CN209553555U - A kind of aircraft power system experimental bench - Google Patents
A kind of aircraft power system experimental bench Download PDFInfo
- Publication number
- CN209553555U CN209553555U CN201920176155.9U CN201920176155U CN209553555U CN 209553555 U CN209553555 U CN 209553555U CN 201920176155 U CN201920176155 U CN 201920176155U CN 209553555 U CN209553555 U CN 209553555U
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- China
- Prior art keywords
- storage battery
- holding chamber
- experimental bench
- control panel
- stage body
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Abstract
The utility model discloses a kind of aircraft power system experimental benches, including stage body, holding chamber, storage battery, direct current supply disk and alarm, the center position of the stage body bottom is equipped with holding chamber, bottom end inside holding chamber is equipped with hollow out spring support, center position inside the hollow out spring support is equipped with temperature inductor, storage battery is equipped with inside the holding chamber of the hollow out elasticity seating face, fastening spring is all fixed at corner location at the top of the holding chamber, center position at the top of the stage body is equipped with master control panel, side at the top of master control panel is equipped with equidistant switch button, master control panel surface below the switch button is equipped with manipulation frame, center position inside manipulation frame is equipped with single-chip microcontroller.The utility model not only realizes experimental bench to the temperature control regulatory function of storage battery, realizes experimental bench to the protection fastening function of battery, and improves convenience degree when experimental bench uses.
Description
Technical field
The utility model relates to experimental bench technical field, specially a kind of aircraft power system experimental bench.
Background technique
Aircraft refers to advancing by self power driving with wing, a tool or more tool engines, can be in space or atmosphere
In itself density be greater than air aircraft, usually need in the emulation experiment of aircraft using experimental bench.
Such experimental bench on market today is many kinds of, can satisfy the use demand of people substantially, but still deposits
In certain problem, particular problem has the following:
1, traditional such experimental bench is general when in use is not arranged temperature control regulatory function to storage battery, thus serious shortening
The service life of experimental bench；
2, traditional such experimental bench is general when in use is not arranged protection fastening function to storage battery, to greatly influence
Safety when experimental bench uses；
3, traditional such experimental bench is general not convenient enough when in use when in use, so that the use to people is brought
Very big puzzlement.
Utility model content
The purpose of this utility model is to provide a kind of aircraft power system experimental benches, to solve to mention in above-mentioned background technique
Experimental bench adjusts the problem not enough facilitated when in use with protection fastening function and experimental bench to the not set temperature control of storage battery out.
To achieve the above object, the utility model provides the following technical solutions: a kind of aircraft power system experimental bench, including
The center position of stage body, holding chamber, storage battery, direct current supply disk and alarm, the stage body bottom is equipped with holding chamber, holding chamber
Internal bottom end is equipped with hollow out spring support, and the center position inside the hollow out spring support is equipped with temperature inductor, institute
It states and is equipped with storage battery inside the holding chamber of hollow out elasticity seating face, be all fixed with fastening bullet at the corner location at the top of the holding chamber
Spring, one end that fastening spring is located remote from indoor side wall is fixed with L-type clamp, and L-type clamp is closely connect with storage battery, and described
Center position at the top of body is equipped with master control panel, and the side at the top of master control panel is equipped with equidistant switch button, described to open
It closes the master control panel surface below button and manipulation frame is installed, manipulate the center position inside frame and single-chip microcontroller is installed, and is single
The input terminal of piece machine is electrically connected with the output end of switch button and temperature inductor respectively, the platform of master control panel side
Body surface face is equipped with feeding pannel, and the surface of feeding pannel is separately installed with emergency service disk, direct current supply disk and Alternating Current Power Supply disk,
And the center position of emergency service disk, direct current supply disk and Alternating Current Power Supply panel surface is all equipped with indicator light, and urgent confession
The input terminal of electroplax, direct current supply disk and Alternating Current Power Supply disk is electrically connected with the output end of storage battery respectively, the indicator light it is defeated
The output end for entering end and single-chip microcontroller is electrically connected.
