CN204924610U - Probe carries on sends system to with model - Google Patents
Probe carries on sends system to with model Download PDFInfo
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- CN204924610U CN204924610U CN201520479410.9U CN201520479410U CN204924610U CN 204924610 U CN204924610 U CN 204924610U CN 201520479410 U CN201520479410 U CN 201520479410U CN 204924610 U CN204924610 U CN 204924610U
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Abstract
The utility model relates to a system field is sent to the space flight model, discloses a probe carries on sends system to with model, probe carries on sends system to with model includes: probe carrying device, probe carrying device set up in in the pressure vessel, the model feeder, the model feeder set up in in the pressure vessel, be used for with test model sends into and carries out the wind tunnel test in the flow field, a hydraulic system, hydraulic system set up in outside the pressure vessel, for the model feeder provides power. The problem of present probe carries on sends system to with model can not many position survey of fire hole of multi -angle data, degree of automation is not high is solved.
Description
Technical field
The utility model relates to aerospace model feeding system field, particularly a kind of probe-loading and model feeding system.
Background technology
Along with the development of industrial aerodynamics, probe-loading and model feeding system have been widely used in the fields such as Aero-Space, communications and transportation, automobile making.
In prior art, model can be delivered to assigned address and carry out wind tunnel test by probe-loading and model feeding system.
Present inventor, in the process realizing the embodiment of the present application technical scheme, at least finds to there is following technical matters in prior art:
Existing probe-loading and model feeding system, can not multi-angle multiposition ground measurement data, and need manual intervention when test data, automaticity is not high.
Utility model content
The purpose of this utility model is to provide a kind of probe-loading and model feeding system, and solving current probe-loading and model feeding system can not multi-angle multiposition measuring data, problem that automaticity is not high.
To achieve these goals, the utility model provides a kind of probe-loading and model feeding system, comprise pressure vessel and test model, described probe-loading and model feeding system comprise: probe-loading device, and described probe-loading device is arranged in described pressure vessel; Model feeder, described model feeder is arranged in described pressure vessel, carries out wind tunnel test for being sent in flow field by described test model; Hydraulic system, described hydraulic system is arranged at outside described pressure vessel, for described model feeder provides power; Control system, described set-up of control system is outside described pressure vessel, described control system is connected with described probe-loading device, model feeder, hydraulic system respectively, wherein, described control system controls described probe-loading device stream field data and tests, and control described hydraulic system for described model feeder power is provided, thus realize described test model to send in flow field to carry out wind tunnel test.
Further, described probe-loading and model feeding system also comprise, and described probe-loading device specifically comprises: probe; Transverse moving mechanism, described transverse moving mechanism is connected with described probe, for controlling described probe transverse shifting; Axial rotation motion mechanism, described axial rotation motion mechanism is connected with described probe, for controlling described probe axial-rotation.
Further, described probe-loading and model feeding system also comprise, and described model feeder specifically comprises: horizontal mobile mechanism, vertical lifting mechanism and angle of attack modified gear; Described hydraulic system specifically comprises: move horizontally hydraulic package, VTOL (vertical take off and landing) hydraulic package and angle of attack displacement hydraulic package, wherein, described movable hydraulic assembly is connected with horizontal mobile mechanism, for described horizontal mobile mechanism provides power, described horizontal mobile mechanism is made to control the motion of described test model horizontal direction; Described VTOL (vertical take off and landing) hydraulic package is connected with described vertical lifting mechanism, for described vertical lifting mechanism provides power, makes described vertical lifting mechanism control the motion of described test model vertical direction; Described angle of attack displacement hydraulic package is connected with described angle of attack modified gear, for described angle of attack modified gear provides power, makes described angle of attack modified gear control the conversion of described test model angle position.
