CN104518542A - Cell-type riding lawn mower - Google Patents

Cell-type riding lawn mower Download PDF

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Publication number
CN104518542A
CN104518542A CN201310460178.XA CN201310460178A CN104518542A CN 104518542 A CN104518542 A CN 104518542A CN 201310460178 A CN201310460178 A CN 201310460178A CN 104518542 A CN104518542 A CN 104518542A
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CN
China
Prior art keywords
solar panel
battery pack
management system
supply management
power
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.)
Pending
Application number
CN201310460178.XA
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Chinese (zh)
Inventor
孙云红
冉沅忠
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Positec Power Tools Suzhou Co Ltd
Original Assignee
Positec Power Tools Suzhou Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Positec Power Tools Suzhou Co Ltd filed Critical Positec Power Tools Suzhou Co Ltd
Priority to CN201310460178.XA priority Critical patent/CN104518542A/en
Publication of CN104518542A publication Critical patent/CN104518542A/en
Pending legal-status Critical Current

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Abstract

The invention relates to a cell-type riding lawn mower comprising a body and a cell pack mounted on the body. A seat is provided on the body. The cell-type riding lawn mower is characterized by further comprising supports, a solar panel and a power management system, the supports are connected to the body, the solar panel is fixed onto the supports and higher than the seat, the solar panel is used for shielding the seat from sunlight, and the power management system is mounted on the body and connected with the solar panel and the cell pack respectively. According to the arrangement, the solar panel arranged upon the seat by the aid of the supports functions in shielding sunlight and rain for the operator, and under control of the power management system, the solar panel automatically charges the cell pack according to actual needs at any moment.

