CN205719489U - Rotary expansion wing plate ground-testing plant electrodynamic analogy expanding unit - Google Patents
Rotary expansion wing plate ground-testing plant electrodynamic analogy expanding unit Download PDFInfo
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- CN205719489U CN205719489U CN201620197586.XU CN201620197586U CN205719489U CN 205719489 U CN205719489 U CN 205719489U CN 201620197586 U CN201620197586 U CN 201620197586U CN 205719489 U CN205719489 U CN 205719489U
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- gyration
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- rotary expansion
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Abstract
This utility model provides a kind of rotary expansion wing plate ground-testing plant electrodynamic analogy expanding unit, including slider-crank mechanism and trans four-bar mechanism, slider-crank mechanism is using hinge O 〃 as the fixing centre of gyration, trans four-bar mechanism is using hinge O ' as the centre of gyration, hinge O ' or the centre of gyration of rotary expansion wing plate;Servomotor drives slide block to move along the rail by feed screw nut, slide block drives the crank of slider-crank mechanism to rotate around centre of gyration O 〃 by connecting rod, crank is connected with the connecting rod of trans four-bar mechanism by hinge, and then drive rocking bar to rotate around centre of gyration O ', rocking bar drives wing plate drive pin to rotate around centre of gyration O ', by wing plate rotary expansion to operating position by hinge.The present invention can provide the wing plate of continuous-stable to launch kinestate, conveniently realizes the dynamic debugging of equipment;The test data stabilization that commissioning device obtains, repeatability is preferably;Shortening the combined test cycle of equipment, work efficiency is improved.
Description
Technical field
The present invention relates to a kind of electrodynamic analogy expanding unit.
Background technology
Ground-testing plant, when ground experiment, should be debugged by rotary expansion wing plate in advance, in order to obtains in advance and sets
Standby corresponding performance parameter.In existing rotary expansion wing plate ground-testing plant, electrodynamic analogy is not yet set and launches dress
Put.In the early stage of ground-testing plant is debugged, rotate by folded state when storing merely with manually completing wing plate
The work of deployed condition when expanding into normal work, therefore, during the combined test of ground-testing plant, deposits
In many deficiencies:
The most it is not provided that the kinestate of continuous-stable, it is impossible to realize the dynamic debugging of ground-testing plant;
2., in the debugging stage, the data discrete that test obtains is excessive, and cannot reappear;
3. the cycle of equipment combined test is long, inefficiency.
According to interconnection internet retrieval result, do not find the rotary expansion wing plate ground-testing plant electrodynamic analogy of similar structures
Expanding unit.
Summary of the invention
In order to overcome the deficiencies in the prior art, the present invention provides a kind of rotary expansion wing plate ground-testing plant electrodynamic analogy
Expanding unit, solves the combined test problem of rotary expansion wing plate ground-testing plant, optimizes the overall performance of equipment,
Reduce experimentation cost, improve the technical-economic index that equipment runs.
The technical solution adopted for the present invention to solve the technical problems is: include slider-crank mechanism O 〃 BA and trans
Four-bar mechanism O ' CBO 〃, described slider-crank mechanism O 〃 BA using hinge O 〃 as the fixing centre of gyration,
Described trans four-bar mechanism O ' CBO 〃 is using hinge O ' as the centre of gyration, and hinge O ' still rotates exhibition simultaneously
Open the centre of gyration of wing plate;Servomotor drives slide block A to move along the rail by feed screw nut, and slide block A passes through connecting rod
AB drives the crank BO 〃 of slider-crank mechanism to rotate around centre of gyration O 〃, and crank BO 〃 passes through hinge B with anti-
The connecting rod BC of formula four-bar mechanism connects, and then drives rocking bar CO ' D to rotate around centre of gyration O ', rocking bar CO '
D drives wing plate drive pin to rotate around centre of gyration O ', by wing plate rotary expansion to operating position by hinge D.
The invention has the beneficial effects as follows:
1) wing plate that can provide continuous-stable launches kinestate, conveniently realizes the dynamic debugging of equipment;
2) the test data stabilization that commissioning device obtains, repeatability is preferably;
3) compared with the dynamic debugging carried out with product, simplify debugging routine, reduce debugging cost;
4) shortening the combined test cycle of equipment, work efficiency is improved.
Accompanying drawing explanation
Fig. 1 is the principle schematic of electrodynamic analogy expanding unit;
Fig. 2 is pitman pin axial limit structure schematic diagram;
In figure, 1-connecting rod, 2-spacing ring, 3-axle, 4-divide lobe back-up ring, 5-connecting rod.
Detailed description of the invention
The present invention is further described with embodiment below in conjunction with the accompanying drawings, and the present invention includes but are not limited to following embodiment.
This device is arranged on rotary expansion wing plate ground-testing plant, utilizes driven by servomotor, by the rotary expansion wing
Plate is by the deployed condition that collapsed state when storing is normal work.
As it is shown in figure 1, the principle sketch of rotary expansion wing plate ground-testing plant electrodynamic analogy expanding unit, hinge O ',
O 〃 is two fixing centres of gyration of device, and this device is by slider-crank mechanism O 〃 BA and trans four-bar mechanism O '
CBO 〃 combines.When servomotor (not marking in figure) drives slide block A by feed screw nut, along guide rail H-H
Move along a straight line from left to right, by A0Move to A1Time, drive crank BO 〃 along counterclockwise around revolution through connecting rod AB
Center O 〃 rotates, and crank BO 〃 is connected with connecting rod BC by hinge B, and drives rocking bar CO ' D along clockwise
Rotate around centre of gyration O ', then driven wing plate drive pin to rotate around centre of gyration O ' by hinge D, wing plate is rotated
It is expanded to operating position.Centre of gyration O ' is the centre of gyration of rotary expansion wing plate.Letter mark subscript 0 generation in figure
The meter apparatus initial position when wing plate is in folded state, subscript 1 represents device when wing plate is in deployed condition
Final position.
