CN105781746A - Self-adaption inertia particle separator - Google Patents
Self-adaption inertia particle separator Download PDFInfo
- Publication number
- CN105781746A CN105781746A CN201610299853.9A CN201610299853A CN105781746A CN 105781746 A CN105781746 A CN 105781746A CN 201610299853 A CN201610299853 A CN 201610299853A CN 105781746 A CN105781746 A CN 105781746A
- Authority
- CN
- China
- Prior art keywords
- wall
- runner
- cylinder
- particle separator
- self adaptation
- 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.)
- Granted
Links
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 self-adaption inertia particle separator which comprises a housing, a flow passage and cylinders, wherein the flow passage is formed in the housing; the cylinders are installed on the housing; transmission rods of the cylinders penetrate through the housing and are connected with the walls of the flow passage; and the flow passage has a deformable structure. According to the self-adaption inertia particle separator, the shape of the flow passage can be regulated according to dust sand particles in different sizes in different environments, so that the adaptation of a helicopter is improved, and the range of the helicopter of executing a task is expanded.
Description
Technical field
The present invention relates to helicopter manufacturing technology field, especially a kind of self adaptation Inertia particle separator.
Background technology
Helicopter has the features such as maneuverability, good concealment, survival ability be strong, and can undertake other vehicles is difficult to or even irrealizable task, all serves irreplaceable effect in military combat, domestic life.Such as, helicopter on extemporal place, mountain area or desert floor, can perform lifting, transport, rescue or the task such as investigation and motivation, it is desirable to close to ground hovering, take-off and landing, it is also possible to hovering and flight on sea again.For this reason, helicopter just has the many environmental impact issues more serious than other types aircraft.
Aboard, electromotor is a component that is extremely important and that be easily damaged, it is necessary to prevent the hostile environment infringement to it.In various environmental effects, Sand Dust Environment is an environmental factors can not ignore.Being generally sand depending on the particle of 0.01mm ~ 1.0mm, the particle of 0.0001mm ~ 0.01mm is dust.Dirt sand is swallowed the main disastrous effect caused by electromotor: compressor blade abrasion and consequent engine performance deterioration, and namely power drop, rate of fuel consumption increase, and the service life ultimately resulting in electromotor shortens.Therefore, various purification air inlets are widely used on helicopter, such as filter, barrier particle separator, whirlwind particle separator, tubular type particle separator, Inertia particle separator etc..Wherein, Inertia particle separator, due to its simple in construction, the advantage such as lightweight, flow losses are little, is usually used in high velocity air feeder connection.
When the fluid containing solid particles of sand passes through the flow channel turned round, particle is due to its inertia, always centrifugal mobile (or by original rectilinear direction motion) from the position of the bending channel center of curvature.The streamline in this way it is possible to jump over, gets up the dirt sand powder collection being dispersed in fluid exclude from system.
Can the size range of isolated particle be a highly important parameter of Inertia particle separator, it have impact on helicopter to a great extent and performs the scope of task.Several Inertia particle separator inner flow passage shapes currently mainly are all fixing, only the dirt sand of specific dimensions scope there is good separating effect, and the dirt sand particle size of different geographical is different in reality, even the dirt sand in same place also has different distribution of sizes, the adaptive capacity of Inertia particle separator is proposed significantly high requirement by this.
Summary of the invention
The present invention is directed to the deficiencies in the prior art, it is proposed to a kind of self adaptation Inertia particle separator, it is possible to adjust flow channel shape according to various sizes of dirt sand granule under varying environment, improve the adaptability of helicopter, extend helicopter and perform the scope of task.
In order to realize foregoing invention purpose, the present invention provides techniques below scheme:
A kind of self adaptation Inertia particle separator, including shell, runner and cylinder,
Described runner is arranged on described enclosure, and described cylinder is installed on the housing, and the drive link of described cylinder is connected through described shell with described flow path wall, and described flow path wall is deformable structure.
Further, described flow path wall includes runner inner wall and runner outer wall and is oppositely arranged in described shell for runner, described runner inner wall and described runner outer wall therebetween, and described runner inner wall is connected with the first cylinder, and described runner outer wall and the second cylinder connect.
Further, described first cylinder and described second cylinder are interleaved with out in the direction that described flow channel length extends.
Further, the recessed radian in described shell lower half more than the radian of its first half epirelief,
Described runner outer wall and described second cylinder are arranged on the described shell first half, and described runner outer wall raise up highest point time its shape corresponding with described shell first half shape,
Described runner inner wall and described first cylinder are arranged on described shell lower half, and described runner inner wall to be downwardly concaved its shape during lowest point corresponding with described shell lower half shape.
