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The Dornier Do 212 was a four-seat experim … The Dornier Do 212 was a four-seat experimental amphibian flying boat built by the Swiss subsidiary of Dornier, in Altenrhein on Lake Constance. Design was initiated in 1938 by the German and Swiss branches, the latter being responsible for the actual construction of the prototype. The Do 212 was an all-metal cantilever monoplane with fixed wingtip floats and a 343 kW (460 hp) Hirth HM 512-B-0 12-cylinder air-cooled engine which, mounted aft of the cabin, was buried in the fuselage and drove a four-blade airscrew aft of the tail by means of a shaft which could be tilted upward 12° to provide water clearance. Initial water taxiing trials resulted in the enlarging of the wingtip floats. On 3 August 1942, a few attempts to take off from water were made, but these failed. A Do 24 was used to tow the Do 212 and it finally flew; however, instability forced the pilot to ditch just after takeoff. Further trials ended the same way. Difficulties were also experienced with the extension shaft, and the cooling of the engine presented a problem. Consequently, no further testing was undertaken, and the prototype was scrapped in 1943.n, and the prototype was scrapped in 1943.
, Il Dornier Do 212 era un aereo anfibio leg … Il Dornier Do 212 era un aereo anfibio leggero da trasporto passeggeri progettato dall'azienda tedesca Dornier-Werke GmbH e realizzato in Svizzera, nella sua sussidiaria nei primi anni quaranta. Dotato di soluzioni tecniche innovative, venne realizzato per poter soddisfare il mercato del trasporto leggero a corto raggio ma a causa di una serie di problemi tecnici mai risolti non venne avviato alla produzione.risolti non venne avviato alla produzione.
, O Dornier Do 212 foi um hidroavião anfíbio … O Dornier Do 212 foi um hidroavião anfíbio construído pela Dornier. O projecto foi iniciado em 1938 pela empresa da Dornier na Alemanha e na Suíça, ficando a última responsável pela construção. Era um avião todo em metal, monoplano e monomotor. Após o primeiro voo, a performance demonstrada pela aeronave deixaram muito a desejar, apresentando dificuldade em descolar e instabilidade durante o voo. Por fim, o único exemplar construído foi transformado em sucata em 1943.truído foi transformado em sucata em 1943.
, ドルニエ Do 212は4座席の水陸両用の実験機である。ドルニエのスイス工場で製作さ … ドルニエ Do 212は4座席の水陸両用の実験機である。ドルニエのスイス工場で製作された。1938年にドイツのドルニエとスイスの工場で設計が始められ、試作機はスイス工場が製作した。 全金属機で翼端にフロートを取り付け、460 bpの空冷12気筒エンジンは胴体内に収納され、水面から離れて取り付けられた推進式の4枚羽のプロペラを12度傾いたシャフトで駆動するという設計がなされた。 初期の滑走試験の結果、翼端フロートが大きくされた。1942年8月3日、離水試験が行われたが、離水できなかった。 Do 24によって牽引され離水したが、不安定な飛行特性のためにパイロットはすぐに着水させた。試験飛行はそれで終わった。延長シャフトに伴う問題やエンジンの冷却の問題が明白となり、開発は中止され試作機は1943年に廃棄された。題やエンジンの冷却の問題が明白となり、開発は中止され試作機は1943年に廃棄された。
, Die Dornier Do 212 war ein einmotoriges, v … Die Dornier Do 212 war ein einmotoriges, viersitziges Amphibienflugzeug der Dornier-Werke. Die Entwicklung wurde 1938 durch Dornier Friedrichshafen initiiert und im Dornierwerk Altenrhein ab 1941 ein Prototyp konstruiert. Das Flugzeug wurde von einem luftgekühlten 450-PS-Zwölfzylinder-V-Motor Hirth HM 512B-0 mit vierblättrigem Druckpropeller angetrieben, der an einem 2,9 m langen Ausleger über das Heck mit Doppelleitwerk hinausgehend für Start und Landung um 12° nach oben schwenkbar war. Der freitragende Ganzmetall-Schulterdecker hatte starre Stützschwimmer an den Randbögen und ein Bugrad-Einziehfahrwerk. Nach Fertigstellung des Prototyps HB-GOG im Jahr 1942 und „Rollversuchen“ auf dem Wasser wurden die Stützschwimmer vergrößert. Ende Juli 1942 war das Flugzeug fertig für einen Flugversuch. Am 3. August 1942 machte Egon Fath ein paar vergebliche Eigenstartversuche aus dem Wasser. Der Erstflug gelang nur im Schlepp einer Do 24. Nachdem auch spätere Eigenstartversuche scheiterten, das Flugzeug sehr instabil flog und Probleme mit der Fernwelle sowie der Motorkühlung auftraten, wurde das Projekt aufgegeben und der Prototyp 1943 verschrottet.egeben und der Prototyp 1943 verschrottet.
