Tooling and method for removing burrs from aero-engine fuel injectors using abrasive flow technology

A technology for aero-engines and fuel injectors, applied in the aerospace field, can solve problems such as abrasive particle flow cannot remove burrs well, achieve the effects of improving efficiency and consistency, improving surface finish, and reducing damage

Active Publication Date: 2020-11-20
CHANGAN UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

When the current fixture designed for this type of injector is in use, the abrasive flow is quickly ejected from the nozzle hole of the injector and the outlet hole of the fixture under the action of pressure, and the abrasive flow cannot remove the dust at the lower end of the injection port Burrs on the edge of the conical surface of the conical orifice

Method used

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  • Tooling and method for removing burrs from aero-engine fuel injectors using abrasive flow technology
  • Tooling and method for removing burrs from aero-engine fuel injectors using abrasive flow technology
  • Tooling and method for removing burrs from aero-engine fuel injectors using abrasive flow technology

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Embodiment

[0050] Such as Figure 6(a) ~ Figure 6(c) , Figure 7(a) ~ Figure 7(c) as well as Figure 8 As shown, in this embodiment, the tooling for removing burrs from aero-engine fuel injectors using the abrasive flow process adopts an upper and lower two-part structure, which are the upper fixture A and the lower fixture B respectively, wherein both the upper fixture A and the lower fixture B have two positioning The pin hole, the upper fixture A is made of nylon material, which is in soft contact with the upper surface of the fuel injector 7 to be processed, the cylinder boss 3 at the lower end of the upper fixture A can be inserted into the oil inlet at the upper end of the fuel injector 7, and the cylinder convex There is a seamless fit between platform 3 and the oil inlet of the fuel injector. The height of the cylindrical boss 3 is low. The cylindrical boss 3 can prevent the abrasive from flowing out in the gap between the fixture and the upper end of the fuel injector in order ...

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Abstract

The invention discloses a tooling and a method for removing burrs from an aeroengine fuel injector by using an abrasive flow process. The tooling includes an upper clamp and a lower clamp for clamping the fuel injector. The upper clamp is set at a position opposite to the inlet of the fuel injector. There is a central hole for the abrasive grain flow to enter the inlet of the fuel injector; the lower fixture is provided with a conical diversion structure at the position opposite to the conical surface of the conical nozzle hole of the fuel injector, and the taper of the conical diversion structure is consistent with the conical shape The conical surface of the nozzle hole has the same taper, the upper part of the conical diversion structure extends into the outlet of the nozzle, and there is a gap between the conical diversion structure and the conical surface of the nozzle hole for the outflow of abrasive particles; There is a discharge hole, and the discharge hole is used for the abrasive grain flow flowing out of the outlet of the fuel injector to flow out of the lower fixture. The invention can remove the burr of the spray hole of the fuel injection nozzle of the aero-engine with high efficiency and high consistency, and overcomes the defects caused by the traditional processing technology.

Description

technical field [0001] The invention belongs to the field of aerospace technology, and in particular relates to a tool and a method for removing burrs from an aeroengine fuel injection nozzle by using an abrasive particle flow process. Background technique [0002] At present, the micro-holes of aero-engine injector parts are mostly processed by mechanical processing. The advantage is high processing efficiency, but the disadvantage is that it is easy to cause high roughness of the nozzle hole and a large number of burrs on the surface of the nozzle hole. At present, sandpaper, grinding head, etc. are mainly used as auxiliary tools for deburring nozzle holes of aero-engines, and manual deburring methods are used. Manual deburring is inefficient and poor in consistency, and there are often phenomena such as unclean deburring. Moreover, the through-hole diameter of the nozzle is small, and it is difficult for general tools to enter, and some burrs are difficult to completely r...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B24C1/08B24C3/00B24C5/04
CPCB24C1/083B24C3/00B24C5/04
Inventor 陈昊姚禹轩赵伟
Owner CHANGAN UNIV
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