Further, also include controlling bar and splitter,
Described splitter and described control bar are positioned at described runner, and described control bar is extension type and extends along described flow channel length direction, and described splitter is arranged on described control bar near the position of the air inlet of described runner.
Further, the tip of described splitter cross section near described air inlet side, described splitter near described runner outer wall be plane, near described runner inner wall for arcwall face.
One self adaptation Inertia particle separator of the present invention, it is possible to adjust flow channel shape according to various sizes of dirt sand granule under varying environment, improve the adaptability of helicopter, extends helicopter and performs the scope of task.
Accompanying drawing explanation
Fig. 1 is the partial plan view of helicopter described in background of invention, including two electromotors and two separators；
Fig. 2 is the cross sectional representation of a kind of self adaptation Inertia particle separator of the present invention, and wherein dotted line arrow represents the air-flow direction with sand dust；Solid arrow represents the direction that sand dust flies out；Dotted arrow represents gets rid of the direction of air flowing after sand dust；
Fig. 3 is the runner deformation of a kind of self adaptation Inertia particle separator of the present invention and controls bar retraction schematic diagram,
The position of runner inner wall and runner outer wall after the deformation of where the dotted line signifies that runner, and control the position of the position splitter after bar is retracted,
Label 12 is the runner outer wall after change in location；Label 13 is the runner inner wall after change in location.
Detailed description of the invention
Describing the present invention below in conjunction with accompanying drawing, the description of this part is only exemplary and explanatory, and protection scope of the present invention should not have any restriction effect.
A kind of self adaptation Inertia particle separator as Figure 1-3, including shell, runner 3 and cylinder,
Runner 3 is arranged on enclosure, and flow path wall edge is fixing with shell to be connected, 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 flexible structure, can be made up of deformable material.
Flow path wall includes runner inner wall 7 and runner outer wall 2 and is therebetween runner 3, and runner inner wall 7 and runner outer wall 2 are oppositely arranged in the enclosure, and 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 what the second cylinder 4 was interleaved with out in the direction that runner 3 length extends.
The recessed radian of shell lower half 10 cross section more than the radian of its first half 1 cross section epirelief,
Runner outer wall 2 and the second cylinder 4 are arranged on the shell first half 1, and runner outer wall 2 raise up highest point time its shape corresponding with the shell first half 1 shape,
Runner inner wall 7 and the first cylinder 8 are arranged on shell lower half 10, and runner inner wall 7 to be downwardly concaved its shape during lowest point corresponding with shell lower half 10 shape, first cylinder 8 and the second cylinder 4 have control valve to control, and the first cylinder 8 and the second cylinder 4 can be made up of airway and air rammer.
Also include controlling bar 5 and splitter 6,
Splitter 6 and control bar 5 are positioned at runner 3, control bar 5 and are extension type and extend along runner 3 length direction, and splitter 6 is arranged on control bar 5 near the position of the air inlet of runner 3.
The tip of splitter 6 cross section near air inlet side, splitter 6 near runner outer wall 2 for plane, near runner inner wall 7 for this arcwall face of arcwall face in cross for the curved line that is downwardly concaved.
When the air with dirt sand enters runner 3, the size according to dirt sand, air rammer controls flow path wall and forms specific shape, controls bar 5 simultaneously and adjusts the position of splitter 6, makes separator form the configuration this dirt sand size to optimal separation efficiency.The present invention can carry out Non-follow control by driver according to actual environment, it is also possible to is combined with detection equipment and automatic control system, it is achieved automatically carry out runner 3 according to varying environment and adjust.
One self adaptation Inertia particle separator of the present invention, it is possible to adjust flow channel shape according to various sizes of dirt sand granule under varying environment, improve the adaptability of helicopter, extends helicopter and performs the scope of task.
Claims (6)
1. a self adaptation Inertia particle separator, it is characterised in that include shell, runner and cylinder,
Described runner is arranged on described enclosure, and described cylinder is installed on the housing, and the drive link of described cylinder is connected through described shell with described flow path wall, and described flow path wall is deformable structure.
2. a kind of self adaptation Inertia particle separator as claimed in claim 1, it is characterized in that, described flow path wall includes runner inner wall and runner outer wall and therebetween for runner, described runner inner wall and described runner outer wall are oppositely arranged in described shell, described runner inner wall is connected with the first cylinder, and described runner outer wall and the second cylinder connect.
3. a kind of self adaptation Inertia particle separator as claimed in claim 2, it is characterised in that described first cylinder and described second cylinder are interleaved with out in the direction that described flow channel length extends.