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The Dornier Do 212 was a four-seat experim … The Dornier Do 212 was a four-seat experimental amphibian flying boat built by the Swiss subsidiary of Dornier, in Altenrhein on Lake Constance. Design was initiated in 1938 by the German and Swiss branches, the latter being responsible for the actual construction of the prototype. the actual construction of the prototype.
, ドルニエ Do 212は4座席の水陸両用の実験機である。ドルニエのスイス工場で製作さ … ドルニエ Do 212は4座席の水陸両用の実験機である。ドルニエのスイス工場で製作された。1938年にドイツのドルニエとスイスの工場で設計が始められ、試作機はスイス工場が製作した。 全金属機で翼端にフロートを取り付け、460 bpの空冷12気筒エンジンは胴体内に収納され、水面から離れて取り付けられた推進式の4枚羽のプロペラを12度傾いたシャフトで駆動するという設計がなされた。 初期の滑走試験の結果、翼端フロートが大きくされた。1942年8月3日、離水試験が行われたが、離水できなかった。 Do 24によって牽引され離水したが、不安定な飛行特性のためにパイロットはすぐに着水させた。試験飛行はそれで終わった。延長シャフトに伴う問題やエンジンの冷却の問題が明白となり、開発は中止され試作機は1943年に廃棄された。題やエンジンの冷却の問題が明白となり、開発は中止され試作機は1943年に廃棄された。
, O Dornier Do 212 foi um hidroavião anfíbio … O Dornier Do 212 foi um hidroavião anfíbio construído pela Dornier. O projecto foi iniciado em 1938 pela empresa da Dornier na Alemanha e na Suíça, ficando a última responsável pela construção. Era um avião todo em metal, monoplano e monomotor. Após o primeiro voo, a performance demonstrada pela aeronave deixaram muito a desejar, apresentando dificuldade em descolar e instabilidade durante o voo. Por fim, o único exemplar construído foi transformado em sucata em 1943.truído foi transformado em sucata em 1943.
, Il Dornier Do 212 era un aereo anfibio leg … Il Dornier Do 212 era un aereo anfibio leggero da trasporto passeggeri progettato dall'azienda tedesca Dornier-Werke GmbH e realizzato in Svizzera, nella sua sussidiaria nei primi anni quaranta. Dotato di soluzioni tecniche innovative, venne realizzato per poter soddisfare il mercato del trasporto leggero a corto raggio ma a causa di una serie di problemi tecnici mai risolti non venne avviato alla produzione.risolti non venne avviato alla produzione.
, Die Dornier Do 212 war ein einmotoriges, v … Die Dornier Do 212 war ein einmotoriges, viersitziges Amphibienflugzeug der Dornier-Werke. Die Entwicklung wurde 1938 durch Dornier Friedrichshafen initiiert und im Dornierwerk Altenrhein ab 1941 ein Prototyp konstruiert. Das Flugzeug wurde von einem luftgekühlten 450-PS-Zwölfzylinder-V-Motor Hirth HM 512B-0 mit vierblättrigem Druckpropeller angetrieben, der an einem 2,9 m langen Ausleger über das Heck mit Doppelleitwerk hinausgehend für Start und Landung um 12° nach oben schwenkbar war. Der freitragende Ganzmetall-Schulterdecker hatte starre Stützschwimmer an den Randbögen und ein Bugrad-Einziehfahrwerk. Randbögen und ein Bugrad-Einziehfahrwerk.
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, Do 212 (航空機)
|
