请输入您要查询的百科知识:

 

词条 RWD 6
释义

  1. Development

  2. Description

  3. Specifications

  4. See also

  5. References

name =RWD 6image =RWD 6.jpgcaption =RWD 6 of Franciszek Zwirko during a short take-off trial at the Challenge 1932

}}{{Infobox Aircraft Type

type =Sports planemanufacturer =Warsaw University of Technology workshopsdesigner = RWD teamfirst flight =3 June 1932introduced =1932retired =1935status =primary user =Polish civilian aviationmore users =produced =number built =3unit cost =variants with their own articles =
}}

The RWD 6 was a Polish sports plane of 1932, constructed by the RWD team. It was a winner of the Challenge 1932 international tourist aircraft contest.

Development

The aircraft was designed specially for the purpose of competing in the international tourist aircraft contest Challenge, which RWD attended in 1930, without major success. It was constructed by the RWD team of Stanislaw Rogalski, Stanislaw Wigura and Jerzy Drzewiecki in the workshops of Students' Mechanical Club of Warsaw University of Technology (their designs were named RWD after their initial letters). The new plane differed from previous RWD designs, having a cab with two seats next to each other, folding wings and good wing mechanization (slats and flaps).

Only three aircraft were built, the first one was flown on June 3, 1932 by its designer Jerzy Drzewiecki. The aircraft were given civilian registrations SP-AHL, SP-AHM and SP-AHN. During trials, SP-AHM crashed and Drzewiecki was hurt. After some modification of the tail, the two remaining RWD 6s were sent to the Challenge contest.

Challenge 1932, held between August 11 – August 28, 1932, was eventually won by Franciszek Żwirko (pilot) and Stanisław Wigura (mechanic) in their RWD 6 SP-AHN, with a start number O6. The other RWD 6, flown by Tadeusz Karpiński, took ninth place out of 43 competitors (SP-AHL, nr. O4). During contest, the RWD 6 was given the highest scores for technical evaluation of all participating aircraft.

On September 11, 1932, the RWD 6 SP-AHN with Franciszek Żwirko and Stanisław Wigura aboard, crashed during a storm while flying to an air meeting in Czechoslovakia. Both died. The cause was found to be weak wing mountings, that caused wing warping at higher speeds. The last remaining RWD 6 (SP-AHL) was modified after this accident, receiving a strengthened wing with V-shaped struts and the new designation RWD 6bis. The RWD 6bis was completed and flown in September 1933. In 1935 it was broken up, and its fuselage was used to create the RWD 13 touring plane prototype. A direct development of the RWD 6 as a sport plane was a four-seater RWD 9, a winner of the Challenge 1934.

Description

Two-seater sports and touring strutted high-wing monoplane of a mixed construction. A metal frame fuselage covered with canvas, with the engine clad in aluminium sheets. Rectangular single-spar wing of wooden construction, canvas and plywood covered. Wings folded rearwards, and were equipped with automatic slats and flaps. Closed cabin with two seats side-by-side, with dual controls. The cabin had a pair of doors. 7-cylinder Armstrong Siddeley Genet Major radial engine of 104 kW (140 hp) (119 kW, 160 hp start power). Two-blade metal propeller. Conventional landing gear, with a rear skid. Fuel tanks in wings (140 l, 34 US gal). Take-off: 111 m (to altitude 8 m), landing: 106 m (from altitude 8 m – best results from the Challenge contest).

Specifications

{{Aircraft specifications|
|plane or copter?=plane
|jet or prop?=prop
|crew=2
|capacity=2
|length main=6.6 m
|length alt=21 ft 8 in
|span main=11.0 m
|span alt=36 ft 1 in
|height main=2.07 m
|height alt=6 ft 9 in
|area main=16.00 m²
|area alt= 172 ft²
|empty weight main= 474 kg
|empty weight alt= 1,045 lb
|loaded weight main=
|loaded weight alt=
|useful load main= 276 kg
|useful load alt= 607 lb
|max takeoff weight main= 750 kg
|max takeoff weight alt=1,650 lb
|engine (prop)=Armstrong Siddeley Genet Major
|type of prop= air-cooled 7-cylinder radial engine
|number of props=1
|power main=160 hp
|power alt=119 kW
|max speed main=216 km/h
|max speed alt=134 mph
|stall speed main= 57.6 km/h
|stall speed alt= 36 mph
|range main=850 km
|range alt=530 miles
|ceiling main=6,000 m
|ceiling alt=19,700 ft
|climb rate main=5.5 m/s
|climb rate alt=1,080 ft/min
|loading main=47 kg/m²
|loading alt= 9.6 lb/ft²
|power/mass main= 5.3 hp/kg
|power/mass alt=
}}

See also

{{Aircontent
|related=
  • RWD 9
  • RWD 13

|similar aircraft=
|lists=
|see also=
}}

References

{{commons category|RWD 6}}
  • Andrzej Glass: "Polskie konstrukcje lotnicze 1893–1939" (Polish aviation constructions 1893–1939), WKiŁ, Warsaw 1977 (Polish language, no ISBN)
{{RWD aircraft}}

5 : Polish sport aircraft 1930–1939|RWD aircraft|Single-engined tractor aircraft|High-wing aircraft|Aircraft first flown in 1932

随便看

 

开放百科全书收录14589846条英语、德语、日语等多语种百科知识,基本涵盖了大多数领域的百科知识,是一部内容自由、开放的电子版国际百科全书。

 

Copyright © 2023 OENC.NET All Rights Reserved
京ICP备2021023879号 更新时间:2024/9/20 20:43:29