One-driving multi-power multi-turbine-blade multi-side-air inlet/outlet engine
A kind of engine and multiple technologies, applied in the field of one-drive multi-movement multi-turbine blades and multiple side air inlet/outlet engines, can solve problems such as take-off and landing, flight danger, and inability to land
Inactive Publication Date: 2013-09-18
王军
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But its huge rotor makes it dangerous to take off, land and fly between buildings, and it is impossible to land at the doorstep of ordinary people.
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[0015] Most of the technologies in this engine are mature technologies that are now applied in aviation. Turboshaft engines have been widely used in helicopters, and turbofans can be traced back to the end of World War II. My design is just to use a shaft to connect several turbine blades in series, and then use a turbine engine to provide power, then put them into a circular straight cylinder, separate the turbine blades from each other with a partition, and then In the separated space, an air inlet and an air outlet are opened in the upper half of the front and the lower half of the rear with the turbine blade as the boundary. In this way, a sideways passage for entering and exiting the wind is formed, which is a civilian structure. Adding several side air outlets and a common air passage to a rear combustion chamber on this structure is a military engine.
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The invention discloses a one-driving multi-power multi-turbine-blade multi-side-air inlet / outlet engine. The engine mainly integrates an existing engine technology and mainly aims at achieving the design aim that a turbine engine has distinguished vertical climbing capacity and economic fuel oil dynamic property. The design mainly utilizes the characteristics of a turbofan engine. A turboshaft engine provides power to a public transmission shaft, the transmission shaft is provided with multiple turbine blades, all the devices are put into a straight drum together, a partition plate can separate the turbine blades each other, and a tile bearing for fixing the transmission shaft is arranged at the center position of the partition plate; the partition plate can divide the straight drum into a plurality of independent spaces; and with each turbine blade as a boundary, an air inlet is formed in the upper side of the front part of each turbine blade and allows air to flow into, an air outlet is formed in the lower side of the rear part of each turbine blade, and the air erupts from the air outlet. Multiple synchronization air inlet and multiple synchronization downward jet airflow are utilized to replace a huge rotor wing of an active service helicopter, and the engine has the large vertical climbing property due to the design. The air outlets are designed into a steering form so as to control the advance and retreat and steering of the engine.
Description
technical field [0001] Aeronautical low-altitude rapid vertical take-off and landing aircraft engine Background technique [0002] The current aero-engines are mainly divided into turbofan, turboshaft, turboprop, and turbojet. The turbofan type is mainly used for commercial transportation because of its superior fuel economy and power. The turboshaft type is characterized by a 100% power output and is mainly used for helicopters. The turboprop type is mostly used for trainers. The turbojet type Poor fuel economy but strong power are mainly used for special models such as fighter jets. These means of transportation do not meet the use of ordinary people. [0003] The traffic situation in modern cities is deteriorating day by day. The large increase in private cars and almost everyone's driver's license has led to more and more cars on the road, and the policies introduced to stimulate the economy have led to an explosive increase in the number of cars. On the contrary, roa...
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IPC IPC(8): B64C39/00B64D27/02
Inventor 王军
Owner 王军