Preferably, the stage body surface of the holding chamber two sides is all equipped with storage chamber, and storage is hinged on the inner sidewall of storage chamber
Object door body, while handle is fixed on the lateral wall of storing door body one end.
Preferably, cooling fan is all installed inside the holding chamber of the storage battery two sides, and the input terminal of cooling fan with
The output end of storage battery is electrically connected, and the input terminal of cooling fan and the output end of single-chip microcontroller are electrically connected, while the width of storage battery is small
Cover board is hinged in the distance between adjacent heat radiation blower, and in the placement chamber interior walls of storage battery side.
Preferably, the surface of the manipulation frame is fixed with display, and the output end of the input terminal of display and storage battery electricity
Connection, the input terminal of display and the output end of single-chip microcontroller are electrically connected.
Preferably, the stage body surface below the master control panel is equipped with emergency panel.
Preferably, the master control panel is equipped with alarm far from the stage body surface of feeding pannel side, and alarm is defeated
The output end for entering end and single-chip microcontroller is electrically connected.
Compared with prior art, the utility model has the beneficial effects that the aircraft power system experimental bench not only realizes
Experimental bench realizes experimental bench to the protection fastening function of battery to the temperature control regulatory function of storage battery, and improves experimental bench
Convenience degree when use；
1, temperature inductor is installed by center position inside hollow out spring support, inside the holding chamber of storage battery two sides
Cooling fan is installed, and by installing alarm far from the stage body surface of feeding pannel side in master control panel, realizes experimental bench
To the temperature control regulatory function of storage battery, to extend the service life of experimental bench；
2, by fastening spring fixed at the corner location at the top of holding chamber, fastening spring is located remote from indoor side wall
L-type clamp is fixed in one end, and installs hollow out spring support by the bottom end inside holding chamber, realizes protection of the experimental bench to battery
Fastening function, to improve safety when experimental bench uses；
3, equidistant switch button is set by the side at the top of master control panel, and by emergency service disk, direct current
Feeding pannel and the center position of Alternating Current Power Supply panel surface install indicator light, realize instruction function when experimental bench uses,
To improve convenience degree when experimental bench uses.
Detailed description of the invention
Fig. 1 is the schematic cross-sectional view of the utility model；
Fig. 2 is the schematic view of the front view of the utility model；
Fig. 3 is the holding chamber enlarged structure schematic diagram of the utility model；
Fig. 4 is the system frame structure schematic diagram of the utility model.
In figure: 1, stage body；2, holding chamber；3, storage battery；4, storage chamber；5, storing door body；6, feeding pannel；7, emergency service
Disk；8, direct current supply disk；9, Alternating Current Power Supply disk；10, indicator light；11, switch button；12, frame is manipulated；13, single-chip microcontroller；14, main
Control panel；15, alarm；16, emergency panel；17, cover board；18, display；19, hollow out spring support；20, temperature inductor；
21, cooling fan；22, fastening spring；23, L-type clamp.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
Fig. 1-4 is please referred to, a kind of embodiment provided by the utility model: a kind of aircraft power system experimental bench, including platform
The center position of body 1, holding chamber 2, storage battery 3, direct current supply disk 8 and alarm 15,1 bottom of stage body is equipped with holding chamber 2, places
1 surface of stage body of 2 two sides of room is all equipped with storage chamber 4, and storing door body 5, while storing door body are hinged on the inner sidewall of storage chamber 4
It is fixed with handle on the lateral wall of 5 one end, is worked for storing, the bottom end inside holding chamber 2 is equipped with hollow out spring support 19, engraves
Center position inside empty spring support 19 is equipped with temperature inductor 20, and the model of the temperature inductor 20 can be M344830,
It is equipped with storage battery 3 inside the holding chamber 2 on 19 surface of hollow out spring support, cooling fan is all installed inside the holding chamber 2 of 3 two sides of storage battery
21, the model of the cooling fan 21 can be YWF4E-300S, and the input terminal of cooling fan 21 and the output end of storage battery 3 are electrically connected
