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Небесная энциклопедия

Космические корабли и станции, автоматические КА и методы их проектирования, бортовые комплексы управления, системы и средства жизнеобеспечения, особенности технологии производства ракетно-космических систем

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Мониторинг СМИ

Мониторинг СМИ и социальных сетей. Сканирование интернета, новостных сайтов, специализированных контентных площадок на базе мессенджеров. Гибкие настройки фильтров и первоначальных источников.

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Применить Всего найдено 5. Отображено 5.
13-07-1955 дата публикации

Improvements in and relating to fuel-reaction-chambers

Номер: GB0000733385A
Автор: STRANG IAN GOURLAY, BELL RICHARD ALLAN
Принадлежит:

... 733,385. Generating combustion products under pressure. BRITISH THOMSONHOUSTON CO., Ltd. Feb. 17, 1954 [Feb. 17, 1953], No. 4416/53. Class 51 (1). In an arrangement for the production of a flow of working fluid by decomposition of a monofuel comprising a main reaction chamber 1, in which the greater part of the fuel injected at 4, is decomposed to form a flow of fluid through an outlet 5, and an auxiliary reaction chamber 2 in which combustion of a separate supply of monofuel takes place to produce a flow of heated gas into the main chamber to induce decomposition of the fuel therein, the flow of gas from the auxiliary chamber at 3 passes into the main chamber through shrouding means 6 which projects into the main chamber and in which the gas meets a jet 9 of monofuel, the resulting combustion products flowing out of the shrouding means through an aperture 6c at or near its inner end. In a modification of the arrangement shown, the shrouding 6 is open at its inner end, and the jet 9 is ...

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Номер записи: 1
22-02-1961 дата публикации

Improvements relating to aircraft auxiliary installations

Номер: GB0000861761A
Автор: STONE DENIS, STRANG IAN GOURLAY
Принадлежит:

... 861,761. Auxiliary power installations on aircraft. ASSOCIATED ELECTRICAL INDUSTRIES Ltd. April 4, 1957 [April 4, 1956], No. 10317/56. Drawings to Specification. Class 4. [Also in Group XXVI] An auxiliary power installation for aircraft having a main gas turbine power plant, comprising an auxiliary gas turbine unit provided with a compressor supplying air to a combustion chamber feeding a turbine driving the compressor, the compressor having an air inlet receiving ambient air and provided with means for being supplied with additional compressed air from a bleed on the main power plant, has alternative means of control, one for controlling the fuel supply in accordance with speed and the other for controlling the air supply in accordance with speed and the fuel supply in accordance with the inlet temperature of the auxiliary turbine. At sea level, the auxiliary compressor draws its air supply from the atmosphere and the fuel supply is controlled by a speed governor. At altitude, an air regulating ...

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Номер записи: 2
04-01-1961 дата публикации

Improvements in aircraft auxiliary installations

Номер: GB0000857782A
Автор: STONE DENIS, STRANG IAN GOURLAY
Принадлежит:

... 857,782. Gas-turbine plant. BRITISH THOMSON-HOUSTON CO. Ltd. April 4, 1957 [April 4, 1956], No. 10318/56. Class 110 (3). An auxiliary power installation for aircraft having a main gas-turbine power plant comprises a gas-turbine having a plurality of separate banks of inlet nozzles, an auxiliary compressor driven by the gas-turbine for supplying air from the atmosphere to a combustion chamber connected to one of the banks of the nozzles, means for controlling the fuel supply to this combustion chamber in accordance with the speed of the turbine, means for supplying air bled from the main engine compressor to one or more additional combustion chambers connected to the remaining banks of nozzles, means for controlling the fuel supply to the additional combustion chambers in accordance with the turbine inlet tempera-. ture and pressure control means operated by a speed-sensitive device to control the air supply. to the additional combustion chambers. Air from an auxiliary compressor 1 is fed ...

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Номер записи: 3
06-06-1956 дата публикации

Improvements in fuel supply systems for reaction chambers

Номер: GB0000749921A
Автор: WELCH DOUGLAS FRANCIS, RANDALL KENNETH BARRINGTON, STRANG IAN GOURLAY
Принадлежит:

... 749,921. Generating combustion products under pressure. BRITISH-THOMSONHOUSTON CO., Ltd. Oct. 22, 1954 [Oct. 22, 1953], No. 29230/53. Class 51(1). An apparatus for producing a flow of gaseous working fluid, which may be supplied for example to a turbo-starter of a prime mover, comprises an auxiliary reaction chamber 2 and a main reaction' chamber 1, hot gases produced by decomposition of a monofuel within the auxiliary chamber passing into the main chamber. The flow of hot gases is so directed upon admission to the main chamber as to impinge substantially directly upon a jet of monofuel injected into the main chamber whereby atomisation of the monofuel is effected. The hot gases issue into the main chamber 1 through a nozzle 5 which is disposed opposite the nozzle 6 through which the monofuel is injected. The gases from the main chamber pass through an outlet nozzle 7. The auxiliary chamber has a monofuel supply at 3 and a heater 4. The hot gases from the auxiliary chamber may alternatively ...

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Номер записи: 4
06-06-1956 дата публикации

Improvements in reaction chambers

Номер: GB0000749920A
Автор: WELCH DOUGLAS FRANCIS, RANDALL KENNETH BARRINGTON, STRANG IAN GOURLAY
Принадлежит:

... 749,920. Generating combustion products under pressure. BRITISH THOMSONHOUSTON CO., Ltd. Oct. 22, 1954 [Oct. 22, 1953], No. 29229/53. Class 51(1). An apparatus for producing a flow of gaseous working fluid which for example may be supplied to a turbo-starter for a prime mover, e.g. a gas turbine engine, comprises an auxiliary reaction chamber 10 in which heated gases are produced by decomposition of a monofuel, the gases passing through a conduit 34 to a main reaction chamber 11 which is divided into two compartments by a perforated screen 37. The compartment into which the gases from the auxiliary chamber are led also receives a separate supply of monofuel through the orifice 16. The screen 37 becomes heated by the gases produced by decomposition of monofuel in the auxiliary chamber, and the monofuel supplied through the orifice 16 percolates through the heated screen and its decomposition is thereby promoted. The gases pass from the second compartment through two outlets 15 leading to ...

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Номер записи: 5