CN111336162A - Device for converting space directional flow direction to balanced flow - Google Patents
Device for converting space directional flow direction to balanced flow Download PDFInfo
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- CN111336162A CN111336162A CN202010217774.5A CN202010217774A CN111336162A CN 111336162 A CN111336162 A CN 111336162A CN 202010217774 A CN202010217774 A CN 202010217774A CN 111336162 A CN111336162 A CN 111336162A
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- circular
- flow
- truncated cone
- cone structure
- circular truncated
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15D—FLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOW OF GASES OR LIQUIDS
- F15D1/00—Influencing flow of fluids
- F15D1/02—Influencing flow of fluids in pipes or conduits
- F15D1/025—Influencing flow of fluids in pipes or conduits by means of orifice or throttle elements
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E30/00—Energy generation of nuclear origin
- Y02E30/30—Nuclear fission reactors
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- Fluid Mechanics (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Measuring Volume Flow (AREA)
Abstract
The invention belongs to the technical field of space gas incoming flow conversion equipment, and particularly relates to a device for converting space directional flow direction balanced flow, which consists of a circular truncated cone structure (1), a first circular baffle (2), a flow plug (3), a shell (4) and a second circular baffle (8); the end part of one end of the shell (4) is provided with a circular truncated cone structure (1), the end part of the circular truncated cone structure (1) is additionally provided with a sampling hole (5), a first circular baffle (2) extends from the end part close to the circular truncated cone structure (1), a plurality of circular grooves (6) are additionally arranged between the first circular baffle (2) and the circular truncated cone structure (1), and a flow plug (3) is arranged in the circular truncated cone structure (1); a sampling chamber (7) is arranged in the shell (4) towards one side far away from the flow plug (3); a second circular baffle (8) extends outwards from the end part of the other end of the shell (4); the device converts the high-speed gas inflow in a non-equilibrium state into a high-speed gas inflow in an equilibrium state.
Description
Technical Field
The invention belongs to the technical field of space gas incoming flow conversion equipment, and particularly relates to a device for converting space directional flow direction into balanced flow.
Background
The earth thermal layer atmosphere is an important component of a space environment and is influenced by factors such as solar activity, geomagnetic disturbance, longitude and latitude heights and the like, the thermal layer atmosphere changes very severely, related detection is carried out at home and abroad, ionization gauges, ion sources, pressure gauges and the like are common detection instruments which are all mounted on an aircraft, the flying speed of the aircraft is up to 7.8km/s, a balance flow conversion device for directly measuring high-speed airflow in a non-equilibrium state is not provided at present, and the current balance flow conversion device has great difficulty and great error.
Disclosure of Invention
The invention aims to solve the defects of the prior art, and provides a device for converting a space-oriented flow direction to a balanced flow, which converts a high-speed gas incoming flow in a non-balanced state into a high-speed gas incoming flow in a balanced state, and balances the temperature, the speed and the density of the high-speed gas incoming flow in all directions.
The invention provides a device for converting space-oriented flow direction balanced flow, which consists of a circular truncated cone structure, a first circular baffle, a flow plug, a shell and a second circular baffle; wherein the content of the first and second substances,
the end part of one end of the shell is provided with a circular truncated cone structure, the end part of the circular truncated cone structure is additionally provided with a sampling hole, a first circular baffle is extended out of the end part close to the circular truncated cone structure, a plurality of circular grooves are additionally arranged between the first circular baffle and the circular truncated cone structure, and a flow plug is arranged in the circular truncated cone structure; a sampling chamber is arranged in the shell towards one side far away from the flow plug; the other end of the shell extends outwards to form a second round baffle.
As an improvement of the above technical solution, a diameter of one end of the circular truncated cone structure is smaller than a diameter of the other end thereof.
As an improvement of the above technical solution, the first circular blocking piece is located above the second circular blocking piece, and the diameter of the first circular blocking piece is smaller than that of the second circular blocking piece.
As one improvement of the technical scheme, the diameter of the sampling hole is phi 1-30 mm.
As one improvement of the technical scheme, the diameter of the sampling chamber is phi 3-100 mm.
As an improvement of the technical scheme, the flow plug is in a flat plate shape, a conical shape or an arc disc structure.
As one improvement of the technical scheme, the circular truncated cone structure, the first circular baffle, the second circular baffle, the flow plug and the shell are all made of stainless steel, magnesium alloy or aluminum alloy materials.
Compared with the prior art, the invention has the beneficial effects that:
the device converts the high-speed gas incoming flow in the non-equilibrium state into the high-speed gas incoming flow in the equilibrium state, balances the temperature, the speed and the density of the high-speed gas incoming flow in all directions, is convenient for a measuring device arranged at the rear end of the device to measure, and improves the measuring sensitivity and the measuring precision.
Drawings
Fig. 1 is a schematic structural diagram of a device for converting a spatially oriented flow direction into a balanced flow according to the present invention.
Reference numerals:
1. round platform structure 2 and first circular baffle sheet
3. Choke 4, shell
5. Sampling hole 6, circular recess
7. Sampling chamber 8, second circular baffle
Detailed Description
The invention will now be further described with reference to the accompanying drawings.
The invention provides a device for converting a space directional flow direction into a balanced flow, which has the characteristics of exquisite structure, strong direction adaptability and simple structure and realizes the conversion of a high-speed gas incoming flow from a non-balanced state to a balanced state.
As shown in fig. 1, the apparatus includes: the flow plug comprises a circular truncated cone structure 1, a first circular baffle piece 2, a flow plug 3, a shell 4 and a second circular baffle piece 8; the end part of one end of the shell 4 is provided with a circular truncated cone structure 1, the end part of the circular truncated cone structure 1 is additionally provided with a sampling hole 5, a first circular baffle piece 2 extends from the end part close to the circular truncated cone structure 1, 3 circular grooves 6 are additionally arranged between the first circular baffle piece 2 and the circular truncated cone structure 1, and a flow plug 3 is arranged in the circular truncated cone structure 1; towards the side away from the flow plug 3, a sampling chamber 7 is arranged in the shell 4, and the high-speed gas inflow is stored in the sampling chamber 7; the other end of the housing 4 extends outward with a second circular baffle 8.
In the present embodiment, the housing 4 has a hollow cylindrical structure.
The diameter of the upper end of the round platform structure 1 is smaller than that of the lower end thereof, so that the cross section of the round platform structure is in a trapezoidal structure. In this embodiment, the diameter of one end of the truncated cone structure 1 at the port of the housing 4 is smaller than the diameter of the opposite end thereof, preventing the high-speed gas entering through the sampling hole 5 from flowing out, ensuring that it is stored entirely in the sampling chamber 7.
The diameter of the sampling hole 5 is phi 1-30 mm. In the present example, the sampling hole 5 has a diameter of 1 mm.
The sampling chamber 7 has a diameter of phi 3-100 mm. In the present example, the sampling chamber 7 has a diameter of 30 mm.
The flow plug 3 is in a flat plate shape, a conical shape or an arc disc structure, and blocks and collides the gas flowing from the high-speed gas. In this embodiment, the flow stopper 3 has an arc-shaped disk structure.
The first circular baffle plate 2 is positioned above the second circular baffle plate 8, and the diameter of the first circular baffle plate is smaller than that of the second circular baffle plate.
The round platform structure 1, the first circular baffle piece 2, the second circular baffle piece 8, the flow plug 3, the shell 4, the sampling hole 5, the circular groove 6 and the sampling chamber 7 are all made of stainless steel materials, and can also be made of magnesium alloy or aluminum alloy materials according to different application occasions.
When the directional high-speed gas inflow enters the interior through the sampling hole 5 on the circular truncated cone structure 1, gas molecules in the gas inflow collide with the flow plug 3, the collided gas molecules are reflected to the inner wall of the circular truncated cone structure 1 and the inner wall of the circular groove 6, and finally enter the interior of the sampling chamber 7, so that the gas distribution in the interior of the sampling chamber 7 accords with Maxwell distribution, namely the temperature, the speed and the density of the gas are balanced in all directions, and the purpose of converting the non-equilibrium high-speed gas inflow into the equilibrium gas inflow is achieved.
Finally, it should be noted that the above embodiments are only used for illustrating the technical solutions of the present invention and are not limited. Although the present invention has been described in detail with reference to the embodiments, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted without departing from the spirit and scope of the invention as defined in the appended claims.
Claims (7)
1. A device for converting space-oriented flow direction balanced flow comprises a circular truncated cone structure (1), a first circular baffle (2), a flow plug (3), a shell (4) and a second circular baffle (8); it is characterized in that the preparation method is characterized in that,
the end part of one end of the shell (4) is provided with a circular truncated cone structure (1), the end part of the circular truncated cone structure (1) is additionally provided with a sampling hole (5), a first circular baffle (2) extends from the end part close to the circular truncated cone structure (1), a plurality of circular grooves (6) are additionally arranged between the first circular baffle (2) and the circular truncated cone structure (1), and a flow plug (3) is arranged in the circular truncated cone structure (1); a sampling chamber (7) is arranged in the shell (4) towards one side far away from the flow plug (3); the end part of the other end of the shell (4) extends outwards to form a second round baffle plate (8).
2. Device for spatially directed flow direction balanced flow conversion according to claim 1, characterized in that the diameter of one end of the circular truncated cone structure (1) is smaller than the diameter of the other end thereof.
3. The device for spatially oriented flow direction balanced flow conversion according to claim 1, characterized in that the first circular flap (2) is located above the second circular flap (8) and the diameter of the first circular flap (2) is smaller than the diameter of the second circular flap (8).