Description

Battery type riding cropper
Technical field
The present invention relates to hay mover field, particularly relate to a kind of battery type riding cropper.
Background technology
As the instrument on the finishing lawn be suitable for rapidly and efficiently, hay mover is extensive in applications such as urban afforestation and family's weedings.The hay mover carrying battery pack can be divided into battery type hand-push type mower and battery type riding cropper.Battery type riding cropper is than battery type hand-push type mower, more convenient to use and comfortable, and operating personnel only need be sitting on hay mover can complete the work such as urban afforestation and family's weeding.
But battery type riding cropper needs when not using for a long time to be regularly batteries charging, with battery maintenance group, prevents battery pack from causing automatic discharging to cause battery pack to lose efficacy because not charging for a long time.Meanwhile, current battery type riding cropper does not generally possess the function of sun-shading rain-proof, and operating personnel may be subject to burning sun and rain water mitigation when the work of use battery type riding cropper.
Summary of the invention
Based on this, be necessary to provide a kind of and automatically can provide the battery type riding cropper of sun-shading rain-proof function for batteries charging.
A kind of battery type riding cropper, comprise fuselage main body and the battery pack being installed on described fuselage main body, described fuselage main body is provided with seat, it is characterized in that, described battery type riding cropper also comprises bracing frame, solar panel and power-supply management system, support frame as described above is connected to described fuselage main body, described solar panel is fixed on support frame as described above, and the height of described solar panel is greater than the height of described seat, described solar panel is used for keeping the sun off and irradiates described seat, described power-supply management system is installed on described fuselage main body, and described power-supply management system is connected to described solar panel and battery pack,
Described power-supply management system detects the dump energy of described battery pack automatically, when power-supply management system detects the dump energy of battery pack lower than default minimum, described power-supply management system controls solar panel to batteries charging, when power-supply management system detects the dump energy of battery pack higher than default peak, described power-supply management system controls solar panel to be stopped to batteries charging.
Wherein in an embodiment, described solar panel is rectangular configuration, and support frame as described above is provided with 4 altogether, and described 4 bracing frames are connected to 4 corner positions of the solar panel of described rectangular configuration.
Wherein in an embodiment, support frame as described above is the cylindrical of hollow.
Wherein in an embodiment, described power-supply management system is connected to described solar panel by wire, and the described wire for connecting power-supply management system and solar battery group is placed in the inside of the cylindrical support frame of described hollow.
Wherein in an embodiment, described solar panel is parallel to the bottom of described fuselage main body.
Wherein in an embodiment, the distance between described solar panel and described seat is 1.1 ~ 1.3 meters.
Wherein in an embodiment, described power-supply management system comprises microcontroller and electronic switch, and described microcontroller is connected to described battery pack and electronic switch, and described electronic switch is connected between solar panel and battery pack;
Described microcontroller detects the dump energy of described battery pack automatically, when microcontroller detects the dump energy of battery pack lower than default minimum, and described microprocessor controls electronic switch closes, now solar panel is to batteries charging; When microcontroller detects the dump energy of battery pack higher than default peak, described microprocessor controls electronic switch disconnects, and now solar panel stops to batteries charging.
Wherein in an embodiment, described power-supply management system also comprises diode, described diode is connected between described electronic switch and battery pack, and the positive pole pin of described diode is connected by the positive pole of described electronic switch with described solar panel, the negative pole pin of described diode is connected with the positive pole of described battery pack.
Wherein in an embodiment, described battery type riding cropper also comprises sectioned housing, described sectioned housing is positioned at the bottom of described fuselage main body, and described sectioned housing is connected to described battery pack, and described battery pack provides operating voltage for described sectioned housing.
Wherein in an embodiment, described sectioned housing is mounted on the bottom of described fuselage main body by two connecting rods, and described connecting rod is connected with height regulating rod, and described height regulating rod adjusts the height of described sectioned housing by controlling described connecting rod.
Above-mentioned battery type riding cropper, its solar panel be arranged on above seat by bracing frame can be operating personnel's sun-shading rain-proof, and simultaneously under the control of power-supply management system, solar panel can at any time as required from trend batteries charging.
Accompanying drawing explanation
Fig. 1 is the structural representation of the battery type riding cropper of an embodiment;
Fig. 2 is the schematic diagram of the charging control circuit of an embodiment.
Battery type riding cropper 100 seat 112 fuselage main body 110
Battery pack 120 bracing frame 130 solar panel 140
Power-supply management system 150 microcontroller 152 electronic switch 154
Diode 156 sectioned housing 160 connecting rod 170
Height regulating rod 180
Embodiment
In order to solve current battery formula riding cropper do not possess the function of sun-shading rain-proof and its battery pack because of can not the problem that lost efficacy of automatic charging and causing in time, present embodiments provide for a kind of battery type riding cropper.Below in conjunction with specific embodiment, battery type riding cropper is specifically described.