Further, described probe-loading and model feeding system also comprise, the described hydraulic package that moves horizontally comprises and moves horizontally hydraulic efficiency servo-valve and move horizontally hydraulic cylinder, the described hydraulic efficiency servo-valve that moves horizontally is arranged on the first hydraulic pump, control pressure and the flow of hydraulic oil in described first hydraulic pump, the described hydraulic cylinder that moves horizontally is connected with described first hydraulic pump, for being mechanical energy by the hydraulic energy transfer in described first hydraulic pump; Described VTOL (vertical take off and landing) hydraulic package comprises VTOL (vertical take off and landing) hydraulic efficiency servo-valve and VTOL (vertical take off and landing) hydraulic cylinder, described VTOL (vertical take off and landing) hydraulic efficiency servo-valve is arranged on the second hydraulic pump, control pressure and the flow of hydraulic oil in described second hydraulic pump, described VTOL (vertical take off and landing) hydraulic cylinder is connected with described second hydraulic pump, for being mechanical energy by the hydraulic energy transfer in described second hydraulic pump; Described angle of attack displacement hydraulic package comprises angle of attack displacement hydraulic efficiency servo-valve and angle of attack displacement oil motor, described angle of attack displacement hydraulic efficiency servo-valve is arranged on the 3rd hydraulic pump, control pressure and the flow of hydraulic oil in described 3rd hydraulic pump, described angle of attack displacement oil motor is connected with described first hydraulic pump, for being mechanical energy by the hydraulic energy transfer in described 3rd hydraulic pump.
Further, described probe-loading and model feeding system also comprise, and described control system comprises: motion controller, operated from a distance computing machine; Wherein, described motion controller is connected with described operated from a distance compunication, and described operated from a distance computing machine makes described probe-loading device and the motion of described model feeder by controlling described motion controller.
Compared with prior art, the probe-loading that provides of the utility model and model feeding system have the following advantages and beneficial effect:
1, the probe-loading that provides of the present embodiment and model feeding system comprise two cover probe-loading devices, and probe-loading all can transverse shifting and axial-rotation location, carry out flow field data test with can realizing multi-angle multiposition, make test data more comprehensively, more accurate.
2, the model feeder in the present embodiment, by hydraulic-driven, driving force is large and registration is high, and avoids electromagnetic interference (EMI).
3, the probe-loading that provides of the present embodiment and model feeding system are provided with control system, probe is sent into flow-field test data by probe-loading device by control system, after test data reaches model test requirement, test model is tested according to the feeding flow field, path of formulating in advance by model feed mechanism, both execute-in-place can be passed through, also can carry out Long-distance Control, can realize many test routine planning, automaticity is high.
Accompanying drawing explanation
In order to be illustrated more clearly in the technical scheme in the embodiment of the present application, below the accompanying drawing that uses required in describing embodiment and Reference numeral are briefly described, apparently, accompanying drawing in the following describes is only the embodiment of the application, for those of ordinary skill in the art, under the prerequisite not paying creative work, other accompanying drawing can also be obtained according to the accompanying drawing provided.
The front view of the probe-loading that Fig. 1 provides for the utility model embodiment and model feeding system;
The side view of the probe-loading that Fig. 2 provides for the utility model embodiment and model feeding system;
The structural representation of the model feeder that Fig. 3 provides for the utility model embodiment.
Description of reference numerals:
1. probe-loading device 2. model feeder 3. hydraulic system 4. control system 5. pressure vessel 6. test model 11. probe 12. transverse moving mechanism 13. axial-rotation mechanism 21. horizontal mobile mechanism 22. vertical lifting mechanism 23. angle of attack modified gear 31. moves horizontally hydraulic cylinder 32. VTOL (vertical take off and landing) hydraulic cylinder 33. angle of attack displacement oil motor
Embodiment
The embodiment of the present application is by providing a kind of probe-loading and model feeding system, solving current probe-loading and model feeding system can not multiangular measurement data, problem that automaticity is not high, achieves multi-angle multiposition and carries out flow field data test and supermatic Systematical control.
