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Super Constellation : ウィキペディア英語版
Lockheed L-1049 Super Constellation

The Lockheed L-1049 Super Constellation is an American aircraft, a member of the Lockheed Constellation aircraft line. The L-1049 was Lockheed's response to the successful Douglas DC-6 airliner, first flying in 1950. The aircraft was also produced for both the United States Navy and Air Force as transport and AWACS aircraft.
==Development==
Since 1943 Lockheed had been planning a stretched variant of the Constellation family. The first was an L-049 with a fuselage lengthened by 13 feet (4m). The next was an L-749 lengthened by 18 feet (5.5m). Neither was built due to the lack of suitable engines on the civilian market.
The idea was relaunched after a rival aircraft appeared, when Douglas launched a stretched version of its DC-6 airliner as a cargo transport, designated DC-6A, for both military and civilian operators. Douglas was soon to launch a passenger version (the DC-6B) of this new aircraft. The DC-6B could carry 23 more passengers than Lockheed's current production L-749 Constellation.
In 1950 Lockheed had repurchased the XC-69 Constellation prototype from the Hughes Tool Company. The XC-69 however, was equipped with four Pratt & Whitney R-2800 radial engines instead of the Wright R-3350s used on production models (Lockheed had made that installation on the prototype to test the R-2800 as a possible engine option for the L-049). Lockheed lengthened XC-69 by 18 feet (5.5m), to become the basis for the L-1049 Super Constellation. The aircraft first flew later that year still fitted with R-2800 engines, then was refitted with R-3350 956-C18CA-1 engines with jet stacks for slightly increased thrust. Later modifications included strengthened landing gear and larger vertical stabilizers. Eastern Air Lines ordered 10 aircraft, while Trans World Airlines (TWA) followed with an order for 14. The L-1049 had some 550 improvements and modifications compared to the L-749, including greater fuel capacity, rectangular windows, larger cockpit windshields and improved heating and pressurization.
In 1953 R-3350 Turbo-compounds were made available for civil use. Lockheed incorporated them into the L-1049C, which first flew on February 17 of that year. The R-3350-972-TC18DA-1 turbo-compound engines on the L-1049C had a new turbine system, the Power Recovery Turbines (PRT). Each engine's exhaust gas flowed through three turbines, increasing power by 550 hp (410 kW). One drawback of the PRT was the visible flame from the exhaust pipes; this was resolved by placing armor plating 2 in (5.08 cm) thick under the stack. The L-1049C had a higher cruising speed and climb rate. Although still lacking the range of the DC-6B, the L-1049C was now identical in performance to the Douglas and could carry a larger payload. The wings of the new model were strengthened, cabin soundproofing was increased, and the landing gear retraction system was improved. A new series of interior layouts was offered for the new model; "Siesta" (47 Passengers with increased luxury), "Intercontinental" (54 - 60 Passengers) and "Inter-urban" (105 Passengers). Each of these new layouts included reading lights at each seat. 48 L-1049Cs were built, being used by Eastern, TWA, Air France, KLM, Trans-Canada Air Lines, QANTAS, Air India, Pakistan International Airlines, Avianca, Iberia, Línea Aeropostal Venezolana and Cubana de Aviación.
A freighter version, the L-1049D, first flew in August 1954. It had two cargo doors on the left side and a reinforced magnesium floor as used on the R7V-1 military variant of the L-1049B. The L-1049D could carry a 36,916 lb (16,745 kg) payload and had a volume of 5,579 ft³ (158 m³). At the time of its first flight, the L-1049D was the largest civil cargo aircraft. In the end four were produced, all delivered to Seaboard & Western Airlines. Two of the four L-1049D aircraft were later converted to L-1049H standards.
The L-1049E was more successful; 28 were delivered to eight airlines. Similar to the L-1049C, the L-1049E was able to carry the same load as the L-1049D. The L-1049C and L-1049E could not usually fly Europe to New York nonstop against the wind. Lockheed thought of fitting a new variant based on the L-1049E with more powerful engines, but the project was cancelled. A different variant surfaced: using the L-1049C as a base, R-3350-972-TC18DA-3 turbo-compound engines were fitted. The aircraft could carry 71 to 95 passengers at a speed of 331 mph (533 km/h). Wingtip tanks of 1,037 gallon (3,925 L) total capacity were incorporated, increasing range by 1,110 miles (1,770 km). A new Bendix or RCA weather radar could be installed in the nose, which changed the nosecone shape. New Hamilton Standard or Curtiss Electric propellers were offered. This new version of the L-1049 with over 100 modifications from the L-1049C was unveiled as the L-1049G (the L-1049F being already used for the military C-121C). Over 100 L-1049G aircraft were ordered by sixteen airlines. The L-1049G flew on December 17, 1954 and entered service with TWA and Northwest in 1955.〔The 2/55 OAG shows a daily NW 1049G SEA-ANC and back starting on 15 Feb; TWA started 1049G flights on 1 April.〕 The nickname "Super G" (first used by TWA) was later adopted for the L-1049G.
The L-1049H flew on November 20, 1956. Called "Super H" and "Husky", the L-1049H was a convertible passenger/freight aircraft, mating a C-121C-based fuselage with L-1049G components. The cargo hold had a volume of 565 ft³ (16 m³) when including the lower hold. The aircraft could carry up to 120 people with seats, luggage lockers and toilets all available along with the option of decorating the walls of the aircraft. When not in use, the luggage lockers and seats could be stowed in the lower hold. The aircraft entered service with QANTAS a month later. Some L-1049G and H aircraft in later production were fitted with the TC-18EA series engines used on the L-1649 Starliner. A final variant was planned in 1957, known as the L-1049J. Powered by four R-3350-988-TC-18EA-6 engines, the L-1049J was based on the L-1049H with the wings of the R7V-2 Constellation and an extra fuselage-mounted fuel tank.

抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
ウィキペディアで「Lockheed L-1049 Super Constellation」の詳細全文を読む



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