Please refer to Fig. 1, the battery type riding cropper 100 that present embodiment provides, comprises fuselage main body 110, is installed on the battery pack 120 of fuselage main body 110, the seat 112 be arranged in fuselage main body 110, bracing frame 130, solar panel 140 and power-supply management system 150.
Bracing frame 130 is connected in fuselage main body 110.Bracing frame 130 is mainly used in support solar cell panel 140.In the present embodiment, solar panel 140 is rectangular configuration, bracing frame 130 is provided with altogether 4, these 4 bracing frames 130 are arranged on around seat 112, and be connected to 4 corner positions of the solar panel 140 of rectangular configuration, such solar panel 140 just can be horizontally fixed on the top of seat 112, thus is embodied as the function of the operating personnel's sun-shading rain-proof be sitting on seat 112.
In order to ensure that operating personnel can be seated comfortably on seat 112, solar panel 140 should exceed seat 112 certain altitude.According to the height that general adult sits down, the distance between solar panel 140 and seat 112 is set to 1.1 ~ 1.3 meters.
Power-supply management system 150 is arranged in fuselage main body 110, and power-supply management system 150 is connected to solar panel 140 and battery pack 120.Power-supply management system 150 can detect the dump energy of battery pack 120 automatically, when power-supply management system 150 detects the dump energy of battery pack 120 lower than default minimum, power-supply management system 150 just can control solar panel 140 and charge to battery pack 120; And when power-supply management system 150 detects the dump energy of battery pack 120 higher than default peak, power-supply management system 150 just can control solar panel 140 to be stopped charging to battery pack 120.
Because power-supply management system 150 is mounted in fuselage main body 110, and solar panel 140 distance fuselage main body 110 1 segment distance, therefore also need to use wire connecting power management system 150 and solar panel 140.Seem neat and artistic to make whole battery type riding cropper 100, in the present embodiment, what bracing frame 130 adopted is the cylindrical structural of hollow, and is just placed in the inside of the cylindrical support frame 130 of this hollow for connecting power-supply management system 150 and the wire of solar panel 140.
Please refer to Fig. 2, further, in the present embodiment, power-supply management system 150 mainly comprises microcontroller 152 and electronic switch 154.Microcontroller 152 is connected to battery pack 120 and electronic switch 154, and electronic switch 154 is connected between solar panel 140 and battery pack 120.
Microcontroller 152 can detect the dump energy of battery pack 120 automatically, when microcontroller 152 detects the dump energy of battery pack 120 lower than default minimum, microcontroller 152 just can control electronic switch 154 and close, and now solar panel 140 charges to battery pack 120.And when microcontroller 152 detects the dump energy of battery pack 120 higher than default peak, microcontroller 152 just can control electronic switch 154 and disconnect, now solar panel 140 stops charging to battery pack 120.
In order to improve the fail safe that solar panel 140 charges to battery pack 120, in the present embodiment, power-supply management system 150 also comprises diode 156.Diode 156 is connected between electronic switch 154 and battery pack 120, and the positive pole pin of diode 156 is connected by the positive pole of electronic switch 154 with solar panel 140, and the negative pole pin of diode 156 is connected with the positive pole of battery pack 120.Diode 156 can improve the fail safe that solar panel 140 charges to battery pack 120 and be mainly reflected in following aspect:
According to the connection of above-mentioned diode 156 in charging control circuit, based on diode 156 unilateral conduction we know, only have when battery pack 120 according to correct polarity access charging control circuit time, solar panel 140 just understand charge to battery pack 120; Otherwise cell panel 140 can not charge to battery pack 120, thus ensure that battery pack 120 polarity causes improper consequence when wrong.
In addition, the battery type riding cropper 100 that present embodiment provides also comprises the sectioned housing 160 for mowing.Sectioned housing 160 is positioned at the bottom of fuselage main body 110, and sectioned housing 160 is connected to battery pack 120.Such battery pack 120 just can provide operating voltage for sectioned housing 160.
In order to make sectioned housing 160 select cutting-height, the sectioned housing 160 that makes in present embodiment can need freely to adjust height according to reality cutting.Adjustment principle brief description is as follows:
Sectioned housing 160 is mounted on the bottom of fuselage main body 110 by two connecting rods 170, and the bottom of such two connecting rods 170, sectioned housing 160 and fuselage main body 110 can be formed one " structure of parallelogram ".Connecting rod 170 is connected with height regulating rod 180.So only need control height regulating rod 180, make height regulating rod 180 pull connecting rod 170 above-mentioned " structure of parallelogram " can be produced distortion, thus change the height of sectioned housing 160.After sectioned housing 160 adjusts height, as long as fix height regulating rod 180 to make that connecting rod 170 is fixing just can make above-mentioned " structure of parallelogram " to stablize, thus sectioned housing 160 is stabilized in current location.
Above-mentioned battery type riding cropper 100, it can be operating personnel's sun-shading rain-proof by bracing frame 130 solar panel 140 be arranged on above seat 112, simultaneously under the control of power-supply management system 150, solar panel 140 can charge from trend battery pack 120 at any time as required.
The above embodiment only have expressed several execution mode of the present invention, and it describes comparatively concrete and detailed, but therefore can not be interpreted as the restriction to the scope of the claims of the present invention.It should be pointed out that for the person of ordinary skill of the art, without departing from the inventive concept of the premise, can also make some distortion and improvement, these all belong to protection scope of the present invention.Therefore, the protection range of patent of the present invention should be as the criterion with claims.