In order to understand the technical scheme of the application better, below in conjunction with Figure of description and concrete embodiment, technique scheme is described in detail, the specific features being to be understood that in the utility model embodiment and embodiment is the detailed description to technical scheme, instead of the restriction to technical scheme, when not conflicting, the technical characteristic in the embodiment of the present application and embodiment can combine mutually.
Refer to Fig. 1 to Fig. 3, the utility model embodiment provides a kind of probe-loading and model feeding system, comprises pressure vessel 5 and test model 6, and described probe-loading and model feeding system comprise:
Probe-loading device 1, described probe-loading device 1 is arranged in described pressure vessel 5;
Model feeder 2, described model feeder 2 is arranged in described pressure vessel 5, carries out wind tunnel test for being sent in flow field by described test model 6;
Hydraulic system 3, described hydraulic system 3 is arranged at outside described pressure vessel 5, for described model feeder 2 provides power;
Control system 4, described control system 4 is arranged at outside described pressure vessel 5, described control system 4 is connected with described probe-loading device 1, model feeder 2, hydraulic system 3 respectively, wherein said control system 4 controls described probe-loading device 1 stream field data and tests, and control described hydraulic system 3 for described model feeder 2 power is provided, thus realize described test model 6 to send in flow field to carry out wind tunnel test.
Further, probe-loading device 1 comprises:
Probe 11;
Transverse moving mechanism 12, described transverse moving mechanism 12 is connected with described probe 11, for controlling described probe 11 transverse shifting;
Axial rotation motion mechanism 13, described axial rotation motion mechanism 13 is connected with described probe 11, for controlling described probe 11 axial-rotation.
Specifically, described transverse moving mechanism 12 and described axial-rotation mechanism 13 respectively by driven by servomotor, and control servomotor by control system 4, thus make described probe-loading device 1 realize the multipoint test of multi-angle.
Further, described model feeder 2 specifically comprises: horizontal mobile mechanism 21, vertical lifting mechanism 22 and angle of attack modified gear 23;
Described hydraulic system 3 specifically comprises: move horizontally hydraulic package, VTOL (vertical take off and landing) hydraulic package and angle of attack displacement hydraulic package,
Wherein, described in move horizontally hydraulic package and be connected with horizontal mobile mechanism 21, for described horizontal mobile mechanism 21 provides power, make described horizontal mobile mechanism 21 control the motion of described test model 6 horizontal direction; Described VTOL (vertical take off and landing) hydraulic package is connected with described vertical lifting mechanism 22, for described vertical lifting mechanism 22 provides power, makes described vertical lifting mechanism 22 control the motion of described test model 6 vertical direction; Described angle of attack displacement hydraulic package is connected with described angle of attack modified gear 23, for described angle of attack modified gear 23 provides power, makes described angle of attack modified gear 23 control the conversion of described test model 6 angle position.
Thus described test model 6 is sent in flow field by described model feeder 2 carry out wind tunnel test.
Further, the described hydraulic package that moves horizontally comprises and moves horizontally hydraulic efficiency servo-valve and move horizontally hydraulic cylinder 31, the described hydraulic efficiency servo-valve that moves horizontally is arranged on the first hydraulic pump, control pressure and the flow of hydraulic oil in described first hydraulic pump, the described hydraulic cylinder 31 that moves horizontally is connected with described first hydraulic pump, for being mechanical energy by the hydraulic energy transfer in described first hydraulic pump;
Described VTOL (vertical take off and landing) hydraulic package comprises VTOL (vertical take off and landing) hydraulic efficiency servo-valve and VTOL (vertical take off and landing) hydraulic cylinder 32, described VTOL (vertical take off and landing) hydraulic efficiency servo-valve is arranged on the second hydraulic pump, control pressure and the flow of hydraulic oil in described second hydraulic pump, described VTOL (vertical take off and landing) hydraulic cylinder 32 is connected with described second hydraulic pump, for being mechanical energy by the hydraulic energy transfer in described second hydraulic pump;
Described angle of attack displacement hydraulic package comprises angle of attack displacement hydraulic efficiency servo-valve and angle of attack displacement oil motor 33, described angle of attack displacement hydraulic efficiency servo-valve is arranged on the 3rd hydraulic pump, control pressure and the flow of hydraulic oil in described 3rd hydraulic pump, described angle of attack displacement oil motor 33 is connected with described first hydraulic pump, for being mechanical energy by the hydraulic energy transfer in described 3rd hydraulic pump.
