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

High-speed high-temperature efficient fuel pump for aerospace

A technology for aerospace and fuel pumps, applied in pumps, pump components, rotary piston pumps, etc., can solve problems such as increased contact stress of gears, loss of liquid heating power, and inability to discharge to the outlet, and achieves improved meshing transmission efficiency, The effect of reducing volumetric efficiency loss and suppressing flow pulsation

Pending Publication Date: 2022-04-12
浙江环誉泵业科技有限公司
View PDF0 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] The traditional oil pump uses a spur gear pump. The disadvantage is that the contact line of the spur gear is parallel to the axis, and the gear teeth enter and separate at the same time during operation, which causes problems such as large flow pulsation, large vibration impact, and high noise of the pump. It will be more obvious at high speed; at the same time, during the working process of the gear pump, part of the liquid between the two meshing gears is trapped and cannot be discharged to the outlet cavity, resulting in trapped oil, which makes the shaft and bearing bear a huge load. The pulsating load will greatly reduce the life of the bearing, and it will also increase the contact stress of the gear, increase the wear of the gear, and cause the gear to vibrate during operation, generate noise, heat the liquid, and increase power loss.

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
  • High-speed high-temperature efficient fuel pump for aerospace
  • High-speed high-temperature efficient fuel pump for aerospace
  • High-speed high-temperature efficient fuel pump for aerospace

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0028] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.

[0029] In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer" etc. The indicated orientation or positional relationship is based on the orientation or positional relationship shown in the drawings, and is only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the referred device or element must have a specific orientation, or in a specific orientation. construction and operation, and therefore cannot be constru...

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 discloses a high-speed, high-temperature and high-efficiency fuel pump for aerospace, and aims to solve the problems of large flow pulsation, large vibration impact, high noise and the like of the pump due to the fact that a straight-tooth gear pump is adopted as a traditional oil pump and gear teeth enter and are separated at the same time when the straight-tooth gear pump works because a contact line of a straight gear is parallel to an axis. Meanwhile, due to the oil trapping phenomenon of the gear pump, a shaft and a bearing need to bear huge pulsating loads, the service life of the bearing is greatly shortened, the contact stress of the gear is increased, abrasion of the gear is increased, and vibration, noise, liquid heating, power loss increase and the like are caused when the gear works. According to the invention, the problem of noise is effectively controlled by adopting a proper meshing angle, adjusting an unloading groove, additionally arranging an oil suction extension groove, a deviation floating bearing, a tooth-shaped modification pump cover and the like, the problem of oil trapping is solved, the overall working efficiency is improved, and the service life of the fuel pump is also prolonged.

Description

technical field [0001] The invention relates to the technical field of engine fuel pumps, in particular to a high-speed, high-temperature and high-efficiency fuel pump for aerospace. Background technique [0002] The traditional oil pump uses a spur gear pump, the disadvantage of which is that the contact line of the spur gear is parallel to the axis, and the gear teeth enter and separate at the same time during operation, which causes problems such as large flow pulsation, large vibration shock and high noise of the pump. It will be more obvious at high speed; at the same time, during the working process of the gear pump, part of the liquid between the two meshing gears is trapped and cannot be discharged to the outlet cavity, resulting in trapped oil, which makes the shaft and bearing bear a huge The pulsating load greatly reduces the life of the bearing, and also increases the contact stress of the gear, increases the wear of the gear, and causes vibration, noise, liquid ...

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
Patent Type & Authority Applications(China)
IPC IPC(8): F04C2/14F04C2/18F04C15/00F02C7/22
Inventor 高永操李传仓杨光武何钰琳韩俊浩白坤
Owner 浙江环誉泵业科技有限公司