Unlock instant, AI-driven research and patent intelligence for your innovation.

Rotor system and micro gas turbine

A rotor and shaft technology, applied in gas turbine devices, mechanical equipment, engine components, etc., can solve the problems of insufficient rigidity, difficult processing and manufacturing, high processing and manufacturing costs, etc., to improve dynamic performance and stability, and improve pneumatic lubrication. effect, the effect of improving the overall performance

Pending Publication Date: 2020-03-31
刘慕华
View PDF0 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] In the rotor system of the prior art, when the radial bearing and the thrust bearing used are air bearings, it has the following defects: for the radial air bearing, when the stiffness is not enough, it can store air through the eight-character groove, and it can be used at low speeds. Increase the bearing capacity, but it will cause air blockage at high speed. When the air is blocked, due to the high-speed rotation of the shaft, high-frequency vibration will be generated. The blocked air will become an energy absorber, and the temperature will rise rapidly, and can rise to several The high temperature of 1000 degrees will cause the shaft / sleeve to melt, the shaft and the shaft sleeve will be bonded and stuck, and at the same time, it will cause the bearing air to recharge, further blocking the air passage,
[0006] 1. Due to the throttling effect, in order to maintain a high bearing rigidity, it is necessary to reduce the aperture and air film gap of the throttle hole. The smaller aperture and gap are not only very difficult in processing and manufacturing, but also bring higher processing costs. manufacturing cost
[0007] 2. During the high-speed rotation of the bearing, with the increase of the rotor speed, the temperature inside the air film is high, and the orifice is easily oxidized in high-temperature air, resulting in black holes and blockage of air holes
[0008] The small bearing clearance is easy to cause the wear of the rotor and the stator to produce metal shavings, which will cause the blockage of the orifice and reduce the overall reliability of the bearing
[0009] 3. Air bearings are generally installed with rubber rings on the bearing seat to prevent the circumferential rotation of the shaft. However, in the actual application of radial air bearings, when the rotational speed of the rotating shaft reaches about 100,000 revolutions or more, the compressed air film and the rotating shaft The friction between them also increases, and the torque generated by this friction makes the radial air bearing rotate with the shaft more obviously and frequently, and the rubber ring is also easy to wear and damage

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Rotor system and micro gas turbine
  • Rotor system and micro gas turbine
  • Rotor system and micro gas turbine

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0099] In order to better understand the technical solutions of the present invention, the present invention will be further described below in conjunction with specific embodiments and accompanying drawings.

[0100] According to one aspect of the invention, a rotor system is provided.

[0101] Such as figure 1 The rotor system shown includes a rotating shaft 110, the shaft body of the rotating shaft 110 is an integral structure, the rotating shaft 110 is arranged horizontally or vertically, and the rotating shaft 110 is sequentially sleeved with a thrust bearing 100, a first radial bearing 200, a motor 300, a second Radial bearing 400, compressor 500, turbine 600.

[0102] Such as figure 2 The rotor system shown includes a rotating shaft 110, the shaft body of which is an integral structure, the rotating shaft 110 is arranged horizontally or vertically, and the first radial bearing 200, the motor 300, and the second radial bearing 400 are sleeved on the rotating shaft 110...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

No PUM Login to View More

Abstract

The invention provides a rotor system and a micro gas turbine. The rotor system comprises a rotating shaft. The rotating shaft is an integrated structure, the rotating shaft is horizontally or vertically arranged, and the rotating shaft is provided with a motor, a radial bearing, a gas compressor, a thrust bearing and a turbine. The radial bearing is provided with a throttling hole. The throttlinghole is a variable diameter hole. An outer wall throttling orifice of the bearing body is greater than an inner wall throttling orifice. An annular groove is arranged in an inner wall of the bearingin a circumferential direction. The inner wall throttling orifice is partially or integrally intersected with the annular groove, a first air groove is arranged in the thrust bearing, a second air groove is arranged in a circumferential surface of a position where the bearing body is correspondingly installed on the rotating shaft or in the inner wall of the bearing body along the circumferentialdirection, and the thrust bearing and the radial bearing are anti-rotating bearings. The rotor system and the micro gas turbine have an advantage of efficient and stable operation.

Description

technical field [0001] The invention relates to the technical field of rotor dynamics, in particular to a rotor system and a micro gas turbine. Background technique [0002] The micro gas turbine is a newly developed small heat engine, its stand-alone power ranges from 25 to 300kW, and its basic technical features are radial flow impeller machinery and regenerative cycle. A micro gas turbine mainly includes three major components: a compressor, a combustor and a turbine. After the air enters the compressor, it is compressed into high-temperature and high-pressure air, and then supplied to the combustion chamber for mixed combustion with fuel, and the high-temperature and high-pressure gas generated expands in the turbine to perform work. In the rotor system of a micro gas turbine, radial bearings and thrust bearings need to be installed to stably support the rotating shaft in the radial and axial directions. [0003] In the rotor system of the prior art, when the radial be...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
IPC IPC(8): F02C3/04F02C7/06F01D5/06F16C17/04F16C32/06
CPCF01D5/06F02C3/04F02C7/06F16C17/045F16C32/0614F16C32/0692F16C2360/23
Inventor 靳普刘慕华
Owner 刘慕华