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A device for controlling incoming flow parameters of channel-type components in an ice wind tunnel

A technology for controlling channels and ice wind tunnels, which is applied in the testing of machines/structural components, measuring devices, and engine testing. It can solve problems such as size mismatch and achieve the effect of ensuring accuracy and avoiding deviations in results

Active Publication Date: 2021-05-25
AECC SHENYANG ENGINE RES INST
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  • Abstract
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  • Claims
  • Application Information

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Problems solved by technology

[0008] In order to solve the above problems, this application provides a device for controlling the incoming flow parameters of channel-type components in the ice wind tunnel. Aiming at the problem that the size of the channel-type components does not match the size of the test section of the ice wind tunnel, the components are built into the test section And set up a special flow area control device to control the flow conditions of the channel-type components in the way of gas bypass overflow, so as to meet the parameters of icing and anti-icing tests

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  • A device for controlling incoming flow parameters of channel-type components in an ice wind tunnel
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  • A device for controlling incoming flow parameters of channel-type components in an ice wind tunnel

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[0025] In order to make the objectives, technical solutions and advantages of the implementation of the application clearer, the technical solutions in the implementation modes of the application will be described in more detail below with reference to the drawings in the implementation modes of the application. In the drawings, the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The described embodiments are some, but not all, embodiments of the present application. The embodiments described below by referring to the figures are exemplary and are intended to explain the present application, and should not be construed as limiting the present application. Based on the implementation manners in this application, all other implementation manners obtained by persons of ordinary skill in the art without creative efforts fall within the scope of protection of this application. Embodiments of the pr...

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Abstract

This application belongs to the field of gas turbine engine anti -ice test technology, involving a device that controls the channel -type components in the ice wind cave to flow parameters.This device mainly includes an overflow device installed on the front end of the channel -type component. The overflow device includes a cylinder and ring component. The cylinder is installed on the intake port of the channel -type component.The inner wall of the rectifier, the ring component is installed on the outer wall of the cylinder, and the inlet of the inlet near the channel -type component is located.The flow speed of the type component.This application adopts the flow device control channel type component to flow the speed of flow speed, which can enable the ice -winded cave to be frozen and anti -ice test of small -sized channel components., Ensure the accuracy of the test results.

Description

technical field [0001] The application belongs to the technical field of anti-icing tests of gas turbine engines, and in particular relates to a device for controlling incoming flow parameters of channel-type components in an ice wind tunnel. Background technique [0002] The icing and anti-icing effect tests of gas turbine engine imported parts are one of the important verification activities in the engine design process. The anti-icing test of components should be carried out on ice wind tunnel equipment. There are generally two types of ice wind tunnels: free jet type and closed loop type. For the closed-circulation ice wind tunnel, when conducting the anti-icing test of channel-type components (for example, air intake casing), in order to ensure the incoming flow velocity, flow rate and surface water impact characteristics of the channel-type components, ice is usually The wind tunnel test section is directly connected to the channel-type component, that is, the mainstr...

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01M9/04G01M9/06G01M15/02
CPCG01M9/04G01M9/065G01M15/02
Inventor 刘国朝曹智顺陆海鹰高艳欣冉媛
Owner AECC SHENYANG ENGINE RES INST
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