Not to be confused with the Kawanishi K6K1 seaplane trainer of 1938.
The Kawanishi K-6 was a passenger-carrying biplane floatplane, built in Japan in the 1920s. The sole example took part in an around Japan flight then flew as a transport with Japan Aviation.
Kawanishi's first floatplane design was the K-5, which though foreseen as Japan's first successful large seaplane transport turned out to lack the power to take-off carrying any significant load. As no more powerful engine than the 260–305 hp (194–227 kW) Maybach Mb.IV was available, the K-5's development was abandoned late in 1922. Instead, Eiji Sekiguchi designed a new, smaller, lighter aircraft with the same engine. This, the K-6, was informed by the latest control and stability research from Göttingen. It was completed in November 1923 and was intended to be used by Kawanishi's Nippon Koku KK (Japan Aviation Co. Ltd)[1]
The K-6 was a two bay biplane with fabric covering over a wooden structure. Its equal span wings were rectangular in plan out to rounded tips and braced together without stagger by parallel pairs of interplane struts. The pilot's open cockpit was between the wings, close behind the upright, water-cooled Maybach. The K-6's two passengers were in a separate cockpit behind him, originally open but later enclosed under multi-panel glazing faired smoothly into the upper rear fuselage. The latter was flat sided and remained deep to the tail; its surface served to stabilize the aircraft in yaw and there was no conventional fixed fin. The K-6 had a straight-edged, round-topped rudder, hinged on the extreme fuselage and cut-away for elevator movement, which was unusual in projecting only below the fuselage. Its tailplane was mounted on top of the fuselage and braced to the lower fuselage longerons with pairs of parallel struts.[1]
The sides of its flat-surfaced floats met at bow and stern. Each float had a shallow step under the trailing edge. They were held under the fuselage on fore and aft struts to the lower longerons.[1]
Operational historyedit
Soon after completion it was decided that instead of immediate commercial use the K-6 should be part of the Around Japan Flight, an event sponsored by Nippon Koku KK and the Daimai Tonichi Shimbun newspaper. Some modifications followed: the passenger seats were replaced with extra fuel tanks, the engine radiator was moved, shallow fins were added on the tailplane undersides together with outrigger floats under the wing. Normally well above the water, these limited roll when afloat. The July 1924 flight began and ended at Osaka and covered 4,389 km (2,727 mi; 2,370 nmi). The K-6, flown by Yukichi Goto with flight engineer Minezo Yonesawa, covered the route in eight days, though flying for only 33 hr 48 min.[1]
On 2 December 1924 the K-6 won the seaplane category in the competitive Round Ise Bay event, covering three circuits totalling 850 km (530 mi; 460 nmi) in 6 hr 30 min. After that the K-6, with passenger seats reinstalled, was returned to transport duties. No more were built as Kawanishi's attention turned to its successor, the K-7.[1]
^ abcdefMikesh, Robert C.; Abe, Shorzoe (1990). Japanese Aircraft 1910-1941. London: Putnam Publishing. p. 127-8. ISBN1-55750-563-2.
January 01, 1970
kawanishi, confused, with, kawanishi, k6k1, seaplane, trainer, 1938, passenger, carrying, biplane, floatplane, built, japan, 1920s, sole, example, took, part, around, japan, flight, then, flew, transport, with, japan, aviation, role, three, seat, civil, floatp. Not to be confused with the Kawanishi K6K1 seaplane trainer of 1938 The Kawanishi K 6 was a passenger carrying biplane floatplane built in Japan in the 1920s The sole example took part in an around Japan flight then flew as a transport with Japan Aviation Kawanishi K 6 Role Three seat civil floatplane transport National origin Japan Manufacturer Kawanishi Designer Eiji Sekiguchi First flight 1923 Primary user Japan Aviation Number built 1 Contents 1 Design and development 2 Operational history 3 Specifications 4 ReferencesDesign and development editKawanishi s first floatplane design was the K 5 which though foreseen as Japan s first successful large seaplane transport turned out to lack the power to take off carrying any significant load As no more powerful engine than the 260 305 hp 194 227 kW Maybach Mb IV was available the K 5 s development was abandoned late in 1922 Instead Eiji Sekiguchi designed a new smaller lighter aircraft with the same engine This the K 6 was informed by the latest control and stability research from Gottingen It was completed in November 1923 and was intended to be used by Kawanishi s Nippon Koku KK Japan Aviation Co Ltd 1 The K 6 was a two bay biplane with fabric covering over a wooden structure Its equal span wings were rectangular in plan out to rounded tips and braced together without stagger by parallel pairs of interplane struts The pilot s open cockpit was between the wings close behind the upright water cooled Maybach The K 6 s two passengers were in a separate cockpit behind him originally open but later enclosed under multi panel glazing faired smoothly into the upper rear fuselage The latter was flat sided and remained deep to the tail its surface served to stabilize the aircraft in yaw and there was no conventional fixed fin The K 6 had a straight edged round topped rudder hinged on the extreme fuselage and cut away for elevator movement which was unusual in projecting only below the fuselage Its tailplane was mounted on top of the fuselage and braced to the lower fuselage longerons with pairs of parallel struts 1 The sides of its flat surfaced floats met at bow and stern Each float had a shallow step under the trailing edge They were held under the fuselage on fore and aft struts to the lower longerons 1 Operational history editSoon after completion it was decided that instead of immediate commercial use the K 6 should be part of the Around Japan Flight an event sponsored by Nippon Koku KK and the Daimai Tonichi Shimbun newspaper Some modifications followed the passenger seats were replaced with extra fuel tanks the engine radiator was moved shallow fins were added on the tailplane undersides together with outrigger floats under the wing Normally well above the water these limited roll when afloat The July 1924 flight began and ended at Osaka and covered 4 389 km 2 727 mi 2 370 nmi The K 6 flown by Yukichi Goto with flight engineer Minezo Yonesawa covered the route in eight days though flying for only 33 hr 48 min 1 On 2 December 1924 the K 6 won the seaplane category in the competitive Round Ise Bay event covering three circuits totalling 850 km 530 mi 460 nmi in 6 hr 30 min After that the K 6 with passenger seats reinstalled was returned to transport duties No more were built as Kawanishi s attention turned to its successor the K 7 1 Specifications editData from Japanese Aircraft 1910 1941 1 General characteristicsCrew one Capacity two passengers Length 9 90 m 32 ft 6 in Wingspan 13 60 m 44 ft 7 in Height 3 95 m 13 ft 0 in Wing area 43 6 m2 469 sq ft Airfoil RAF 15 Empty weight 1 150 kg 2 535 lb Gross weight 1 890 kg 4 167 lb Powerplant 1 Maybach Mb IVa six cylinder water cooled inline 194 227 kW 260 305 hp Propellers 2 bladed wooden Performance Maximum speed 167 km h 104 mph 90 kn Alighting speed 95 km h 59 mph 51 kn Endurance 4 hr Service ceiling 7 000 m 23 000 ft Time to altitude 17 min to 3 000 m 9 800 ft References edit a b c d e f Mikesh Robert C Abe Shorzoe 1990 Japanese Aircraft 1910 1941 London Putnam Publishing p 127 8 ISBN 1 55750 563 2 Retrieved from https en wikipedia org w index php title Kawanishi K 6 amp oldid 1101725032, wikipedia, wiki, book, books, library,
