翻訳と辞書
Words near each other
・ Romano Galvani
・ Romano Garagnani
・ Romano Guardini
・ Romano Kristoff
・ Romano L. Mazzoli
・ Romano Lemm
・ Romano Maria la Russa
・ Romano Mussolini
・ Romano Negri
・ Romano Obilinović
・ Romano Perticone
・ Romano Pontifici Eligendo
・ Romano Prodi
・ Romano Puppo
・ Romano R.82
Romano R.90
・ Romano Racing
・ Romano Ricciardi
・ Romano Rodrigues
・ Romano Romanelli
・ Romano Scarpa
・ Romano Scavolini
・ Romano Scott
・ Romano Sgheiz
・ Romano Sion
・ Romano Terblanche
・ Romano Tozzi Borsoi
・ Romano TV
・ Romano Voltolina
・ Romano WE84


Dictionary Lists
翻訳と辞書 辞書検索 [ 開発暫定版 ]
スポンサード リンク

Romano R.90 : ウィキペディア英語版
Romano R.90

The Romano R.90 was a prototype single-seat French floatplane fighter of the 1930s. A single example of the R.90 was built, but the type did form the basis of the Romano R.83 and Romano R.92 fighters which were built in secret for the Spanish Republicans during the Spanish Civil War.
==Design and development==
In 1933, the French Navy issued a specification for a single-seat seaplane fighter capable of being operated from the catapults of its Cruisers and Battleships. To meet this requirement, the Chantiers aéronavals Étienne Romano designed a floatplane, the Romano R.90, with designs also being prepared by Loire, Bernard and Potez.〔Green and Swanborough 1994, p. 353.〕
Unlike the other three designs, the R.90 was a biplane. It was of mixed construction, with a welded steel-tube fuselage and wooden, single-bay wings,〔Green and Swanborough 1994, p. 502.〕 with the upper wings being gulled into the top of the fuselage to give a better view for the pilot.〔Donald 1997, p. 785.〕 Two floats were fitted.〔 The proposed armament was four 7.5mm machine guns, two in the lower wing and two in the floats.〔''Flight'' 23 January 1936, p. 87.〕〔Parmentier, B. ("Romano R-90" ). ''Aviafrance''. 30 November 2001. Retrieved 18 December 2010.〕
It made its maiden flight in August 1935, powered by a 720 hp (537 kW) Hispano-Suiza 9Vbrs radial engine. With this engine it reached a speed of 352 km/h (219 mph).〔 In October that year it was re-engined with a 680 hp (507 kW) Hispano-Suiza 14Hbrs radial in a NACA cowling, increasing the speed and the floats were modified.〔〔 It was re-engined again in October 1937 with a 900 hp (671 kW) Hispano-Suiza 12Ycrs-1 V12 engine with a 20mm cannon firing through the propeller boss. Despite reaching 400 km/h (248 mph),〔Green and Swanborough 1994, p. 503.〕 faster than any of the other competitors,〔Green and Swanborough 1994, pp. 62, 353, 481–482.〕 the R.90 was not ordered into production, 20 Loire 210s being purchased instead.〔
Although the attempts to sell the R.90 to the French Navy failed, the aircraft attracted the attention of the Spanish Republican Air Force, which placed an order for 24 of a landplane derivative, the Romano R.83. This differed in having a conventional fixed tailwheel undercarriage, a non-gulled upper wing and was to be powered by a 450 hp (336 kW) Pratt & Whitney Wasp Junior engine. These aircraft were to be assembled in secret by the Belgium company LACEBA (Les Atleliers de Construction et d'Exploitation de Brevets Aéronautiqes). Flight testing in Belgium was carried out with a 280 hp (209 kW) Salmson 9ABa engine, to give the impression that the aircraft was a trainer rather than a fighter, with the more powerful engine to be fitted when the aircraft was delivered to Spain.〔
A second landplane fighter derivative was designed and built for the Spanish Republicans, the Romano R.92. This was powered by a Hispano-Suiza 12Ycrs engine as tested in the Romano R.90, and reverted to the gulled upper wing of the floatplane. A single example was built in 1938.〔

抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
ウィキペディアで「Romano R.90」の詳細全文を読む



スポンサード リンク
翻訳と辞書 : 翻訳のためのインターネットリソース

Copyright(C) kotoba.ne.jp 1997-2016. All Rights Reserved.