CN2225705Y - Electric liquid load simulator - Google Patents
Electric liquid load simulator Download PDFInfo
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- CN2225705Y CN2225705Y CN 95201542 CN95201542U CN2225705Y CN 2225705 Y CN2225705 Y CN 2225705Y CN 95201542 CN95201542 CN 95201542 CN 95201542 U CN95201542 U CN 95201542U CN 2225705 Y CN2225705 Y CN 2225705Y
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Abstract
The utility model relates to an electric liquid load simulator for simulating aerodynamic moment on the rudder surface of a flying vehicle and overcoming redundant force, which is composed of a base, a loading motor, an object motor and a sensor frame. The utility model is characterized in that a position synchronous motor is arranged between the base and the loading motor, so that the synchronous motor can be moved synchronously along with a loaded object; accordingly, position movement and loading which are commonly born by the loading motor can be respectively born by the synchronous motor and the loading motor, the loading motor only bears the loading task, and position disturbance which acts on the loading motor is close to zero, so that the influence of the redundant force can be eliminated, and the frequency span of a loading system can be enhanced. The utility model can enhance the loading precision of the load simulator and the accuracy of ground loading experiments.
Description
The utility model relates to a kind of electrohydraulic load simulator that is used for the suffered aerodynamic couple of simulated flight device rudder face, overcomes redundant force.
Load simulator is the charger of simulated flight device suffered aerodynamic couple of rudder face in flight course, is typical passive type force servo system.Redundant force is owing to be loaded the object active movement, produces at loading motor (oil cylinder) two load cavities and forces flow, forces pressure thereby produce, and is exactly redundant force by the power output of forcing pressure to produce, and the existence of redundant force has a strong impact on loading accuracy and system's frequency range.Redundant force is the function that is loaded the object rotating speed, and the value of the high more redundant force of speed that is loaded object is just big more.Thereby, overcoming redundant force is the key of load simulator design, existing overcome the load simulator redundant force and mainly take measures to overcome redundant force from hardware, as to loading parameters of hydraulic motor optimal design, double valves compensation scheme, latch plate correcting scheme etc., though certain effect is all arranged to overcoming redundant force, but all there is certain defective, still can not satisfies actual requirement.
The purpose of this utility model is that a kind of improved electrohydraulic load simulator that can overcome redundant force will be provided, and improves the loading accuracy of load simulator and the accuracy of ground loading experiment.
The technical solution of the utility model: between the loading motor of load simulator and support, introduce position synchronous compensation motor, when the carrying object motion, syncmotor one steering wheel is synchronized with the movement and makes that loading the motor corner approaches zero, act on the position disturbance that loads on the motor thereby eliminated, reached the purpose that overcomes redundant force.Because of the work corner that loads motor approaches zero, the cavity volume that loads motor is reduced, so the frequency range of loading system also is improved.
Enforcement of the present utility model is for the loading accuracy that improves load simulator, the accuracy that improves the ground loading experiment has important techniques to be worth and practical significance, and can be generalized in aircraft rudder surface loading and the naval vessel rudder face loading experiment, therefore social effect is widely arranged.
Below in conjunction with embodiment and accompanying drawing thereof the utility model is specified.
Fig. 1 is a structural representation of the present utility model.
Among the figure: 1 support, 2 pots, 3 sensor frames, 4 electrohydraulic servo valves, 5 syncmotors, 6 dead rings, 7 connectors, 8 shaft couplings, 9 shaft joints, 10 pots, 11 load motor, 12 electrohydraulic servo valves, 13 dead rings, 14 bearings, 15 aiding support covers, 16 torque sensors, 17 inertia dishes, 18 dead rings, 19 object motors, 20 electrohydraulic servo valves, 21 sensor frames, 22 pots.