4. as claimed in claim 2 a kind of self adaptation Inertia particle separator, it is characterised in that the recessed radian in described shell lower half more than the radian of its first half epirelief,
Described runner outer wall and described second cylinder are arranged on the described shell first half, and described runner outer wall raise up highest point time its shape corresponding with described shell first half shape,
Described runner inner wall and described first cylinder are arranged on described shell lower half, and described runner inner wall to be downwardly concaved its shape during lowest point corresponding with described shell lower half shape.
5. a kind of self adaptation Inertia particle separator as described in as arbitrary in Claims 1-4, it is characterised in that also include controlling bar and splitter,
Described splitter and described control bar are positioned at described runner, and described control bar is extension type and extends along described flow channel length direction, and described splitter is arranged on described control bar near the position of the air inlet of described runner.
6. as claimed in claim 5 a kind of self adaptation Inertia particle separator, it is characterised in that the tip of described splitter cross section near described air inlet side, described splitter near described runner outer wall be plane, be arcwall face near described runner inner wall.
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 true CN105781746A (en) | 2016-07-20 |
| CN105781746B 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) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106523158A (en) * | 2016-11-09 | 2017-03-22 | 南京航空航天大学 | Turboshaft engine intake device and operation method |
| CN111544964A (en) * | 2020-05-13 | 2020-08-18 | 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 |
|---|
| 付焱晶: ""直升机发动机进气防护装置研究"", 《中国优秀硕士学位论文全文数据库 工程科技Ⅱ辑》 * |
| 孙亮亮等: ""应用正交试验法进行惯性粒子分离器结构优化"", 《热能动力工程》 * |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106523158A (en) * | 2016-11-09 | 2017-03-22 | 南京航空航天大学 | Turboshaft engine intake device and operation method |
| CN107605602A (en) * | 2016-11-09 | 2018-01-19 | 南京航空航天大学 | A kind of structure changes turboshaft engine gas handling system |
| CN107605602B (en) * | 2016-11-09 | 2018-08-31 | 南京航空航天大学 | A kind of structure changes turboshaft engine gas handling system |
| CN111544964A (en) * | 2020-05-13 | 2020-08-18 | 中国航发湖南动力机械研究所 | Engine and particle separator thereof |
| 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 |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105781746B (en) | 2017-11-10 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN205618256U (en) | Self -adaptation inertia particle separator | |
| JP5996040B2 (en) | Aircraft with an air intake for an air intake propulsion engine | |
| US7922784B2 (en) | System for inertial particles separation | |
| US10723475B2 (en) | Air intake unit for an aircraft engine and provided with an air filter and with an air filter bypass duct | |
| US20150096627A1 (en) | Engine mounted inlet plenum for a rotorcraft | |
| EP3147210A2 (en) | Unmanned helicopter | |
| CN105781746A (en) | Self-adaption inertia particle separator | |
| CN109677608A (en) | Anury all-wing aircraft couples power aerial vehicle | |
| US9988148B2 (en) | Vehicle with asymmetric nacelle configuration | |
| CN107021235B (en) | A kind of low-to-medium altitude aircraft driving device, driving method and low-to-medium altitude aircraft | |
| CN206243476U (en) | VTOL fixed-wing unmanned plane | |
| CN109850128A (en) | Multistage air blowing circular rector high lift device and aircraft | |
| US20160280388A1 (en) | Intake structure of aircraft | |
| CN109383765A (en) | Damping device for exposed undercarriage chamber | |
| CN107161352B (en) | Floating body type four-rotor flying robot landing platform | |
| CN113335499B (en) | High-mobility unmanned aerial vehicle based on solid rocket auxiliary power | |
| CN107585305A (en) | A kind of light and handy unmanned plane | |
| CN213800151U (en) | Shaftless duct vertical take-off and landing carrier-based fighter plane | |
| CN210821697U (en) | Power device for rescuing in scenic spot and dangerous area and unmanned aerial vehicle | |
| CN209241325U (en) | Anury all-wing aircraft couples power aerial vehicle | |
| CN207242025U (en) | A kind of laterally folded quadrotor unmanned aerial vehicle body | |
| CN205707327U (en) | Portable electric four rotor unmanned aircraft | |
| CN109484635B (en) | A kuppe for oiling move unmanned aerial vehicle's rotor | |
| CN110844091A (en) | Injection type engine sand prevention system and method | |
| CN109484636A (en) | The support construction of pod for the dynamic unmanned plane of oil |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 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 |