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Energy conversion device based on fluid volume change and rotor engine

An energy conversion device and volume change technology, which can be used in liquid fuel engines, rotary piston engines, rotary or oscillating piston engines, etc., and can solve the problems of difficulty in improving the sealing effect, low speed, large vibration and energy loss, etc.

Inactive Publication Date: 2019-10-08
李松
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] Defects: poor sealing, low conversion efficiency, complex structure
[0006] Defects: poor sealing, low conversion efficiency, large vibration
[0008] Defects: There is sliding friction between the rotary vane, the rotor and the pump chamber. The rotary vane not only performs linear reciprocating motion, but also rotates eccentrically. The sealing performance is not high, the speed is not high, and the wear, energy consumption and vibration are relatively large.
[0010] Defects: poor sealing, poor dynamic balance performance, high wear, high vibration and noise, low speed, low energy efficiency
[0012] Defects: processing and assembly are difficult, the shape of the screw and the dynamic meshing method determine that the sealing effect is difficult to improve, the gap leakage is large, the cost is high, the volume is large, the displacement is small, and the vibration is large in some cases
[0014] Defects: The shape of the rotor and the way of meshing make it difficult to improve the sealing effect, the gap leakage is large, the energy efficiency is not high, and the processing is difficult
[0016] Defects: poor sealing, large gap leakage, low compression ratio, eccentric movement of the moving plate limits the speed increase, and has vibration, and the volume flow is low
[0018] Disadvantages: lower compression ratio affects fuel combustion efficiency, loud noise
[0020] Disadvantages: The conversion efficiency of the turbine to gas kinetic energy is low, and it is easy to cause turbulence to the jet
[0022] Defects: The three tops of the triangular rotor and the stator wall are always in the sliding friction of constantly changing positions, and the wear is large, which affects the sealing effect of the fluid, high fuel consumption and high emissions; low compression ratio, low fuel combustion efficiency and low emissions High; the shape of the long and narrow combustion chamber also affects the speed of flame propagation, which further affects the combustion efficiency of fuel
The rotor rotates eccentrically in the stator relative to the stator. While revolving around the center of the output shaft, the rotor also rotates around the center of the protruding shaft on the output shaft. Therefore, it is difficult to provide good lubrication and cooling for the rotor, and the vibration and energy loss are large.
The compression ratio of the engine is low, so that the combustion cannot be sufficient, the combustion efficiency is low, and the emission is difficult to meet the standard. The shape of the long and narrow combustion chamber also affects the speed of flame propagation, which further affects the combustion efficiency of the fuel. Moreover, the low compression ratio leads to the use of ignition instead of The compression ignition method is adopted, that is, gasoline can only be used as fuel and diesel oil cannot be used

Method used

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  • Energy conversion device based on fluid volume change and rotor engine

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0087] Such as figure 1 and figure 2 As shown, the energy conversion device based on fluid volume change includes a stator 1 and a rotor 6 located in the inner cavity of the stator 1. The rotor 6 is rotatably supported at both ends of the stator 1 by a rotor shaft 7. The rotor 6 is a cylinder Body shape, which rotates coaxially with the stator 1 cavity in the stator 1 cavity, and on the cylindrical cavity wall of the stator 1 that rotates with the rotor 6, there are grooves 9 along the circumference, so that the stator 1 and A closed working chamber 12 is formed between the rotors 6. The inner contour line of the cross section of the working chamber 12 is a circle with the axis center of the rotor 6 as the center and the radius of the rotor 6 as the radius. The outer contour line of the cross section of the working chamber 12 is determined by the first One arc line 33, the second arc line 18, the third arc line 21, the fourth arc line 24, the fifth arc line 27, the sixth arc...