As shown in Figure 1: the utility model comprises by support (1), load motor (11), object motor (19) and sensor frame (3,21) form, it is characterized in that at support (1) and load introducing position synchronous compensation motor (5) between the motor (11), in syncmotor (5), load motor (11), the object motor is equipped with electrohydraulic servo valve (4 on (19), 12,20) and dispose pot (2,10,22), pass through by dead ring (6) between syncmotor (5) and the loading motor (11), connector (7), shaft coupling (8) and shaft joint (9) setting-in mutually connect, and load between motor (11) and the object motor (19) by dead ring (13,18), bearing (14), aiding support cover (15), torque sensor (16) and inertia dish (17) setting-in mutually connect.When the carrying object motion, syncmotor (5) be loaded object (steering wheel) and be synchronized with the movement, make that loading motor (11) corner approaches zero, act on the position disturbance that loads on the motor (11) thereby eliminated, reach the requirement that overcomes redundant force, because of the work corner that loads motor (11) can significantly reduce (can reduce by 90%) than ordinary load motor, the cavity volume that loads motor (11) is also reduced, thereby improved the frequency range of loading system.
Claims (1)
1, a kind of electrohydraulic load simulator, it is made up of support (1), loading motor (11), object motor (19) and sensor frame (3,21), it is characterized in that at support (1) and load introducing position synchronous motor (5) between the motor (11), on syncmotor (5), loading motor (11), object motor (19), electrohydraulic servo valve (4,12,20) is housed and disposes pot (2,10,22).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 95201542 CN2225705Y (en) | 1995-01-28 | 1995-01-28 | Electric liquid load simulator |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 95201542 CN2225705Y (en) | 1995-01-28 | 1995-01-28 | Electric liquid load simulator |
Publications (1)
Publication Number | Publication Date |
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CN2225705Y true CN2225705Y (en) | 1996-04-24 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN 95201542 Expired - Fee Related CN2225705Y (en) | 1995-01-28 | 1995-01-28 | Electric liquid load simulator |
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CN (1) | CN2225705Y (en) |
Cited By (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102122135A (en) * | 2010-06-25 | 2011-07-13 | 北京理工大学 | Closed loop load rigidity changing device |
CN102175441A (en) * | 2011-01-28 | 2011-09-07 | 北京航空航天大学 | Load simulator based on series-parallel mechanism |
CN102589919A (en) * | 2012-02-29 | 2012-07-18 | 北京航空航天大学 | Load simulator based on follow-up moment load |
CN102654754A (en) * | 2012-04-18 | 2012-09-05 | 中国工程物理研究院总体工程研究所 | Method for detecting vibration control dynamic range by using load simulator and load simulator |
CN103048139A (en) * | 2012-12-19 | 2013-04-17 | 天津工程机械研究院 | Inertia load loading device for hydraulic motor test |
CN103413474A (en) * | 2013-08-08 | 2013-11-27 | 北京航空航天大学 | Servo mechanism load simulator |
CN103543641A (en) * | 2013-09-30 | 2014-01-29 | 中国人民解放军国防科学技术大学 | Steering engine hinge torque real-time dynamic loading device |
CN105045134A (en) * | 2015-05-25 | 2015-11-11 | 哈尔滨工业大学 | Double-friction-disk loading mechanism and bidirectional friction loading-type no-additional-torque electro-hydraulic load simulator employing same |
CN105159076A (en) * | 2015-08-24 | 2015-12-16 | 南京理工大学 | Fusion type adaptive robust-based electro-hydraulic load simulator force control method |
CN105206132A (en) * | 2014-06-03 | 2015-12-30 | 南京航空航天大学 | Double-motor active loading steering engine load simulator |
CN105865818A (en) * | 2016-03-29 | 2016-08-17 | 南京航空航天大学 | Dual-channel linear steering engine electric loading system |
CN106323618A (en) * | 2016-08-30 | 2017-01-11 | 北京交通大学 | Electric servo mechanism load simulation system and simulation method thereof |
