Experimentální létající člun Giju č. 3

Experimental Giyu No.3 Flying Boat
第三義勇飛行艇
     
Název:
Name:
Experimentální létající člun Giju č. 3 Experimental Giyu No.3 Flying Boat
Originální název:
Original Name:
第三義勇飛行艇
Kategorie:
Category:
experimentální letoun experimental aeroplane
Výrobce:
Producer:
DD.MM.1928-DD.08.1928 Kawasaki Shipyard, Ltd., Kobe /
Období výroby:
Production Period:
DD.04.1927-DD.08.1928
Vyrobeno kusů:
Number of Produced:
1
První vzlet:
Maiden Flight:
DD.08.1928
Osádka:
Crew:
5~10
Základní charakteristika:
Basic Characteristics:
 
Vzlet a přistání:
Take-off and Landing:
CTOL - konvenční vzlet a přistání CTOL - conventional take-off and landing
Uspořádání křídla:
Arrangement of Wing:
jednoplošník monoplane
Uspořádání letounu:
Aircraft Concept:
klasické conventional
Podvozek:
Undercarriage:
pevný fixed
Přistávací zařízení:
Landing Gear:
člunový trup flying boat
Technické údaje:
Technical Data:
 
Hmotnost prázdného letounu:
Empty Weight:
5400 kg 11905 lb
Vzletová hmotnost:
Take-off Weight:
8600 kg 18960 lb
Maximální vzletová hmotnost:
Maximum Take-off Weight:
? kg ? lb
Rozpětí:
Wingspan:
29,500 m 96ft 9,42in
Délka:
Length:
19,972 m 65ft 6,29in
Výška:
Height:
5,272 m 17ft 3,56in
Plocha křídla:
Wing Area:
141,00 m2 1517.71 ft2
Plošné zatížení:
Wing Loading:
60,993 kg/m2 12.49 lb/ft2
Pohon:
Propulsion:
 
Kategorie:
Category:
pístový piston
Počet motorů:
Number of Engines:
2
Typ:
Type:
Kawasaki-BMW VI, kapalinou chlazený vidlicový dvanáctiválec v tandemovém uspořádání, výkon 368-552 kW (500-750 k).
Vrtule dvoulisté dřevěné nebo
čtyřlisté kovové s pevným úhlem náběhu.
Kawasaki-BMW VI twelve-cylinder vee water-cooled engines mounted in tandem, rated 493-740 hp,
driving a two-blade wooden propellers late four-blade fixed-pitch metal propellers.
Objem palivových nádrží:
Fuel Tank Capacity:
? ?
Výkony:
Performance:
 
Maximální rychlost:
Maximum Speed:
196.3 km/h v 0 m 122 mph in 0 ft
Cestovní rychlost:
Cruise Speed:
155 km/h v 2000 m mph in ft
Rychlost stoupání:
Climb Rate:
? m/s ? ft/min
Čas výstupu na výšku:
Time to Climb to:
15,5 min do 2000 m 15,5 min to 6562 ft
Operační dostup:
Service Ceiling:
4500 m 14764 ft
Dolet:
Range:
1110 km 690 mi
Maximální dolet:
Maximum Range:
3000 km 1864.1 mi
Výzbroj:
Armament:
1x pohyblivý kulomet ráže 7,7 mm v předním střelišti,
1x pohyblivý kulomet ráže 7,7 mm ve hřbetním střelišti a
1x pohyblivý kulomet ráže 7,7 mm ve spodním střelišti.
Pumový náklad: 2x 250 kg pumy.
One flexible 0.303 inch machine-gun in nose position,
one flexible 0.303 inch machine-gun in dorsal position and
one flexible 0.303 inch machine-gun in ventral position.
Bomb load: two 551 lb bombs.
bombs.,
one dorsal flexible 7.7mm machinegun,
one ventral flexibl 7. 7mm machinegun.
Bomb load: two 2S0kg (551Ib)
bombs.
Uživatelské státy:
User States:
- -
Poznámka:
Note:
Letová vytrvalost: 5,5 h


viz historie
Endurance: 5 hours 30 minutes


The aeroplane was given good marks in general performance but had shortcomings in roughish water and vibration developed around the engine nacelle causing other related problems and a decrease in performance and greatly hampered further test fIying.
Zdroje:
Sources:
Robert C. Mikesh and Shorzoe Abe, Japanese Aircraft 1910-1941, Naval Institute Press Annapolis, Maryland 21402, 1990, ISBN: 1-155750-563-2
archiv autora
URL : https://www.valka.cz/Experimentalni-letajici-clun-Giju-c-3-t50713#194493 Version : 0
Brief history:


