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Micro-miniature turbine engine shaft sleeve

A turbine engine, micro-miniature technology, applied in the direction of engine components, engine lubrication, machine/engine, etc., can solve the problems of increasing the use and maintenance cost of micro-turbine engines, affecting the service life of the engine, and insufficient cooling of bearing components, etc., to achieve simplification The effect of complex oil circuit design, increased life, and reduced maintenance costs

Pending Publication Date: 2018-07-10
NORTHWESTERN POLYTECHNICAL UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The traditional micro turbine engine lubricating oil system only uses a small part of the fuel-lubricating oil mixture to cool and lubricate the bearing parts through the bushing. During the start-up and cooling process, it is easy to cause insufficient cooling of the bearing parts, resulting in overheating damage or even carbonization of the bearing. Seriously affects the service life of the engine, and also increases the maintenance cost of the micro turbine engine

Method used

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  • Micro-miniature turbine engine shaft sleeve
  • Micro-miniature turbine engine shaft sleeve
  • Micro-miniature turbine engine shaft sleeve

Examples

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Embodiment Construction

[0021] The principles and features of the present invention are described below in conjunction with the accompanying drawings, and the examples given are only used to explain the present invention, and are not intended to limit the scope of the present invention.

[0022] Such as Figures 1 to 7 As shown, the bushing of a micro turbine engine is characterized in that it includes a bushing housing 5 installed on the shaft 6 through a bearing 12, the front end of the bushing housing 5 is connected with the diffuser 1, and the bushing shell The shaft 6 outside the front end bearing 12 of the body 5 is provided with a front carbon ring 9, the front carbon ring 9 is installed on the sleeve 4 of the shaft 6 through the front baffle plate 2 and the front carbon ring outer cover 3, and the rear end of the shaft sleeve housing 5 is connected to the The turbine guide 14 is connected, and the shaft 6 outside the rear end bearing 12 of the shaft sleeve housing 5 is provided with a rear ca...

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Abstract

The invention relates to the technical field of manufacturing of micro-miniature turbine engines, in particular to a micro-miniature turbine engine shaft sleeve. The shaft sleeve is characterized by comprising a shaft sleeve shell installed on a shaft through bearings, the front end of the shaft sleeve shell is connected to a diffuser, a front carbon ring is arranged on the position, on the exteriors of the front end bearings of the shaft sleeve shell, of the shaft, and the front carbon ring is installed on a sleeve of the shaft through a front baffle and a front carbon ring outer sleeve; andthe rear end of the shaft sleeve shell is connected to a turbine guider, a rear carbon ring is arranged on the position, on the exterior of the rear end bearings of the shaft sleeve shell, of the shaft, the rear carbon ring is installed on the shaft through a rear baffle and a rear carbon ring outer sleeve, and fuel nozzles and an oil inlet are further formed in the shaft sleeve shell. According to the micro-miniature turbine engine shaft sleeve, a mechanical sealing shaft sleeve design method is adopted, so that a bearing part is cooled and lubricated to the maximum degree, the requirement ofthe engine on the bearings is reduced, the service life of the bearings is prolonged, and maintenance cost of the engine is reduced; and the novel fuel nozzles are adopted, the design of a complex oil way of a fuel and lubricating oil system is simplified, and replaceability of the nozzles is improved.

Description

technical field [0001] The invention relates to the technical field of micro turbine engine manufacturing, in particular to a micro turbine engine shaft sleeve. Background technique [0002] With the opening of domestic low-altitude areas in recent years, various types of aircraft have developed rapidly, and at the same time, engines as the power source of aircraft have also been fully developed. At present, consumer-grade aircraft mainly use battery-driven motors as power sources, while industrial-grade aircraft, large-scale aircraft models, general aviation / unmanned aerial vehicles, etc. mainly use micro-turbine engines as power devices, mainly including micro-turbojet engines and micro-miniature turbofan engines And micro-turbine engines such as micro-turboprop engines. The shaft sleeve is one of the main components of the micro-turbine engine. It mainly works in a severe working condition of high temperature and high pressure. At the same time, the bearing components in...

Claims

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Application Information

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IPC IPC(8): F02C7/00F02C7/06F02C7/28F02C7/22F01D25/12
CPCF01D25/125F02C7/00F02C7/06F02C7/22F02C7/28
Inventor 陈玉春赵博博黄新春李夏鑫
Owner NORTHWESTERN POLYTECHNICAL UNIV
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