CN106564617A (en) * | 2016-10-27 | 2017-04-19 | 北京实验工厂 | FLAP control plane loading device and function testing method |
CN106840725A (en) * | 2017-02-17 | 2017-06-13 | 北京航空航天大学 | A kind of servo control mechanism torque loading equipemtn |
CN113888926A (en) * | 2021-08-12 | 2022-01-04 | 北京精密机电控制设备研究所 | Electromechanical force servo load bearing platform |
-
1995
- 1995-01-28 CN CN 95201542 patent/CN2225705Y/en not_active Expired - Fee Related
Cited By (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102122135A (en) * | 2010-06-25 | 2011-07-13 | 北京理工大学 | Closed loop load rigidity changing device |
CN102122135B (en) * | 2010-06-25 | 2013-06-26 | 北京理工大学 | Closed loop load rigidity changing device |
CN102175441A (en) * | 2011-01-28 | 2011-09-07 | 北京航空航天大学 | Load simulator based on series-parallel mechanism |
CN102175441B (en) * | 2011-01-28 | 2012-07-25 | 北京航空航天大学 | Load simulator based on series-parallel mechanism |
CN102589919A (en) * | 2012-02-29 | 2012-07-18 | 北京航空航天大学 | Load simulator based on follow-up moment load |
CN102589919B (en) * | 2012-02-29 | 2014-04-02 | 北京航空航天大学 | Load simulator based on follow-up moment load |
CN102654754A (en) * | 2012-04-18 | 2012-09-05 | 中国工程物理研究院总体工程研究所 | Method for detecting vibration control dynamic range by using load simulator and load simulator |
CN103048139A (en) * | 2012-12-19 | 2013-04-17 | 天津工程机械研究院 | Inertia load loading device for hydraulic motor test |
CN103048139B (en) * | 2012-12-19 | 2018-01-16 | 天津工程机械研究院 | Inertia load loading device is used in a kind of hydraulic motor test |
CN103413474A (en) * | 2013-08-08 | 2013-11-27 | 北京航空航天大学 | Servo mechanism load simulator |
CN103543641A (en) * | 2013-09-30 | 2014-01-29 | 中国人民解放军国防科学技术大学 | Steering engine hinge torque real-time dynamic loading device |
CN103543641B (en) * | 2013-09-30 | 2016-03-16 | 中国人民解放军国防科学技术大学 | The real-time dynamic loading device of a kind of steering wheel hinge moment |
CN105206132A (en) * | 2014-06-03 | 2015-12-30 | 南京航空航天大学 | Double-motor active loading steering engine load simulator |
CN105045134B (en) * | 2015-05-25 | 2017-08-25 | 哈尔滨工业大学 | The bi-directional friction loaded type of double frictional disk load maintainers and the use mechanism is without Surplus Moment electrohydraulic load simulator |
CN105045134A (en) * | 2015-05-25 | 2015-11-11 | 哈尔滨工业大学 | Double-friction-disk loading mechanism and bidirectional friction loading-type no-additional-torque electro-hydraulic load simulator employing same |
CN105159076A (en) * | 2015-08-24 | 2015-12-16 | 南京理工大学 | Fusion type adaptive robust-based electro-hydraulic load simulator force control method |
CN105159076B (en) * | 2015-08-24 | 2018-01-05 | 南京理工大学 | Electrohydraulic load simulator force control method based on pattern of fusion ADAPTIVE ROBUST |
CN105865818A (en) * | 2016-03-29 | 2016-08-17 | 南京航空航天大学 | Dual-channel linear steering engine electric loading system |
CN106323618A (en) * | 2016-08-30 | 2017-01-11 | 北京交通大学 | Electric servo mechanism load simulation system and simulation method thereof |
CN106323618B (en) * | 2016-08-30 | 2019-01-22 | 北京交通大学 | Electric servomechanism load simulation system and its analogy method |
CN106564617A (en) * | 2016-10-27 | 2017-04-19 | 北京实验工厂 | FLAP control plane loading device and function testing method |
CN106840725A (en) * | 2017-02-17 | 2017-06-13 | 北京航空航天大学 | A kind of servo control mechanism torque loading equipemtn |
CN113888926A (en) * | 2021-08-12 | 2022-01-04 | 北京精密机电控制设备研究所 | Electromechanical force servo load bearing platform |
CN113888926B (en) * | 2021-08-12 | 2023-10-31 | 北京精密机电控制设备研究所 | Electromechanical power servo load table |
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Legal Events
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C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
C19 | Lapse of patent right due to non-payment of the annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |