Testing stand and method of researching rotation characteristics of part of components in fluid system

A technology of rotation characteristics and fluid systems, applied in the field of aerospace, can solve the problems of wasting manpower and material resources, bulky, complex construction and layout, etc., and achieve the effect of reducing the difficulty of pipeline connection, reducing complexity, and simple structure

Inactive Publication Date: 2017-03-15
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] However, the current domestic rotary test benches are too large in size, and the purpose is to place the entire fluid system on the rotary bench to study the flow characteristics of the fluid in a certain component
Therefore, the construction and arrangement of the system on the turntable is particularly complicated, and a lot of manpower and material resources will be wasted

Method used

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  • Testing stand and method of researching rotation characteristics of part of components in fluid system

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Embodiment Construction

[0013] As shown in the figure, a test bench for studying the rotational characteristics of some parts of the fluid system described in the present invention includes the following components: a rotating bench 1 for installing the research object device, a bearing 3, a rotating shaft 4, a shaft Cover 5, variable frequency motor 9, fixed tripod 12. The surface of the rotating platform 1 has threaded holes 11 for installing research components; the rotating shaft 4 and the rotating platform 1 are connected by flanges and fixed by several bolts 2 . There are anti-rotation holes 6 and several pipeline connection holes 7 on the shaft sleeve 5; several fluid passages 10 are opened inside the rotating platform 1 and the rotating shaft 4 .

[0014] The concrete implementation operation of patent of the present invention is as follows:

[0015] When studying the working characteristics of a single component or multiple components in the system under different overload conditions, it is...

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Abstract

The invention relates to a testing stand and method of researching rotation characteristics of part of components in a fluid system, and belongs to the technical field of aerospace engineering. The testing stand of researching rotation characteristics of part of components in a fluid system includes the following components: a rotation stand rack (1), bearings (3), a rotating shaft (4), a shaft sleeve (5), a variable frequency motor (9) and a fixed foot rest (12); the rotation stand rack (1), the bearing (3), the rotating shaft (4), the shaft sleeve (5), the variable frequency motor (9) and the fixed foot rest (12) are used for mounting research object apparatus; the surface of the rotation stand rack (1) is provided with a screwed hole (11) for mounting research components; the rotating shaft (4) and the rotation stand rack (1) are connected through a flange, and are fixed by means of a plurality of bolts (2); a standstill locking hole (6) and a plurality of connection holes (7) are formed in the shaft sleeve (5); and a plurality of fluid channels (10) are formed in the rotation stand rack (1) and the rotating shaft (4). The testing stand of researching rotation characteristics of part of components in a fluid system can be used for researching the operating characteristics of the fluid in the part of components in the system in different overload environment, and has the advantages of being simple in structure, being simple to operate, and being efficient in operating.

Description

technical field [0001] The invention relates to a test bench and method for studying the rotational characteristics of some parts of a fluid system, belonging to the technical field of aerospace. Background technique [0002] With the development of the aerospace industry, the overload characteristics of the fluid system inside the aircraft have attracted much attention, such as the air cycle refrigeration system, the evaporative cycle refrigeration system in the environmental control system, and the cooling system of the aircraft equipment. These systems all involve the working characteristics of the fluid under different overloads. [0003] For example, when a fighter jet is doing ordinary high-speed maneuvering flight, the overload on the fuselage can reach 6-9g in value. During the high-speed flight of modern top fighter jets, the overload may rise to 12g within one second. Various systems and components on the aircraft, including the onboard evaporative cycle refrigera...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01M13/00
CPCG01M13/00
Inventor 孙程斌王镭蒋彦龙刘湘婉高放
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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