It connects, the input terminal of cooling fan 21 and the output end of single-chip microcontroller 13 are electrically connected, while the width of storage battery 3 is less than adjacent heat radiation wind
The distance between machine 21, and it is hinged with cover board 17 on 2 inner wall of holding chamber of 3 side of storage battery, for work of radiating, holding chamber 2
Fastening spring 22 is all fixed at the corner location at top, one end that fastening spring 22 is located remote from 2 inner sidewall of room is fixed with L-type
Clamp 23, and L-type clamp 23 is closely connect with storage battery 3, the center position at 1 top of stage body is equipped with master control panel 14, master control face
The side at 14 top of plate is equipped with equidistant switch button 11, and 14 surface of master control panel of 11 lower section of switch button is equipped with manipulation
Frame 12 manipulates the center position inside frame 12 and is equipped with single-chip microcontroller 13, and the model of the single-chip microcontroller 13 can be SH69P25, and single
The input terminal of piece machine 13 is electrically connected with the output end of switch button 11 and temperature inductor 20 respectively, manipulates the surface of frame 12
It is fixed with display 18, the model of the display 18 can be LKSC021, and the output end of the input terminal of display 18 and storage battery 3
Electrical connection, the input terminal of display 18 and the output end of single-chip microcontroller 13 are electrically connected, for showing work, 14 lower section of master control panel
1 surface of stage body be equipped with emergency panel 16, be used for emergency, 1 surface of stage body of 14 side of master control panel is equipped with feeding pannel
6, the surface of feeding pannel 6 is separately installed with emergency service disk 7, direct current supply disk 8 and Alternating Current Power Supply disk 9, and emergency service disk
7, the input terminal of direct current supply disk 8 and Alternating Current Power Supply disk 9 is electrically connected with the output end of storage battery 3 respectively, emergency service disk 7, straight
Stream feeding pannel 8 and the center position on 9 surface of Alternating Current Power Supply disk are all equipped with indicator light 10, and the model of the indicator light 10 can be
HR-2PE-LT, and the output end of the input terminal of indicator light 10 and single-chip microcontroller 13 is electrically connected, master control panel 14 is far from feeding pannel 6
1 surface of stage body of side is equipped with alarm 15, and the model of the alarm 15 can be FU-JS001, and the input terminal of alarm 15
It is electrically connected with the output end of single-chip microcontroller 13, works for failure warning.
Working principle: in use, storage battery 3 is placed on 19 surface of hollow out spring support, is being put by opening cover board 17 first
It pushes the movement of L-type clamp 23 to be clamped protection by the fastening spring 22 at 2 top of holding chamber during setting, closes later
Cover board 17 makes it in the mutual of single-chip microcontroller 13 and storage battery 3 later by the switch button 11 of operation 14 top side of master control panel
Promote emergency service disk 7, direct current supply disk 8 and Alternating Current Power Supply disk 9 to be powered use under cooperation, leads to during use
The indicator light 10 crossed at 9 centre of surface position of urgent feeding pannel 7, direct current supply disk 8 and Alternating Current Power Supply disk is indicated, to increase
Add convenience degree when use, passes through the temperature inductor 20 at 19 inner hub location of hollow out spring support when storage battery 3 uses
Temperature detection is carried out, and the result that will test is delivered to inside single-chip microcontroller 13,3 two sides holding chamber 2 of storage battery is controlled by single-chip microcontroller 13
Internal cooling fan 21 radiates, while the alarm 15 for controlling 1 surface of stage body is alarmed, to maintain in holding chamber 2
Constant, the service life of extension storage battery 3 of portion's temperature, completes the use work of experimental bench.
It is obvious to a person skilled in the art that the present invention is not limited to the details of the above exemplary embodiments, and
And without departing substantially from the spirit or essential attributes of the utility model, it can realize that this is practical new in other specific forms
Type.Therefore, in all respects, the present embodiments are to be considered as illustrative and not restrictive, this is practical new
The range of type is indicated by the appended claims rather than the foregoing description, it is intended that containing for the equivalent requirements of the claims will be fallen in
All changes in justice and range are embraced therein.It should not treat any reference in the claims as limiting
Related claim.
