| 词条 | Heinkel He 119 | |||||||||||||||||
| 释义 |
The Heinkel He 119 was an experimental single-propeller monoplane with two coupled engines, developed in Germany. A private venture by Heinkel to test radical ideas by the Günter brothers, the He 119 was originally intended to act as an unarmed reconnaissance bomber capable of eluding all fighters due to its high performance. DevelopmentDesign was begun in the late summer of 1936. A notable feature of the aircraft was the streamlined fuselage, most likely as an evolutionary descendant of the 1932-vintage Heinkel He 70 record-setting single-engined mailplane design, but without the He 70's protruding canopy-enclosed crew accommodation existing anywhere along the exterior. Instead, the He 119's forward fuselage featured an extensively glazed cockpit forming the nose itself, heavily framed with many diagonally braced windows immediately behind the propeller spinner's rear edge. Two of the three-man crew sat on either side of the driveshaft, which ran aft to a "power system", a coupled pair of Daimler-Benz DB 601 engines mounted above the wing center-section within the fuselage, mounted together within a common mount (the starboard component engine having a "mirror-image" centrifugal supercharger) with a common gear reduction unit fitted to the front ends of each component engine, forming a drive unit known as the DB 606, the first German aircraft to use the "high-power" powerplant system. meant to provide German aircraft with an aviation powerplant design of over-1,500 kW (2,000 PS) output capability. The DB 606 was installed just behind the aft cockpit wall, near the center of gravity, with an enclosed extension shaft passing through the centerline of the extensively glazed cockpit to drive a large four-blade variable-pitch airscrew in the nose. An evaporative cooling system was used on the V1, with the remaining prototypes receiving a semi-retractable radiator directly below the engine to augment cooling during take-off and climb. Only eight prototypes were completed and the aircraft did not see production, mainly because of the shortages of DB 601 "component" engines to construct the {{convert|1500|kg|lb|abbr=on}} "power systems" they formed. The first two prototypes were built as land planes, with retractable landing gear. The third prototype (V3) was constructed as a seaplane with twin floats. This was tested at the Erprobungsstelle Travemünde military seaplane test facility on the Baltic coast, and was scrapped in 1942 at Heinkel's factory airfield in the coastal Rostock-Schmarl community, then known as Marienehe. On 22 November 1937, the fourth prototype (V4) made a world class-record flight in which it recorded an airspeed of 505 km/h (314 mph), with a payload of 1,000 kg (2,205 lb), over a distance of 1,000 km (621 mi). The four remaining prototypes were completed during the spring and early summer of 1938, the V5 and V6 being A-series production prototypes for the reconnaissance model, and the V7 and V8 being B-series production prototypes for the bomber model. These four aircraft were three-seaters with a defensive armament of one {{convert|7.92|mm|in|abbr=on}} MG 15 machine gun in a dorsal position, V7 and V8 having provision for a normal bombload of three 250 kg (551 lb) bombs or maximum bombload of 1,000 kg (2,205 lb). V7 and V8 were sold to Japan in May 1940, and extensively studied; the insights thus gained were used in the design of the Yokosuka R2Y.{{citation needed|date=July 2015}} The remaining prototypes served as engine test-beds, flying with various prototype versions of the DB 606 and DB 610 (twinned DB 605s) and the experimental DB 613 (twinned DB 603). Variants
Propaganda designation of the He 119
Basic version, eight prototypes built.
Specifications (He 119 V6){{aircraft specifications|plane or copter?=plane |jet or prop?=prop |ref=Warplanes of the Third Reich[2] |crew=3 |length main=14.80 m |length alt=48 ft 6½ in |span main=15.90 m |span alt=52 ft 2 in |height main=5.40 m |height alt=17 ft 8½ in |area main=50.02 m² |area alt=538.2 ft² |empty weight main=5,201 kg |empty weight alt=11,464 lb |loaded weight main=7,581 kg |loaded weight alt=16,678 lb |max takeoff weight main= |max takeoff weight alt= |engine (prop)=Daimler-Benz DB 606A-2, |type of prop=twenty-four-cylinder liquid-cooled coupled engine |number of props=1 |power main=1,753 kW |power alt=2,350 hp |max speed main=591 km/h |max speed alt=319 knots, 367 mph |max speed more=at 4,500 m (14,765 ft) |cruise speed main=510 km/h |cruise speed alt=276 knots, 317 mph |cruise speed more=at 4,500 m (14,765 ft) (60% power) |range main=3,123 km |range alt=1,687 nmi, 1,940 mi |range more=at 6,000 m (19,685 ft) |ceiling main=8,500 m |ceiling alt=27,890 ft |climb rate main= |climb rate alt= |loading main= |loading alt= |power/mass main= |power/mass alt= |more performance=*Climb to 2,000 m (6,560 ft): 3.1 min
|guns=1 × 7.9 mm (.312 in) MG 15 machine gun in dorsal position |bombs= }} See also{{aircontent||related= |similar aircraft=
|lists=
|see also= }} References{{commons category}}1. ^Heinkel He 519 - Project 2. ^Green 1971, p. 331. Sources
9 : German experimental aircraft 1930–1939|German military reconnaissance aircraft 1930–1939|Abandoned military aircraft projects of Germany|Heinkel aircraft|Mid-engined aircraft|Inverted gull-wing aircraft|Low-wing aircraft|Single-engined tractor aircraft|Aircraft first flown in 1937 |
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