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词条 Kawanishi K-7 Transport Seaplane
释义

  1. Design and development

  2. Operational history

  3. Variants

  4. Operators

  5. Specifications (K-7A)

  6. References

name= K-7 Transport Seaplane image= caption=

}}{{Infobox Aircraft Type

type= Airliner national origin= Japan manufacturer= Kawanishi Aircraft Company designer= Eiji Sekiguchi first flight= 1924 introduced= 1925 retired= status= primary user= Nippon Koku KK more users= produced= number built= 11 program cost= unit cost= developed from= variants with their own articles=
}}

The Kawanishi K-7 Transport Seaplane was a Japanese single-engined biplane floatplane of the 1920s. Eleven were built from 1924 to 1927, being used to carry passengers and airmail.

Design and development

In December 1923, Eiji Sekiguchi, chief designer of the aircraft department of Kawanishi Kikai Setsakuho (Kawanishi Machinery Manufacturing Works), started design of a new high speed transport floatplane to equip Nippon Koku KK (Japan Aviation Co. Ltd.), an airline subsidiary of Kawanishi. Sekiguchi designed a single-engined sesquiplane (i.e. a biplane with the lower wing much smaller than the upper wing) of all-wooden construction. Seating for four passengers was provided in an enclosed cabin, while the aircraft's two pilots sat in individual open tandem cockpits aft of the passenger cabin. The aircraft was powered by a single Maybach Mb.IVa water-cooled inline-engine providing 305 hp (228 kW), an engine type usually used to power Zeppelins or Riesenflugzeug like the Zeppelin-Staaken R.VI, received as part of Germany's reparations to Japan after the end of the First World War.[1][2]

The first example of the new aircraft, the K-7A Transport Seaplane was completed in November 1924, demonstrating both good performance and handling. A further nine K-7As were built by the time production ended in 1927, together with a single example of the K-7B Mail-Carrying Aircraft, a modified version that could be operated either on floats or with a tailwheel undercarriage.[1]

Operational history

The K-7A entered service on Nippon Koku's service between Osaka and Fukuoka in January 1925, mainly carrying airmail rather than passengers. The K-7A proved successful in service, one carrying mail from Fukuoka and Shanghai, China, a distance of over {{convert|950|km|mi|sp=us}} in May 1926, while the K-7B was used together with the Kawanishi K-10 Transport to operate an airmail route between Osaka and the Japanese occupied city of Dalian in September 1926. The K-7A continued in use until 1929, when Nippon Koku was forced to be disbanded, with its routes transferred to the government owned Nihon Koko Yuso KK (Japan Air Transport).[4][3]

Variants

K-7A Transport Seaplane

Six-seat airliner/transport floatplane, powered by Maybach MIVa engine. Ten built.[1]

K-7B Mail-carrying Aircraft

Modified version of K-7A, capable of operating with a fixed tailwheel undercarriage or floats, powered by 440 hp (328 kW) Lorraine 1 V12 engine. One built in 1925.[4]

Operators

{{JPN}}
  • Dai Nippon Kōkū Kabushiki Kaisha The Imperial Japanese Airways, in short Nippon Koku KK.

Specifications (K-7A)

{{Aircraft specs
|ref=Japanese Aircraft 1910–1941[5]
|prime units?= met
|genhide=
|crew= 2
|capacity= 4 passengers
|length m= 11
|length ft=
|length in=
|length note=
|span m= 12
|span ft=
|span in=
|span note=
|height m= 4.08
|height ft=
|height in=
|height note=
|wing area sqm= 34
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg= 1250
|empty weight lb=
|empty weight note=
|gross weight kg= 2000
|gross weight lb=
|gross weight note=
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|lift kg=
|lift lb=
|lift note=
|more general=


|eng1 number= 1
|eng1 name= Maybach Mb.IVa
|eng1 type= water-cooled six-cylinder inline engine
|eng1 kw=
|eng1 hp= 305
|power original=
|thrust original=


|perfhide=
|max speed kmh=
|max speed mph=
|max speed kts= 106
|max speed note= at sea level
|max speed mach=
|range km=
|range miles=
|range nmi=
|range note=
|endurance= 6 hr
|ceiling m= 6000
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude=
|avionics=
}}{{aircontent
|see also=
|related=
|similar aircraft=
|lists=
}}

References

Notes
1. ^{{Harvnb|Mikesh and Abe|1990|pp=128–129.}}
2. ^{{Harvnb|Mikesh and Abe|1990|p=126.}}
3. ^History {{webarchive|url=https://web.archive.org/web/20100223022619/http://www.shinmaywa.co.jp/english/company/history.htm |date=2010-02-23 }} ShinMaywa Industries via http://www.shinmaywa.co.jp. Retrieved 7 June 2010.
4. ^{{Harvnb|Mikesh and Abe|1990|pp=129–131.}}
5. ^{{Harvnb|Mikesh and Abe|1990|p=129.}}
Bibliography
{{commons category|Kawanishi Aircraft Company}}{{refbegin}}
  • Mikesh, Robert C. and Shorzoe Abe. Japanese Aircraft 1910–1941. London: Putnam & Company Ltd., 1990. {{ISBN|0-85177-840-2}}.
{{refend}}{{Kawanishi aircraft}}

6 : Japanese airliners 1920–1929|Floatplanes|Kawanishi aircraft|Sesquiplanes|Single-engined tractor aircraft|Aircraft first flown in 1924

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