Claims (6)
1. a kind of aircraft power system experimental bench, including stage body (1), holding chamber (2), storage battery (3), direct current supply disk (8) and report
Alert device (15), it is characterised in that: the center position of stage body (1) bottom is equipped with holding chamber (2), holding chamber (2) inside
Bottom end is equipped with hollow out spring support (19), and the internal center position of the hollow out spring support (19) is equipped with temperature inductor
(20), storage battery (3) are equipped with inside the holding chamber (2) on hollow out spring support (19) surface, the turning at the top of the holding chamber (2)
It is all fixed at position fastening spring (22), one end that fastening spring (22) is located remote from room (2) inner sidewall is fixed with L-type clamp
(23), and L-type clamp (23) is closely connect with storage battery (3), and the center position at the top of the stage body (1) is equipped with master control panel
(14), the side at the top of master control panel (14) is equipped with equidistant switch button (11), the master below the switch button (11)
Control panel (14) surface is equipped with manipulation frame (12), and the internal center position of manipulation frame (12) is equipped with single-chip microcontroller (13), and
The input terminal of single-chip microcontroller (13) is electrically connected with the output end of switch button (11) and temperature inductor (20) respectively, the master
Stage body (1) surface of control panel (14) side is equipped with feeding pannel (6), and the surface of feeding pannel (6) is separately installed with emergency service
Disk (7), direct current supply disk (8) and Alternating Current Power Supply disk (9), and emergency service disk (7), direct current supply disk (8) and exchange supply
The input terminal of electroplax (9) is electrically connected with the output end of storage battery (3) respectively, the emergency service disk (7), direct current supply disk (8) with
And the center position on Alternating Current Power Supply disk (9) surface is all equipped with indicator light (10), and the input terminal and monolithic of indicator light (10)
The output end of machine (13) is electrically connected.
2. a kind of aircraft power system experimental bench according to claim 1, it is characterised in that: holding chamber (2) two sides
Stage body (1) surface be all equipped with storage chamber (4), be hinged on the inner sidewall of storage chamber (4) storing door body (5), while storing door
Handle is fixed on the lateral wall of body (5) one end.
3. a kind of aircraft power system experimental bench according to claim 1, it is characterised in that: storage battery (3) two sides
It is all equipped with cooling fan (21) inside holding chamber (2), and the input terminal of cooling fan (21) and the output end of storage battery (3) are electrically connected
It connects, the input terminal of cooling fan (21) and the output end of single-chip microcontroller (13) are electrically connected, while the width of storage battery (3) is less than adjacent
The distance between cooling fan (21), and cover board (17) are hinged on holding chamber (2) inner wall of storage battery (3) side.
4. a kind of aircraft power system experimental bench according to claim 1, it is characterised in that: the table of manipulation frame (12)
Face is fixed with display (18), and the input terminal of display (18) is electrically connected with the output end of storage battery (3), display (18) it is defeated
The output end for entering end and single-chip microcontroller (13) is electrically connected.
5. a kind of aircraft power system experimental bench according to claim 1, it is characterised in that: under the master control panel (14)
Stage body (1) surface of side is equipped with emergency panel (16).
6. a kind of aircraft power system experimental bench according to claim 1, it is characterised in that: the master control panel (14) is remote
Stage body (1) surface from feeding pannel (6) side is equipped with alarm (15), and the input terminal of alarm (15) and single-chip microcontroller (13)
Output end be electrically connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920176155.9U CN209553555U (en) | 2019-02-01 | 2019-02-01 | A kind of aircraft power system experimental bench |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920176155.9U CN209553555U (en) | 2019-02-01 | 2019-02-01 | A kind of aircraft power system experimental bench |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209553555U true CN209553555U (en) | 2019-10-29 |
Family
ID=68310262
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920176155.9U Expired - Fee Related CN209553555U (en) | 2019-02-01 | 2019-02-01 | A kind of aircraft power system experimental bench |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209553555U (en) |
-
2019
- 2019-02-01 CN CN201920176155.9U patent/CN209553555U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20191029 Termination date: 20220201 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |