre-war version with Train engine
Hennion II
1956 revision with a more powerful Continental engine

Specifications (Hennion II)

Шаблон:Aircraft specs

References

Шаблон:Reflist

  1. 1,0 1,1 1,2 1,3 1,4 1,5 Ошибка цитирования Неверный тег <ref>; для сносок LAiles39 не указан текст
  2. 2,0 2,1 2,2 2,3 Ошибка цитирования Неверный тег <ref>; для сносок GaillardI не указан текст
  3. 3,0 3,1 Ошибка цитирования Неверный тег <ref>; для сносок LAiles40 не указан текст
  4. 4,0 4,1 Ошибка цитирования Неверный тег <ref>; для сносок Chillon не указан текст