Further, described control system comprises: motion controller, operated from a distance computing machine; Wherein, described operated from a distance computing machine, passes to described motion controller signal, makes described motion controller control the motion of described probe-loading device and described model feeder, thus realizes the wind tunnel test test of described test model.
Lower mask body introduces the operational process of probe-loading and model feeding system, first, the path of probe 11 and test model 6 can be planned by on-the-spot touch-screen or remote computer, triggered by external signal, to described motion controller signal, described motion controller controls the motion of probe-loading device 1 and model feeder 2, particularly, the motion controller of control system 4 controls the motion of servomotor, thus make probe-loading device 1 that probe 11 is sent into flow-field test data, after test data reaches testing requirements, then the motion of motion controller hydraulic control system 3, hydraulic system 3 is made to produce power, and then test model 6 is carried out wind tunnel test test by model feeder 2 according in the feeding flow field, path of formulating.
Compared with prior art, the probe-loading that provides of the utility model and model feeding system have the following advantages and beneficial effect:
1, the probe-loading that provides of the present embodiment and model feeding system comprise two cover probe-loading devices, and probe-loading all can transverse shifting and axial-rotation location, multi-angle multiposition can be realized and carry out flow field data test, make test data more comprehensively, more accurate.
2, the model feeder in the present embodiment, by hydraulic-driven, driving force is large and registration is high, and avoids electromagnetic interference (EMI).
3, the probe-loading that provides of the present embodiment and model feeding system are provided with control system, probe is sent into flow-field test data by probe-loading device by control system, after test data reaches model test requirement, test model is tested according to the feeding flow field, path of formulating in advance by model feed mechanism, both can pass through execute-in-place, also can carry out Long-distance Control, many test routine planning can be realized, one key starts, and automaticity is high.
Obviously, those skilled in the art can carry out various change and modification to the utility model and not depart from spirit and scope of the present utility model.Like this, if these amendments of the present utility model and modification belong within the scope of the utility model claim and equivalent technologies thereof, then the utility model is also intended to comprise these change and modification.
Claims (6)
1. probe-loading and a model feeding system, comprise pressure vessel and test model, it is characterized in that, described probe-loading and model feeding system comprise:
Probe-loading device, described probe-loading device is arranged in described pressure vessel;
Model feeder, described model feeder is arranged in described pressure vessel, carries out wind tunnel test for being sent in flow field by described test model;
Hydraulic system, described hydraulic system is arranged at outside described pressure vessel, for described model feeder provides power;
Control system, described set-up of control system is outside described pressure vessel, and described control system is connected with described probe-loading device, model feeder, hydraulic system respectively;
Wherein, described control system controls described probe-loading device stream field data and tests, and controls described hydraulic system for described model feeder and provide power, thus realizes described test model to send in flow field to carry out wind tunnel test.
2. probe-loading according to claim 1 and model feeding system, is characterized in that, described probe-loading device specifically comprises:
Probe;
Transverse moving mechanism, described transverse moving mechanism is connected with described probe, for controlling described probe transverse shifting;
Axial rotation motion mechanism, described axial rotation motion mechanism is connected with described probe, for controlling described probe axial-rotation.