In September 1926, shortly after the destruction of an experimental seaplane Kaiba Ginkai KB, adopted the voluntary committee of the Kaibo Gikai decision to build another large seaplane. The new seaplane was to be built on the basis of a completely new design. This construction had several objectives, both the designers and the technicians had to gain experience with the design and construction of all-metal flying boats, and on maritime pilots and mechanics could acquaint with all-metal aircraft in operation, mainly with the differences in maintenance and operating instructions.


On the construction of the work together naval and civilian engineers, which was led by Dr. Aikichi Tanakadate and Narihisa Yokota, he was the chief designer, naval air force supervised the naval lieutenant engineer Yoshio Hashiguchi. The designers used the experience gained during the construction of the seaplane Kaiba Ginkai KB, Dornierova Walu and also the experience gained in the German factory of Rohrbach, where they were some japanese specialists on the intern.
The new aircraft was from April 1927 to August 1928 built in the shipyards of Kawasaki in Kobe, was designated as an Experimental flying boat Gyiu no. 3 (Experimental Giyu Well.3 Flying-boat) and featured at the time the largest japanese plane. Drive put two on-line monitoring of the stored fork-engines of the BMW VI with the power of 500 horses, which the motorcycle department of the Kawasaki under license produced. The performance of the engine first, carry forward the dvoulisté wooden propellers, which were later, already during the tests, replaced by čtyřlistými propellers metal. These propellers were subsequently exchanged for wooden dvoulisté, because there was concern about the possible destruction of the metal propeller.


After the completion of the was the flying boat was transported to the base in Jokosuce, where they were immediately launched test flights. During the intensive six-month testing, it was found that the hydroplane has a very good performance, but large flaws revealed on the choppy water surface. The aircraft was also for the whole period of tests, accompanied by strong vibration of the engines, this vibration led to the fact that the engines could not achieve the full performance and the tests were strongly limited. The vibration of the engines they tried to remove the engineers in the maritime arsenal in Hiru, the aircraft was again tested with metal and wooden propellers, but it was done already only a few flights at low altitude.


In may of the year 1931 was a seaplane in Hiru disassembled, and all disassembled parts have been subjected to a thorough inspection, during which it was monitored by their wear and fatigue of the material.


sources:
Robert C. Mikesh and Shorzoe Abe, Japanese Aircraft 1910-1941, Naval Institute Press Annapolis, Maryland 21402, 1990, ISBN: 1-155750-563-2
author archive
.
URL : https://www.valka.cz/Experimentalni-letajici-clun-Giju-c-3-t50713#419286 Version : 0

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Fotografie tohoto experimentálního letadla.
Zdroj:
Robert C. Mikesh and Shorzoe Abe, Japanese Aircraft 1910-1941, Naval Institute Press Annapolis, Maryland 21402, 1990, ISBN: 1-155750-563-2

Experimentální létající člun Giju č. 3 -


URL : https://www.valka.cz/Experimentalni-letajici-clun-Giju-c-3-t50713#194494 Version : 0
It looks like the corporate designation sounded Kawasaki KDN-1, or (according to the japanese wiki) KDN-2.

www.secretprojects.co.uk
ja.wikipedia.org
.
Experimentální létající člun Giju č. 3 -


Experimentální létající člun Giju č. 3 -


Experimentální létající člun Giju č. 3 -


URL : https://www.valka.cz/Experimentalni-letajici-clun-Giju-c-3-t50713#575484 Version : 0
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