Embodiment 2

[0117] Such as figure 1 and image 3 As shown, the rotary engine (compression ignition type) based on fluid volume change includes a stator 1 and a rotor 6 located in the inner cavity of the stator 1, and the rotor 6 is rotatably supported at both ends of the stator 1 through a rotor shaft 7. The rotor 6 is in the shape of a cylinder, which rotates coaxially with the inner cavity of the stator 1 and cooperates with the inner cavity of the stator 1. On the wall of the cylindrical inner cavity of the stator 1 which rotates with the rotor 6, a groove 9 is opened along the circumferential direction, so that A closed working chamber 12 is formed between the stator 1 and the rotor 6. The inner contour line of the cross section of the working chamber 12 is a circle with the axis center of the rotor 6 as the center and the radius of the rotor 6 as the radius. The outer contour line of the cross section of the working chamber 12 is By the first arc line 33, the second arc line 18, the...

Embodiment 3

[0148] Such as figure 1 and image 3 As shown, the rotary engine (spark plug ignition type) based on fluid volume change includes a stator 1 and a rotor 6 located in the inner cavity of the stator 1, and the rotor 6 is rotatably supported at both ends of the stator 1 through a rotor shaft 7, said The rotor 6 is in the shape of a cylinder, which rotates coaxially with the inner cavity of the stator 1 and cooperates with the inner cavity of the stator 1. On the wall of the cylindrical inner cavity of the stator 1 which rotates with the rotor 6, a groove 9 is opened along the circumferential direction, so that A closed working chamber 12 is formed between the stator 1 and the rotor 6. The inner contour line of the cross section of the working chamber 12 is a circle with the axis center of the rotor 6 as the center and the radius of the rotor 6 as the radius. The outer contour line of the cross section of the working chamber 12 is By the first arc line 33, the second arc line 18,...

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Abstract

The invention relates to an energy conversion device based on fluid volume change and a rotor engine. The energy conversion device comprises a stator and a rotor, wherein a closed working cavity is formed between the stator and the rotor, and six planetary rollers are uniformly arranged on the rotor in the circumferential direction; the outer contour line of the cross section of the working cavityis a closed line formed by connecting a first arc line, a second arc line, a third arc line, a fourth arc line, a fifth arc line, a sixth arc line, a first curve, a second curve, a third curve, a fifth curve and a sixth arc line, a seventh curve, an eighth curve, a ninth curve, a tenth curve, an eleventh curve and a twelfth curve, the inner contour line of the cross section of the working cavityis a circle taking the axis of the rotor as a circle center and the radius of the rotor as a radius, and the contour line of the cross section of each planetary roller is a closed line formed by connecting a seventh arc line, an eighth arc line, a ninth arc line, a tenth arc line, an eleventh arc line, a twelfth arc line, a thirteenth curve. a fourteenth curve, a fifteenth curve, a sixteenth curve, a seventeenth curve and an eighteenth curve. According to the energy conversion device based on fluid volume change and the rotor engine, the requirements of variable volume, reliable sealing and coaxial rotation of the rotor relative to the inner cavity of the stator can be met at the same time, so that the performance of the energy conversion device and the performance of the engine can be improved.

Description

technical field [0001] The invention relates to an energy conversion device and a rotary engine based on fluid volume changes, which can convert fluid pressure potential energy into drive torque, or convert input torque into fluid kinetic energy or potential energy through fluid volume changes, and are mainly used in internal combustion engines, steam turbines, Water turbines, compressors, air motors, hydraulic motors, fluid pumps, vacuum pumps and other fields. Background technique [0002] At present, many fluid energy conversion devices realize energy conversion or fluid transportation through the change of fluid volume, and the change of fluid volume is mostly realized by the relative rotational motion between the stator and the rotor, such as rotary engines, steam turbines, water turbines , compressors, air motors, hydraulic motors, hydraulic pumps, vacuum pumps, etc. There are many types of mechanical structures for these devices, including blade type, impeller type, ...

Claims

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Application Information

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IPC IPC(8): F02B53/00F02B55/02F02B55/08F02B53/02F02B53/04F02M61/14F02B53/12F01C1/113F03B5/00F03C2/08F04C2/113F04C18/113F04C25/02
CPCF01C1/113F02B53/00F02B53/02F02B53/04F02B53/12F02B55/02F02B55/08F02M61/14F03B5/00F03C2/08F04C2/113F04C18/113F04C25/02Y02E10/20Y02T10/12
Inventor 李松
Owner 李松