Aerodynamic engine electronically controlled throttle system
An aerodynamic and engine technology, which is applied to the layout of engine components, machines/engines, power plant control mechanisms, etc., can solve the problems of low utilization rate of compressed air and low adjustment accuracy
Active Publication Date: 2015-10-28
咸宁祥天空气能电力有限公司
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Problems solved by technology
[0008]Based on the above problems, the present invention provides an electronically controlled throttle system for aerodynamic engines, which aims to solve the problems of low adjustment accuracy and low utilization rate of compressed air, etc. So as to achieve economical and efficient electronically controlled throttle system
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[0030] The following description is merely exemplary in nature and not intended to limit the disclosure, application or use. It should be understood that throughout the drawings, corresponding reference numerals indicate like or corresponding parts and features.
[0031] now refer to figure 1 , figure 1 A schematic structural diagram of an electronically controlled throttle system for an aerodynamic engine according to the present invention is described (thick lines are pipeline lines, and thin lines are circuit connection lines). The electronic control throttle system of the aerodynamic engine comprises: an air tank group 1, an accelerator actuator 5, an accelerator pedal 9, a lever 10, and an accelerator cable 11; when the accelerator pedal 9 is stepped on, the lever 10 under the accelerator pedal 9 affects the accelerator cable 11, The throttle cable 11 drives the travel switch slider 5-4 in the throttle actuator 5 to rotate counterclockwise from the horizontal direction,...
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The invention relates to an electronic control accelerator system of an aerodynamic generator. An accelerator pedal is stepped down, a lever under the accelerator pedal drives an accelerator draw wire which drives a position switch slider to rotate counterclockwise, an on limit travel switch is switched on, a small direct-current motor connected with the limit travel switch coaxially is started to start a coaxially connected high-pressure ball valve, and high-pressure air in an air tank group is discharged to be used by the engine and other devices; when the accelerator pedal is released slowly, the accelerator draw wire is loosened, the travel switch slider rotates clockwise, and the motor stops operating; and when a driver releases the accelerator completely, the accelerator pedal is uplifted under the inertia, the travel switch slider touches an off limit travel switch, the motor operates in an opposite direction, the high-pressure ball valve is closed, the air tank group stops supplying air for the engine and the other devices, and the motor stops operating. The system further comprises a circuit module, a storage battery in the system charges a power supply and is communicated with an accelerator control unit, and the control unit outputs power to be used by the motor and the travel switches.
Description
technical field [0001] The invention relates to an accelerator system, in particular to an electronically controlled accelerator system for an aerodynamic engine. Background technique [0002] Engines are widely used in all walks of life. In modern transportation tools such as automobiles and ships, piston-type internal combustion engines that use fuel as a power source are generally used. On the one hand, this kind of engine using fuel oil as the power source pollutes the environment due to insufficient fuel combustion, so that the discharged gas contains a large amount of harmful substances and pollutes the environment. The shortage makes the development and utilization of fuel engines more and more restricted. Therefore, developing new, clean, non-polluting alternative energy sources, or reducing fuel consumption and emissions as much as possible has become an urgent problem in the development of engines, and aerodynamic engines using compressed air as a power source jus...
Claims
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IPC IPC(8): B60K26/04F01B25/02
Inventor 周登荣周剑
Owner 咸宁祥天空气能电力有限公司