Debugging needs according to equipment, by changing the control parameter of servomotor, slide block A can obtain different fortune
Row state and velocity variations rule, thus wing plate obtains corresponding running status when rotary expansion.
Running state parameter when master control system is by the wing plate rotary expansion loading rule parameter different from charger is entered
After row is appropriately combined, ground-testing plant is achieved with testing required various service datas.
The relation of each assembly relevant parameter:
The length of connecting rod: CO '=B O 〃
As it is shown in figure 1, this device uses the drive system that two kinds of four-bar mechanisms combine, the input of mechanism, output
Having uniqueness, the designing points of Tu Zhong mechanism each several part is described below:
1) structure of hinge is connected: as in figure 2 it is shown, hinge pin axial limiting mode uses split-type shaft block ring to tie
Structure, such as patent 201420503997.6 disclosure of that.
2) electrodynamic analogy expanding unit is combined by slider-crank mechanism O 〃 BA and trans four-bar mechanism O ' CBO 〃
Forming, the straight-line displacement input of slide block A becomes monotropic function between exporting with wing plate rotary expansion angle, i.e. corresponding position
Shifting relation has uniqueness.
3) ball screw assembly, of slide block A is driven to bear tension in the working region of wing plate rotary expansion.
The mechanism size of the embodiment of the present invention is as follows:
Centre of gyration O ' is the centre of gyration of rotary expansion wing plate.
The relative position of the connecting rod centre of gyration: X=310, Y=360.
Length of connecting rod: CO '=B O 〃=205mm, BC=353.6mm, BC=370mm, DO=82mm.
The relevant parameter that device is chosen is:
Slide block A stroke: A0A1=370mm;
Rocking bar CO ' D corner: ∠ C0O ' C1=90 °;
Hinge pin between connecting rod: diameter phi 25, axial limit structure uses split-type shaft block ring patent;
The feed screw nut of driving slide block A is: ball screw assembly, FF5010-5.
Claims (1)
1. a rotary expansion wing plate ground-testing plant electrodynamic analogy expanding unit, including slider-crank mechanism O 〃 BA and
Trans four-bar mechanism O ' CBO 〃, it is characterised in that: described slider-crank mechanism O 〃 BA is with hinge O 〃
As the fixing centre of gyration, described trans four-bar mechanism O ' CBO 〃 is using hinge O ' as the centre of gyration, same
Time hinge O ' or the centre of gyration of rotary expansion wing plate;Servomotor drives slide block A edge by feed screw nut
Guide rail moves, and slide block A drives the crank BO 〃 of slider-crank mechanism to turn around centre of gyration O 〃 by connecting rod AB
Dynamic, crank BO 〃 is connected with the connecting rod BC of trans four-bar mechanism by hinge B, and then drives rocking bar CO ' D
Rotating around centre of gyration O ', rocking bar CO ' D drives wing plate drive pin to turn around centre of gyration O ' by hinge D
Dynamic, by wing plate rotary expansion to operating position.
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CN201620197586.XU CN205719489U (en) | 2016-03-15 | 2016-03-15 | Rotary expansion wing plate ground-testing plant electrodynamic analogy expanding unit |
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CN201620197586.XU CN205719489U (en) | 2016-03-15 | 2016-03-15 | Rotary expansion wing plate ground-testing plant electrodynamic analogy expanding unit |
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Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
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CN106871747A (en) * | 2017-01-11 | 2017-06-20 | 北京理工大学 | The device that missile wing launches is tested under a kind of body multi-angle high rotational speeds |
CN106871748A (en) * | 2017-01-11 | 2017-06-20 | 北京理工大学 | For testing the turntable that missile wing launches under body multi-angle high rotational speeds |
CN109131836A (en) * | 2018-09-21 | 2019-01-04 | 北京宇航系统工程研究所 | A kind of mini folding steering engine structure automating repeat function |
CN115309196A (en) * | 2022-10-11 | 2022-11-08 | 季华实验室 | Turntable control method, device, equipment and storage medium |
CN115373433A (en) * | 2022-10-25 | 2022-11-22 | 季华实验室 | Turntable motion compensation method, device, equipment and storage medium |
-
2016
- 2016-03-15 CN CN201620197586.XU patent/CN205719489U/en active Active
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106871747A (en) * | 2017-01-11 | 2017-06-20 | 北京理工大学 | The device that missile wing launches is tested under a kind of body multi-angle high rotational speeds |
CN106871748A (en) * | 2017-01-11 | 2017-06-20 | 北京理工大学 | For testing the turntable that missile wing launches under body multi-angle high rotational speeds |
CN109131836A (en) * | 2018-09-21 | 2019-01-04 | 北京宇航系统工程研究所 | A kind of mini folding steering engine structure automating repeat function |
CN115309196A (en) * | 2022-10-11 | 2022-11-08 | 季华实验室 | Turntable control method, device, equipment and storage medium |
CN115309196B (en) * | 2022-10-11 | 2022-12-30 | 季华实验室 | Turntable control method, device, equipment and storage medium |
CN115373433A (en) * | 2022-10-25 | 2022-11-22 | 季华实验室 | Turntable motion compensation method, device, equipment and storage medium |
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