3. probe-loading according to claim 1 and model feeding system, is characterized in that, described model feeder specifically comprises: horizontal mobile mechanism, vertical lifting mechanism and angle of attack modified gear;
Described hydraulic system specifically comprises: move horizontally hydraulic package, VTOL (vertical take off and landing) hydraulic package and angle of attack displacement hydraulic package, wherein, the described hydraulic package that moves horizontally is connected with horizontal mobile mechanism, for described horizontal mobile mechanism provides power, described horizontal mobile mechanism is made to control the motion of described test model horizontal direction; Described VTOL (vertical take off and landing) hydraulic package is connected with described vertical lifting mechanism, for described vertical lifting mechanism provides power, makes described vertical lifting mechanism control the motion of described test model vertical direction; Described angle of attack displacement hydraulic package is connected with described angle of attack modified gear, for described angle of attack modified gear provides power, makes described angle of attack modified gear control the conversion of described test model angle position.
4. probe-loading according to claim 3 and model feeding system, it is characterized in that, the described hydraulic package that moves horizontally comprises and moves horizontally hydraulic efficiency servo-valve and move horizontally hydraulic cylinder, the described hydraulic efficiency servo-valve that moves horizontally is arranged on the first hydraulic pump, control pressure and the flow of hydraulic oil in described first hydraulic pump, the described hydraulic cylinder that moves horizontally is connected with described first hydraulic pump, for being mechanical energy by the hydraulic energy transfer in described first hydraulic pump;
Described VTOL (vertical take off and landing) hydraulic package comprises VTOL (vertical take off and landing) hydraulic efficiency servo-valve and VTOL (vertical take off and landing) hydraulic cylinder, described VTOL (vertical take off and landing) hydraulic efficiency servo-valve is arranged on the second hydraulic pump, control pressure and the flow of hydraulic oil in described second hydraulic pump, described VTOL (vertical take off and landing) hydraulic cylinder is connected with described second hydraulic pump, for being mechanical energy by the hydraulic energy transfer in described second hydraulic pump;
Described angle of attack displacement hydraulic package comprises angle of attack displacement hydraulic efficiency servo-valve and angle of attack displacement oil motor, described angle of attack displacement hydraulic efficiency servo-valve is arranged on the 3rd hydraulic pump, control pressure and the flow of hydraulic oil in described 3rd hydraulic pump, described angle of attack displacement oil motor is connected with described first hydraulic pump, for being mechanical energy by the hydraulic energy transfer in described 3rd hydraulic pump.
5. probe-loading according to claim 1 and model feeding system, is characterized in that, described control system comprises: motion controller, operated from a distance computing machine;
Wherein, described motion controller is connected with described operated from a distance compunication, and described operated from a distance computing machine makes described probe-loading device and the motion of described model feeder by controlling described motion controller.
6. probe-loading according to claim 1 and model feeding system, is characterized in that, described system comprises two cover probe-loading devices.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520479410.9U CN204924610U (en) | 2015-07-06 | 2015-07-06 | Probe carries on sends system to with model |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520479410.9U CN204924610U (en) | 2015-07-06 | 2015-07-06 | Probe carries on sends system to with model |
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| Publication Number | Publication Date |
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| CN204924610U true CN204924610U (en) | 2015-12-30 |
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| CN201520479410.9U Active CN204924610U (en) | 2015-07-06 | 2015-07-06 | Probe carries on sends system to with model |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112577707A (en) * | 2020-12-29 | 2021-03-30 | 中国航天空气动力技术研究院 | Impulse wind tunnel air-breathing type engine push resistance measurement test system |
| CN115371999A (en) * | 2022-10-24 | 2022-11-22 | 中国航发四川燃气涡轮研究院 | Inlet flow field parameter measuring device in high-temperature and high-pressure test |
-
2015
- 2015-07-06 CN CN201520479410.9U patent/CN204924610U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112577707A (en) * | 2020-12-29 | 2021-03-30 | 中国航天空气动力技术研究院 | Impulse wind tunnel air-breathing type engine push resistance measurement test system |
| CN115371999A (en) * | 2022-10-24 | 2022-11-22 | 中国航发四川燃气涡轮研究院 | Inlet flow field parameter measuring device in high-temperature and high-pressure test |
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| GR01 | Patent grant |