CN105781746B - A kind of adaptive Inertia particle separator - Google Patents
A kind of adaptive Inertia particle separator Download PDFInfo
- Publication number
- CN105781746B CN105781746B CN201610299853.9A CN201610299853A CN105781746B CN 105781746 B CN105781746 B CN 105781746B CN 201610299853 A CN201610299853 A CN 201610299853A CN 105781746 B CN105781746 B CN 105781746B
- Authority
- CN
- China
- Prior art keywords
- runner
- wall
- cylinder
- shell
- splitter
- 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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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/05—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for obviating the penetration of damaging objects or particles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01D—SEPARATION
- B01D45/00—Separating dispersed particles from gases or vapours by gravity, inertia, or centrifugal forces
- B01D45/04—Separating dispersed particles from gases or vapours by gravity, inertia, or centrifugal forces by utilising inertia
- B01D45/06—Separating dispersed particles from gases or vapours by gravity, inertia, or centrifugal forces by utilising inertia by reversal of direction of flow
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/042—Air intakes for gas-turbine plants or jet-propulsion plants having variable geometry
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/32—Application in turbines in gas turbines
- F05D2220/329—Application in turbines in gas turbines in helicopters
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Geometry (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Cyclones (AREA)
Abstract
The invention discloses a kind of adaptive Inertia particle separator, including shell, runner and cylinder, the runner is arranged on the enclosure, and the cylinder installation is on the housing, the drive link of the cylinder is connected through the shell with the flow path wall, and the flow path wall is deformable structure.The present invention can adjust flow channel shape according to various sizes of dirt sand particle under varying environment, improve the adaptability of helicopter, extend the scope that helicopter performs task.
Description
Technical field
The present invention relates to helicopter manufacturing technology field, especially a kind of adaptive Inertia particle separator.
Background technology
Helicopter has the characteristics that maneuverability, good concealment, survival ability are strong, can undertake other vehicles and be difficult to very
To being irrealizable task, irreplaceable effect is all served in military combat, domestic life.For example helicopter can
With on extemporal place, mountain area or desert floor, the tasks such as lifting, transport, rescue or investigation and motivation are performed,
Ask close to ground hovering, take-off and landing, can also hover and fly on sea again.For this reason, helicopter just has
Serious more environmental impact issues than other types aircraft.
Aboard, engine is a component that is extremely important and being easily damaged, it is necessary to prevents hostile environment to it
Infringement.In various environmental effects, Sand Dust Environment is an environmental factor that can not ignore.It is general to regard 0.01mm ~ 1.0mm's
Particle is sand, and 0.0001mm ~ 0.01mm particle is dust.Dirt sand swallows caused main disastrous effect by engine：Pressure
Mechanism of qi blade is denuded and resulting engine performance deterioration, i.e. power drop, rate of fuel consumption increase, ultimately results in engine
Service life shortens.Therefore, various purification air inlets are widely used on helicopter, such as filter, barrier particle separator, rotation
Wind particle separator, tubular type particle separator, Inertia particle separator etc..Wherein, Inertia particle separator is due to the letter of its structure
The advantages that single, in light weight, flow losses are small, it is usually used in high velocity air feeder connection.
When flow channel of the fluid containing solid particles of sand by turn, particle is due to its inertia, always from bending
The position centrifugation movement of the passage center of curvature（Or moved by original rectilinear direction）.In this way it is possible to streamline of jumping over, point
The dirt sand powder collection being dispersed in fluid gets up and excluded from system.
The size range for the particle that can be isolated is a highly important parameter of Inertia particle separator, and it is very
The scope that helicopter performs task is have impact in big degree.Several Inertia particle separator inner flow passage shapes main at present are all
Be fixed, only there is preferable separating effect to the dirt sand of specific dimensions scope, and in reality different geographical dirt sand particle chi
Very little difference, even the dirt sand in same place also has different Size Distributions, this adaptability to Inertia particle separator carries
Very high requirement is gone out.
The content of the invention
The present invention in view of the shortcomings of the prior art, proposes a kind of adaptive Inertia particle separator, can be according to different rings
Various sizes of dirt sand particle adjustment flow channel shape under border, improves the adaptability of helicopter, extends helicopter and perform task
Scope.
In order to realize foregoing invention purpose, the present invention provides following technical scheme：
A kind of adaptive Inertia particle separator, including shell, runner and cylinder,
The runner is arranged on the enclosure, and the cylinder is installed on the housing, the drive link of the cylinder
It is connected through the shell with the flow path wall, the flow path wall is deformable structure.
