Rotary ramjet shock wave supercharging gas turbine engine
The invention provides a rotary ramjet shock wave supercharging gas turbine engine, and belongs to the technical field of turbine engines, the rotary ramjet shock wave supercharging gas turbine engine comprises an outer casing and an inner casing, an outer duct is formed between the inner casing and...
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creator | CHEN XUAN SHAO CHUNLEI XIE JIAN QIU BINGQING LI PING YIN YUEQIAN JIN HAILIANG SHI SHANGUANG |
description | The invention provides a rotary ramjet shock wave supercharging gas turbine engine, and belongs to the technical field of turbine engines, the rotary ramjet shock wave supercharging gas turbine engine comprises an outer casing and an inner casing, an outer duct is formed between the inner casing and the outer casing, a guide vane is installed in the outer casing, and the guide vane is used for guiding in airflow; a first mechanism is installed in the inner casing and used for pressurizing and heating airflow and doing work. A second mechanism is further arranged on one side of the inner casing and used for conducting secondary pressurization and heating on the airflow. The rotary punching compressor is used for solving the problems that an elastic centrifugal compressor is large in windward area, multiple in multi-stage axial flow compressor parts and low in small-flow efficiency, higher flow and pressure ratio are obtained under the compact size, it is guaranteed that an original engine obtains larger thrust |
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A second mechanism is further arranged on one side of the inner casing and used for conducting secondary pressurization and heating on the airflow. 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A second mechanism is further arranged on one side of the inner casing and used for conducting secondary pressurization and heating on the airflow. 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A second mechanism is further arranged on one side of the inner casing and used for conducting secondary pressurization and heating on the airflow. The rotary punching compressor is used for solving the problems that an elastic centrifugal compressor is large in windward area, multiple in multi-stage axial flow compressor parts and low in small-flow efficiency, higher flow and pressure ratio are obtained under the compact size, it is guaranteed that an original engine obtains larger thrust</abstract><oa>free_for_read</oa></addata></record> |
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language | chi ; eng |
recordid | cdi_epo_espacenet_CN115962065A |
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subjects | BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS |
title | Rotary ramjet shock wave supercharging gas turbine engine |
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