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Miniature turbine generator

A micro-turbine and generator technology, which is applied in the direction of engine components, combustion engines, engine lubrication, etc., can solve the problems that cannot meet the requirements of small and micro-turbine generators, the bearing damping value cannot be greatly improved, and the stability of high-speed operation is not good. and other problems to achieve the effect of ensuring long-term stable operation, small footprint, and reduced volume

Active Publication Date: 2016-08-24
罗立峰
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] Due to the limit speed of traditional oil-based bearings, when the shaft speed exceeds the limit speed, the bearing will fail, so it can no longer meet the requirements of small and micro turbine generators
The air bearing has gradually become a hot spot in the industry and academia because of its advantages such as small friction loss, good high temperature stability, high reliability, low vibration, no need for lubricating oil, and no restriction on the size of the rotating shaft. : Chinese patent application CN201310703932.8 discloses an exhaust gas turbine generator, which adopts 2 radial air foil bearings and 1 air foil thrust bearing to overcome the defect that traditional bearings are prone to failure when working at high speed and high temperature. It has the advantages of small friction loss, can work in high temperature environment, and high efficiency of waste gas energy recovery. However, because foil bearings generally use metal foil, there are not only some difficulties in material manufacturing technology and processing technology, but also the damping of the bearing. The value cannot be greatly increased, resulting in insufficient rigidity of the bearing, low critical speed of the bearing, easy instability or even jamming at high-speed operation, poor stability of high-speed operation, and limited increase in speed, which limits industrial applications

Method used

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  • Miniature turbine generator
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Experimental program
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Effect test

Embodiment 1

[0079] Such as figure 1 Shown: a kind of small micro turbine generator provided by this embodiment, comprises turbine 1, cooling fan 2, motor 3, 2 radial bearings 4 and 1 thrust bearing 5, and described turbine 1 comprises turbine 11, turbine Machine casing 12, turbine deflector 13 and turbine deflector casing 14, described cooling fan 2 comprises fan casing 21, and described motor 3 comprises rotor 31, stator 32, inner shaft 33, outer shaft 34 and motor Machine housing 35; the radial bearing 4 is a hybrid dynamic pressure gas radial bearing, including a bearing outer sleeve 41, a bearing inner sleeve 42 and a foil-shaped elastic member 45 arranged between the bearing outer sleeve 41 and the inner sleeve 42; The thrust bearing 5 is a hybrid dynamic pressure gas thrust bearing, comprising two side disks 51 and a middle disk 52 sandwiched between the two side disks, between each side disk 51 and the middle disk 52, a There is a foil-shaped elastic member 53; the rotor 31 is sle...

Embodiment 2

[0095] like Figure 14 As shown, the foil-shaped elastic member 45 described in this embodiment is composed of a corrugated foil 451 and a flat foil 452. The transitional bottom edge 4512 between corrugated arches of the corrugated foil 451 is attached to the flat foil 452 .

[0096] Figure 15 Shown is a schematic structural diagram of the corrugated foil 451 .

Embodiment 3

[0098] like Figure 16 As shown, the foil-type elastic member 45 described in this embodiment consists of two flat foils 452 .

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Abstract

The invention discloses a miniature turbine generator which comprises a turbine, a cooling fan, a motor, two radial bearings and a thrust bearing. The radial bearings are hybrid radial hydrodynamic gas-lubricated bearings, and the thrust bearing is a hybrid thrust hydrodynamic gas-lubricated bearing. The middle part of an inner shaft is sleeved with a rotor, the two radial bearings are arranged on the parts, located at the left and right ends of the rotor, of an outer shaft in a sleeving mode correspondingly, and the thrust bearing is arranged on the part, located at the right end, of the outer shaft in a sleeving mode and located at the outer end of the radial bearing at the right end. The turbine and the cooling fan are arranged at the two ends of the inner shaft correspondingly. The miniature turbine generator can stably operate at an ultrahigh speed in a gas-floating state, and for meeting the same power requirement, the size of the turbine generator can be obviously reduced to achieve miniaturization.

Description

technical field [0001] The invention relates to a small and micro turbine generator, which belongs to the technical field of high-precision machinery. Background technique [0002] In recent years, with the development of distributed power supply and multi-electric technology, the power system has gradually replaced the mechanical systems such as hydraulic pressure and air pressure in traditional aircraft, so that the secondary side power system is distributed in the form of electricity. Electric aircraft has become a new development direction of the times. The power system with small and micro turbine generators as the main body will become an important research direction for the power system of the new generation of multi-electric aircraft. [0003] Due to the limit speed of the traditional oil-based bearing, when the shaft speed exceeds the limit speed, the bearing will fail, so it can no longer meet the requirements of small and micro turbine generators. The air bearin...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F16C32/06F16C33/02H02K5/167H02K9/04
CPCF16C32/0603F16C33/02H02K5/167H02K9/04F04D25/0606F04D25/08F04D29/056F04D29/0563F04D29/403F04D29/601F02C7/06F16C33/04F01D15/10F01D25/16F02B37/10F02B41/10F16C17/026F16C17/08H02K5/161F02B37/00H02K5/163H02K9/06H02K7/18F16C17/024F16C17/042
Inventor 罗立峰
Owner 罗立峰