В.Шавров История конструкций самолетов в СССР до 1938 г.
"Меллер-III" ("Меллер № З"). За основу был взят самолет "Ньюпор-IV": его фюзеляж и шасси, но с двойной рессорой; крылья, но с элеронами взамен перекашивания. Горизонтальное оперение было взято от "Фармана-XIV". Двигатель - "Сальмсон" М-7 в 80 л. с., радиаторы были размещены по бортам фюзеляжа за летчиком. От двигателя шли цепные передачи к двум тянущим винтам, установленным на осях - стальных трубах под крыльями, у их передней кромки. Самолет был выпущен в 1913 г., себя не оправдал.
Самолет||
Год выпуска||1913
Двигатель, марка||
Мощность||80
Длина самолета, м||10,5
Размах крыла, м||12,4
Площадь крыла, м2||30
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H.Nowarra, G.Duval Russian Civil and Military Aircraft 1884-1969
Moska’s next design, the Moller III, was another solution of the problem of gun installation avoiding the propeller disc. A shoulder-wing two-seater monoplane, the Moller III had an 80 h.p. Salmson engine mounted in the fuselage with drive transmission to twin tractor propellers, the shafts of which were mounted on the lower surfaces of the wing. It would seem that the test results of this aircraft were unsatisfactory, although Salmson built the Salmson-Moineau SM 1 with a similar arrangement some time later, delivering it to Russia in 1917. The Moller III was the last machine built by Dux from their own designs.
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A.Durkota, T.Darcey, V.Kulikov The Imperial Russian Air Service (Flying Machines)
Meller III
This 1913 monoplane was powered by a Salmson 80hp water-cooled engine turning twin airscrews driven by chains attached to steel tubes on each wing. Some of the basic principals of the Nieuport IV were incorporated, but with modifications, such as the use of ailerons instead of wing warping. Tail components taken from the Farman XVI were also evident. Again, this machine was unsuccessful.
Dux-Built Aircraft Data
Specification Meller I Meller II Meller III Dux No.2 Dux Military Bleriot XIbis Bleriot XI Dux Farman IV Farman VII Farman IX
Year Built 1913 1913 1913 1913 1915 1910 1912 1910 1911 1911
Max. Speed, km/h - - - - - 95 90 65 86 90
Landing Spd, km/h - - - - - - - 60 60 60
Engines, number 1 1 1 1 1 1 1 1 1 1
type G-M G-M Salmson Gnome G-M Gnome Gnome Gnome Gnome Gnome
Power, hp 100 100 80 80 100 50 50 50 50 70
Length, m 9.4 8.1 10.5 7.6 7.6 775 7.2 12.5 9.0 8.0
Span, m (U/L) 12.1 13.7 12.4 12.3 11.2 8.9 8.9 10.5 12.0/7.0 12.0/7.0
Wing Area, m2 22.5 35.0 30.0 22.5 18.0 14.5 20.9 41.0 31.0 28.0
Empty Wt., kg 440 460 - - 420 240 295 400 345 260
Fuel Wt., kg 95 100 - - 130 - 30 75 75
Oil Wt., kg 25 total - - total total 35 total total total
Payload, kg 280 250 - - 280 130 145 180 255 225
Gross Wt., kg 720 710 700 370 440 580 600 485
Wing Load, kg/m2 320 20.3 - - 39.0 25.0 21.0 14.0 19.4 17.3
Power, kg/hp 7.2 7.1 - - 7.0 7.4 8.8 11.6 12.0 7.0
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