CN201688961U - Spray pipe for aerospace wind tunnel test equipment - Google Patents
Spray pipe for aerospace wind tunnel test equipment Download PDFInfo
- Publication number
- CN201688961U CN201688961U CN2010201808588U CN201020180858U CN201688961U CN 201688961 U CN201688961 U CN 201688961U CN 2010201808588 U CN2010201808588 U CN 2010201808588U CN 201020180858 U CN201020180858 U CN 201020180858U CN 201688961 U CN201688961 U CN 201688961U
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- CN
- China
- Prior art keywords
- test equipment
- tunnel test
- wind tunnel
- spray pipe
- jet pipe
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
Abstract
The utility model discloses a spray pipe for aerospace wind tunnel test equipment, which comprises a cylinder body, a reinforcing ring arranged on the external surface of the cylinder body, and the inner surface of the cylinder body is shaped like a parabola. By adopting the technical scheme, the spray pipes are connected sequentially, so the construction is convenient and the use reliability is ensured, and the disadvantages of air pores, slag inclusion and cracks of steel castings are eliminated. The parabola-shaped inner hole of the spray pipe ensures the high-speed parallel wind.
Description
Technical field
The utility model relates to a kind of Aero-Space wind tunnel test equipment jet pipe.
Background technology
Wind-tunnel is a basic equipment that carries out the aerodynamics experiment.Most of aerodynamic force experiment is up to now all finished in wind-tunnel.Because the complicacy of gas flow phenomenon and object (aircraft) geometric shape, many problems in aerodynamic studies and the aircraft pneumatic design all can not rely on theory or numerical simulation to solve merely, and must be by a large amount of experiments, find out its rule or data are provided, and combine research with theoretical the analysis, so just can deal with problems, because wind-tunnel is the basic equipment that carries out the aerodynamic force experiment, so the development of aeronautical technology is just directly relevant with the wind-tunnel development.Before any one aircraft formally designs, finalizes the design, all must be through a large amount of blowing experiments.
Spout is a critical component in the wind-tunnel.Existing spout adopts integral solder, occurs shortcomings such as pore, slag inclusion, crackle easily.
The utility model content
Technical problem to be solved in the utility model provides a kind of Aero-Space wind tunnel test equipment jet pipe.Easy construction is used reliably, has eliminated shortcomings such as the pore in the steel-casting, slag inclusion, crackle.
For solving the problems of the technologies described above, the utility model adopts following technical scheme: Aero-Space wind tunnel test equipment is used jet pipe, comprises cylindrical shell, and the appearance of described cylindrical shell is provided with stiffening ring, and the inside surface of described cylindrical shell is a para-curve.
Described cylindrical shell and the welding of described stiffening ring.
Described jet pipe is a steel-casting.
The utility model is owing to adopted technique scheme, and some jet pipes connect successively, and easy construction is used reliably, has eliminated shortcomings such as the pore in the steel-casting, slag inclusion, crackle.The jet pipe endoporus is a para-curve, has guaranteed high speed parallel wind.
Description of drawings
Fig. 1 is the structural representation of the utility model Aero-Space wind tunnel test equipment with jet pipe.
Embodiment
Below in conjunction with accompanying drawing embodiment of the present utility model is further described.
Figure 1 shows that the utility model Aero-Space wind tunnel test equipment uses jet pipe, comprise cylindrical shell 1, the appearance of described cylindrical shell 1 is provided with stiffening ring 2, and the inside surface 11 of described cylindrical shell 1 is a para-curve.Described cylindrical shell 1 and described stiffening ring 2 welding.Described jet pipe 2 is a steel-casting.
The utility model adopts some jet pipes to connect successively, and easy construction is used reliably, has eliminated shortcomings such as the pore in the steel-casting, slag inclusion, crackle.The jet pipe endoporus is a para-curve, has guaranteed high speed parallel wind.
Claims (3)
1. Aero-Space wind tunnel test equipment is used jet pipe, and it is characterized in that: comprise cylindrical shell (1), the appearance of described cylindrical shell (1) is provided with stiffening ring (2), and the inside surface (11) of described cylindrical shell (1) is a para-curve.
2. use jet pipe according to the described Aero-Space wind tunnel test equipment of claim 1, it is characterized in that: described cylindrical shell (1) and described stiffening ring (2) welding.
3. use jet pipe according to the described Aero-Space wind tunnel test equipment of claim 1, it is characterized in that: described jet pipe (2) is a steel-casting.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010201808588U CN201688961U (en) | 2010-04-30 | 2010-04-30 | Spray pipe for aerospace wind tunnel test equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010201808588U CN201688961U (en) | 2010-04-30 | 2010-04-30 | Spray pipe for aerospace wind tunnel test equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201688961U true CN201688961U (en) | 2010-12-29 |
Family
ID=43377241
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2010201808588U Expired - Fee Related CN201688961U (en) | 2010-04-30 | 2010-04-30 | Spray pipe for aerospace wind tunnel test equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201688961U (en) |
-
2010
- 2010-04-30 CN CN2010201808588U patent/CN201688961U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20101229 Termination date: 20130430 |