Claims (10)

1. a battery type riding cropper, comprise fuselage main body and the battery pack being installed on described fuselage main body, described fuselage main body is provided with seat, it is characterized in that, described battery type riding cropper also comprises bracing frame, solar panel and power-supply management system, support frame as described above is connected to described fuselage main body, described solar panel is fixed on support frame as described above, and the height of described solar panel is greater than the height of described seat, described solar panel is used for keeping the sun off and irradiates described seat, described power-supply management system is installed on described fuselage main body, and described power-supply management system is connected to described solar panel and battery pack,
Described power-supply management system detects the dump energy of described battery pack automatically, when power-supply management system detects the dump energy of battery pack lower than default minimum, described power-supply management system controls solar panel to batteries charging, when power-supply management system detects the dump energy of battery pack higher than default peak, described power-supply management system controls solar panel to be stopped to batteries charging.
2. battery type riding cropper according to claim 1, it is characterized in that, described solar panel is rectangular configuration, and support frame as described above is provided with 4 altogether, and described 4 bracing frames are connected to 4 corner positions of the solar panel of described rectangular configuration.
3. battery type riding cropper according to claim 2, is characterized in that, support frame as described above is the cylindrical of hollow.
4. battery type riding cropper according to claim 3, it is characterized in that, described power-supply management system is connected to described solar panel by wire, and the described wire for connecting power-supply management system and solar battery group is placed in the inside of the cylindrical support frame of described hollow.
5. battery type riding cropper according to claim 1, is characterized in that, described solar panel is parallel to the bottom of described fuselage main body.
6. battery type riding cropper according to claim 5, is characterized in that, the distance between described solar panel and described seat is 1.1 ~ 1.3 meters.
7. battery type riding cropper according to claim 1, it is characterized in that, described power-supply management system comprises microcontroller and electronic switch, and described microcontroller is connected to described battery pack and electronic switch, and described electronic switch is connected between solar panel and battery pack;
Described microcontroller detects the dump energy of described battery pack automatically, when microcontroller detects the dump energy of battery pack lower than default minimum, and described microprocessor controls electronic switch closes, now solar panel is to batteries charging; When microcontroller detects the dump energy of battery pack higher than default peak, described microprocessor controls electronic switch disconnects, and now solar panel stops to batteries charging.
8. battery type riding cropper according to claim 7, it is characterized in that, described power-supply management system also comprises diode, described diode is connected between described electronic switch and battery pack, and the positive pole pin of described diode is connected by the positive pole of described electronic switch with described solar panel, the negative pole pin of described diode is connected with the positive pole of described battery pack.
9. the battery type riding cropper according to claim arbitrary in claim 1 to 8, it is characterized in that, described battery type riding cropper also comprises sectioned housing, described sectioned housing is positioned at the bottom of described fuselage main body, and described sectioned housing is connected to described battery pack, described battery pack provides operating voltage for described sectioned housing.
10. battery type riding cropper according to claim 9, it is characterized in that, described sectioned housing is mounted on the bottom of described fuselage main body by two connecting rods, described connecting rod is connected with height regulating rod, and described height regulating rod adjusts the height of described sectioned housing by controlling described connecting rod.
CN201310460178.XA 2013-09-30 2013-09-30 Cell-type riding lawn mower Pending CN104518542A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201310460178.XA CN104518542A (en) 2013-09-30 2013-09-30 Cell-type riding lawn mower

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201310460178.XA CN104518542A (en) 2013-09-30 2013-09-30 Cell-type riding lawn mower

Publications (1)

Publication Number Publication Date
CN104518542A true CN104518542A (en) 2015-04-15

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CN201310460178.XA Pending CN104518542A (en) 2013-09-30 2013-09-30 Cell-type riding lawn mower

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Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1483306A (en) * 2002-11-22 2004-03-24 石萌达 Mower trolley for lawn
CN101359838A (en) * 2008-09-11 2009-02-04 武汉日新科技照明有限公司 High performance series photovoltaic control system
CN102334400A (en) * 2011-06-23 2012-02-01 宁波大叶园林设备有限公司 Riding mower with noise reduction measure and hydraulic stepless speed change
CN102358195A (en) * 2011-09-18 2012-02-22 王成艳 Solar charging type electric bicycle
CN102403888A (en) * 2011-11-25 2012-04-04 常熟开关制造有限公司(原常熟开关厂) Photovoltaic grid connected inverter with reverse connection prevention function and control method therefor

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1483306A (en) * 2002-11-22 2004-03-24 石萌达 Mower trolley for lawn
CN101359838A (en) * 2008-09-11 2009-02-04 武汉日新科技照明有限公司 High performance series photovoltaic control system
CN102334400A (en) * 2011-06-23 2012-02-01 宁波大叶园林设备有限公司 Riding mower with noise reduction measure and hydraulic stepless speed change
CN102358195A (en) * 2011-09-18 2012-02-22 王成艳 Solar charging type electric bicycle
CN102403888A (en) * 2011-11-25 2012-04-04 常熟开关制造有限公司(原常熟开关厂) Photovoltaic grid connected inverter with reverse connection prevention function and control method therefor

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Application publication date: 20150415