4. The device for spatially directed flow direction balanced flow conversion according to claim 1, characterized in that the sampling holes (5) have a diameter of Φ 1-30 mm.
5. The device for spatially directed flow direction balanced flow conversion according to claim 1, characterized in that the sampling chamber (7) has a diameter of Φ 3-100 mm.
6. The device for spatially oriented flow direction balanced flow conversion as claimed in claim 1, characterized in that the flow stop (3) is of a plate-shaped, conical or arc-shaped disc structure.
7. The device for converting a spatially oriented flow direction into a balanced flow according to claim 1, wherein the circular truncated cone structure (1), the first circular baffle (2), the second circular baffle (8), the flow plug (3) and the housing (4) are made of stainless steel, magnesium alloy or aluminum alloy.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010217774.5A CN111336162B (en) | 2020-03-25 | 2020-03-25 | Device for converting space directional flow direction to balanced flow |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010217774.5A CN111336162B (en) | 2020-03-25 | 2020-03-25 | Device for converting space directional flow direction to balanced flow |
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| Publication Number | Publication Date |
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| CN111336162A true CN111336162A (en) | 2020-06-26 |
| CN111336162B CN111336162B (en) | 2022-05-31 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202010217774.5A Active CN111336162B (en) | 2020-03-25 | 2020-03-25 | Device for converting space directional flow direction to balanced flow |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115576342A (en) * | 2022-12-09 | 2023-01-06 | 中国空气动力研究与发展中心计算空气动力研究所 | Aircraft track control method, device, equipment and medium |
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|---|---|---|---|---|
| US3152617A (en) * | 1961-06-15 | 1964-10-13 | Beloit Iron Works | Stream flow valve |
| US5596152A (en) * | 1994-03-21 | 1997-01-21 | Instromet B.V. | Flow straightener for a turbine-wheel gasmeter |
| DE10148901B4 (en) * | 2001-09-24 | 2004-05-06 | Binder Engineering Gmbh | Flow rectifier module and flow rectifier |
| KR20120124898A (en) * | 2011-05-06 | 2012-11-14 | 엠씨테크주식회사 | Ozone mixing device and apparatus for cold salt water ozonation comprising thereof |
| CN103821801A (en) * | 2014-02-23 | 2014-05-28 | 中国科学院工程热物理研究所 | Resistance reducing rib |
| CN205278654U (en) * | 2015-12-04 | 2016-06-01 | 中国天辰工程有限公司 | Reverse nozzle pressure reduction means |
| CN106643363A (en) * | 2016-12-31 | 2017-05-10 | 何洪彬 | Shot hole plugging device for coal mine underground excavation |
| CN109253253A (en) * | 2018-10-25 | 2019-01-22 | 天津金泰盛世石化设备有限公司 | A kind of metal pressure container that stability is high |
| CN209354846U (en) * | 2018-10-30 | 2019-09-06 | 中国船舶重工集团公司第七一九研究所 | Pipeline shunt device |
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2020
- 2020-03-25 CN CN202010217774.5A patent/CN111336162B/en active Active
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3152617A (en) * | 1961-06-15 | 1964-10-13 | Beloit Iron Works | Stream flow valve |
| US5596152A (en) * | 1994-03-21 | 1997-01-21 | Instromet B.V. | Flow straightener for a turbine-wheel gasmeter |
| DE10148901B4 (en) * | 2001-09-24 | 2004-05-06 | Binder Engineering Gmbh | Flow rectifier module and flow rectifier |
| KR20120124898A (en) * | 2011-05-06 | 2012-11-14 | 엠씨테크주식회사 | Ozone mixing device and apparatus for cold salt water ozonation comprising thereof |
| CN103821801A (en) * | 2014-02-23 | 2014-05-28 | 中国科学院工程热物理研究所 | Resistance reducing rib |
| CN205278654U (en) * | 2015-12-04 | 2016-06-01 | 中国天辰工程有限公司 | Reverse nozzle pressure reduction means |
| CN106643363A (en) * | 2016-12-31 | 2017-05-10 | 何洪彬 | Shot hole plugging device for coal mine underground excavation |
| CN109253253A (en) * | 2018-10-25 | 2019-01-22 | 天津金泰盛世石化设备有限公司 | A kind of metal pressure container that stability is high |
| CN209354846U (en) * | 2018-10-30 | 2019-09-06 | 中国船舶重工集团公司第七一九研究所 | Pipeline shunt device |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115576342A (en) * | 2022-12-09 | 2023-01-06 | 中国空气动力研究与发展中心计算空气动力研究所 | Aircraft track control method, device, equipment and medium |
| CN115576342B (en) * | 2022-12-09 | 2023-03-24 | 中国空气动力研究与发展中心计算空气动力研究所 | Aircraft track control method, device, equipment and medium |
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| Publication number | Publication date |
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| CN111336162B (en) | 2022-05-31 |
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