Further, the flow path wall includes runner inner wall and runner outer wall and is runner therebetween, in the runner
Wall is oppositely arranged in the shell with the runner outer wall, and the runner inner wall is connected with the first cylinder, the runner outer wall
It is connected with the second cylinder.
Further, first cylinder is interleaved in the direction that the flow channel length extends with second cylinder
's.
Further, the big convex radian of half portion thereon of the recessed radian in the shell lower half,
The runner outer wall and second cylinder are arranged on the shell first half, and the runner outer wall is convex
Its shape is corresponding with the shell first half shape when playing highest point,
The runner inner wall and first cylinder are arranged on the shell lower half, and the runner inner wall is to recessed
Enter corresponding with shell lower half shape to its shape during lowest part.
Further, in addition to control-rod and splitter,
The splitter and the control-rod are located in the runner, and the control-rod is extension type and grown along the runner
Direction extension is spent, the splitter is arranged on the control-rod close to the position of the air inlet of the runner.
Further, the tip of the splitter cross section is close to the air inlet side, and the splitter is close to the runner
Outer wall is arcwall face for plane, close to the runner inner wall.
A kind of adaptive Inertia particle separator of the present invention, it can be adjusted according to various sizes of dirt sand particle under varying environment
Rectification road shape, the adaptability of helicopter is improved, extend the scope that helicopter performs task.
Brief description of the drawings
Fig. 1 is the partial plan view of helicopter described in background of invention, including two engines and
Two separators；
Fig. 2 is a kind of cross-sectional view of adaptive Inertia particle separator of the present invention, wherein dotted line arrow
Represent the air-flow direction with sand dust；Solid arrow represents the direction that sand dust flies out；Dotted arrow is represented after excluding sand dust
The direction of air flow；
Fig. 3 is that a kind of runner deformation of adaptive Inertia particle separator of the present invention and control-rod are retracted and illustrated
Figure,
Position behind the position of runner inner wall and runner outer wall after the deformation of where the dotted line signifies that runner, and control-rod retraction
The position of splitter,
Label 12 is the runner outer wall after change in location；Label 13 is the runner inner wall after change in location.
Embodiment
The present invention will be described in detail below in conjunction with the accompanying drawings, and the description of this part is only exemplary and explanatory, should not
There is any restriction effect to protection scope of the present invention.
A kind of adaptive Inertia particle separator as Figure 1-3, including shell, runner 3 and cylinder,
Runner 3 is set inside the housing, and flow path wall edge is fixedly connected with shell, and other positions separate with shell,
Cylinder is arranged on shell, and the drive link of cylinder is connected through shell with flow path wall, and flow path wall is deformable structure, can be flexibility
Structure, it can be made up of deformable material.
Flow path wall includes runner inner wall 7 and runner outer wall 2 and is runner 3, runner inner wall 7 and runner outer wall 2 therebetween
It is oppositely arranged in shell, runner inner wall 7 is connected with the first cylinder 8, and runner outer wall 2 is connected with the second cylinder 4.
First cylinder 8 and the second cylinder 4 are interleaved in the direction that the length of runner 3 extends.
The big convex radian in the cross section of half portion 1 thereon of the recessed radian in the cross section of shell lower half 10,
The cylinder 4 of runner outer wall 2 and second is arranged on the shell first half 1, and when runner outer wall 2 raises up to highest point
Its shape is corresponding with the shape of the shell first half 1,
The cylinder 8 of runner inner wall 7 and first is arranged on shell lower half 10, and runner inner wall 7 is downwardly concaved lowest part
When its shape it is corresponding with the shape of shell lower half 10, the first cylinder 8 and the second cylinder 4 have control valve control, and the He of the first cylinder 8
Second cylinder 4 can be made up of airway tube and air rammer.
Also include control-rod 5 and splitter 6,
Splitter 6 and control-rod 5 are located in runner 3, and control-rod 5 is extension type and extended along the length direction of runner 3, splitter
6 are arranged on control-rod 5 close to the position of the air inlet of runner 3.
The tip of the cross section of splitter 6 is plane, in runner close to runner outer wall 2 close to air inlet side, splitter 6
Wall 7 for the arcwall face arcwall face curved line to be downwardly concaved in cross.
When the air with dirt sand enters air stream enter runner 3, according to the size of dirt sand, air rammer control flow path wall forms specific
Shape, while control-rod 5 adjust splitter 6 position, make separator formed there is optimal separation efficiency for the dirt sand size
Configuration.The present invention can be controlled manually by driver according to actual environment, can also be with detection device and automatic control
System processed combines, and realizes that carrying out runner 3 automatically according to varying environment adjusts.
A kind of adaptive Inertia particle separator of the present invention, it can be adjusted according to various sizes of dirt sand particle under varying environment
Rectification road shape, the adaptability of helicopter is improved, extend the scope that helicopter performs task.
Claims (3)
- A kind of 1. adaptive Inertia particle separator, it is characterised in that including shell, runner and cylinder,The runner is arranged on the enclosure, and on the housing, the drive link of the cylinder passes through for the cylinder installation The shell is connected with the flow path wall, and the flow path wall is deformable structure；The flow path wall includes runner inner wall and runner outer wall and be runner therebetween, outside the runner inner wall and the runner Wall is oppositely arranged in the shell, and the runner inner wall is connected with the first cylinder, and the runner outer wall is connected with the second cylinder；First cylinder is interleaved in the direction that the flow channel length extends with second cylinder；The big convex radian of half portion thereon of the recessed radian in the shell lower half,The runner outer wall and second cylinder are arranged on the shell first half, and the runner outer wall raise up to Its shape is corresponding with the shell first half shape during highest point,The runner inner wall and first cylinder are arranged on the shell lower half, and the runner inner wall is downwardly concaved Its shape is corresponding with the shell lower half shape during lowest part.
- A kind of 2. adaptive Inertia particle separator as claimed in claim 1, it is characterised in that also including control-rod and splitter,The splitter and the control-rod are located in the runner, and the control-rod is extension type and along the flow channel length side To extension, the splitter is arranged on the control-rod close to the position of the air inlet of the runner.
- A kind of 3. adaptive Inertia particle separator as claimed in claim 2, it is characterised in that the tip of the splitter cross section Close to the air inlet side, the splitter is arc for plane, close to the runner inner wall close to the runner outer wall Face.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610299853.9A CN105781746B (en) | 2016-05-09 | 2016-05-09 | A kind of adaptive Inertia particle separator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610299853.9A CN105781746B (en) | 2016-05-09 | 2016-05-09 | A kind of adaptive Inertia particle separator |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105781746A CN105781746A (en) | 2016-07-20 |
| CN105781746B true CN105781746B (en) | 2017-11-10 |
Family
ID=56400990
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610299853.9A Expired - Fee Related CN105781746B (en) | 2016-05-09 | 2016-05-09 | A kind of adaptive Inertia particle separator |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105781746B (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106523158B (en) * | 2016-11-09 | 2018-01-19 | 南京航空航天大学 | A kind of turboshaft engine inlet duct and operating method |
| CN111544964B (en) * | 2020-05-13 | 2022-01-25 | 中国航发湖南动力机械研究所 | Engine and particle separator thereof |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102698510A (en) * | 2012-04-13 | 2012-10-03 | 上海交通大学 | Airflow channel entry inertia particle separator |
| CN102935311A (en) * | 2012-10-19 | 2013-02-20 | 上海交通大学 | Inertia particle separator |
| EP2708737A1 (en) * | 2012-09-12 | 2014-03-19 | Alstom Technology Ltd | Method for operating a thermal power plant |
| CN205618256U (en) * | 2016-05-09 | 2016-10-05 | 兰州大学 | Self -adaptation inertia particle separator |
-
2016
- 2016-05-09 CN CN201610299853.9A patent/CN105781746B/en not_active Expired - Fee Related
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102698510A (en) * | 2012-04-13 | 2012-10-03 | 上海交通大学 | Airflow channel entry inertia particle separator |
| EP2708737A1 (en) * | 2012-09-12 | 2014-03-19 | Alstom Technology Ltd | Method for operating a thermal power plant |
| CN102935311A (en) * | 2012-10-19 | 2013-02-20 | 上海交通大学 | Inertia particle separator |
| CN205618256U (en) * | 2016-05-09 | 2016-10-05 | 兰州大学 | Self -adaptation inertia particle separator |
Non-Patent Citations (2)
| Title |
|---|
| "应用正交试验法进行惯性粒子分离器结构优化";孙亮亮等;《热能动力工程》;20160430;第31卷(第4期);31-37、142 * |
| "直升机发动机进气防护装置研究";付焱晶;《中国优秀硕士学位论文全文数据库 工程科技Ⅱ辑》;20150515(第5期);C031-82 * |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105781746A (en) | 2016-07-20 |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20171110 Termination date: 20190509 |