CN205418128U - Portable starting drive of helicopter - Google Patents
Portable starting drive of helicopter Download PDFInfo
- Publication number
- CN205418128U CN205418128U CN201620211371.9U CN201620211371U CN205418128U CN 205418128 U CN205418128 U CN 205418128U CN 201620211371 U CN201620211371 U CN 201620211371U CN 205418128 U CN205418128 U CN 205418128U
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- Prior art keywords
- helicopter
- cell module
- super capacitance
- capacitance cell
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Abstract
The utility model provides a portable starting drive of helicopter, include: a housing. Place in the casing, adopt to establish ties and/or parallelly connected mode links together and saves the super capacity battery module of electric energy by polylith capacity battery monomer, every capacity battery monomer includes anodal post and negative pole post, and free anodal post of adjacent capacity battery and the free negative pole post of adjacent capacity battery all adopt the connection piece to connect, the setting is in outside the casing, connect the anodal total positive strap of super capacitor battery module, the setting is in outside the casing, connect total negative pole connection piece of super capacitor battery module negative pole, total positive strap with total negative pole connection piece is ear formula structure, respectively with total positive strap with the output port of external output electric energy is connected to total negative pole connection piece. The device can directly be used for starting the circular telegram checksum power of helicopter, compares with conventional starting drive, can carry at random, provides the power guarantee during for the daily flight of helicopter.
Description
Technical field
This utility model relates to power supply technical field, is specifically related to a kind of portable starter of helicopter.
Background technology
Along with development and the raising of living standards of the people of society, helicopter has stepped in the life of people.But when helicopter needs carry out energising inspection or cause helicopter-mounted battery discharge reduced capability owing to outdoor temperature is too low, then need a kind of portable airborne starting device helicopter can being powered or helicopter-mounted battery is started.
Utility model content
In view of this, this utility model provides a kind of portable starter of helicopter, and this device can be directly used for the energising inspection to helicopter and power initiation, can carry at random, provides power supply guarantee during flight daily for helicopter.
For achieving the above object, the following technical scheme of this utility model offer:
A kind of portable starter of helicopter, including:
Housing；
It is placed in described housing, polylith capacitor batteries monomer links together and store the super capacitance cell module of electric energy；Each capacitor batteries monomer includes positive terminal and negative terminal, and the positive terminal of adjacent capacitor battery cell and the negative terminal of adjacent capacitor battery cell all use connection sheet to connect；
It is arranged on outside described housing, connects total positive strap of described super capacitance cell module positive pole；
Being arranged on outside described housing, connect total negative straps of described super capacitance cell module negative pole, described total positive strap and described total negative straps are ear formula structure；
It is connected with described total negative straps with described total positive strap respectively and externally exports the output port of electric energy.
Preferably, described connection sheet is hollow out conduction aluminium sheet or hollow out conductive copper plate.
Preferably, described super capacitance cell module is made up of 36 pieces of capacitor batteries monomers.
Preferably, described housing includes the medial surface being coated with the clathrum inwardly emptied and be made up of stiffener.
Preferably, described output port includes:
The control relay being connected with described total negative straps with described total positive strap respectively；
It is arranged on the first power supply interface and the second power supply interface being connected to described control relay outside described housing that helicopter is powered.
Preferably, also include: be connected to be charged described super capacitance cell module controlling and the control detector of monitoring parameter with described super capacitance cell module.
Preferably, also include: with the display that described control detector is connected to show described super capacitance cell module duty.
Preferably, also include:
It is connected with described control detector and described display, the alarm reported to the police occurs when described super capacitance cell module duty exception.
Preferably, also include: be connected with described control detector and described super capacitance cell module, detect and control in described super capacitance cell module the balance controller of voltage difference between each capacitor batteries monomer.
Preferably, also include:
The power supply adaptor being connected with described super capacitance cell module and super capacitance cell module is charged.
Based on technique scheme, the portable starter of helicopter that this utility model provides, by arranging jumbo super capacitance cell module, and total positive strap and total negative straps are set on the positive pole and negative pole of super capacitance cell module, externally exported electric energy by output port, the power initiation and the energising that are directly used in helicopter check；Meanwhile, in this utility model, capacitor batteries monomer capacitance is big, and multiple capacitor batteries monomers use series connection and parallel way central combination to become super capacitance cell module, and by super capacitance cell module, control detector, display, alarm, being arranged on enclosure interior in the part set such as balance controller, enclosure interior spatial design is reasonable, makes the portable starter of helicopter have and fills speed electricity soon, volume is little, lightweight, it is convenient for carrying, the simple advantage of Operation and Maintenance；Finally, by using hollow type connect sheet and be coated with the clathrum inwardly emptied and be made up of stiffener in case inside face, the weight of the portable starter of helicopter is significantly reduced, it is achieved that the lightness of device.
Accompanying drawing explanation
In order to be illustrated more clearly that this utility model embodiment or technical scheme of the prior art, the accompanying drawing used required in embodiment or description of the prior art will be briefly described below, apparently, accompanying drawing in describing below is only embodiment of the present utility model, for those of ordinary skill in the art, on the premise of not paying creative work, it is also possible to obtain other accompanying drawing according to the accompanying drawing provided.
The structural representation of the super capacitance cell module that Fig. 1 provides for this utility model；
The structural representation that the portable starter of helicopter that Fig. 2 provides for this utility model is overall；
The case inside face structural representation that Fig. 3 provides for this utility model；
The structural representation of the power supply adaptor that Fig. 4 provides for this utility model.
Detailed description of the invention
Below in conjunction with the accompanying drawing in this utility model embodiment, the technical scheme in this utility model embodiment is clearly and completely described, it is clear that described embodiment is only a part of embodiment of this utility model rather than whole embodiments.Based on the embodiment in this utility model, the every other embodiment that those of ordinary skill in the art are obtained under not making creative work premise, broadly fall into the scope of this utility model protection.
Refer to the structural representation of the super capacitance cell module that Fig. 1 to Fig. 2, Fig. 1 show that this utility model provides；Fig. 2 shows the structural representation that the portable starter of helicopter that this utility model provides is overall.This utility model provides a kind of portable starter of helicopter, mainly includes housing 1 and super capacitance cell module 2.Super capacitance cell module 2 is linked together to realize the purpose of increase-volume supercharging by polylith capacitor batteries monomer by the way of series connection and/or parallel connection, simultaneously constitutes the energy bag of a storage electric energy with larger capacity.It is internal that super capacitance cell module 2 is placed on housing 1, and wherein every piece of capacitor batteries monomer all includes positive terminal and negative terminal.Adjacent two pieces of capacitor batteries monomers are mainly attached by connection sheet 3.Concrete, connect sheet 3 and connect the positive terminal of adjacent two pieces of capacitor batteries monomers or connect the negative terminal of adjacent capacitor battery cell.The series connection between multiple capacitor batteries monomer and parallel connection is realized by connecting sheet 3.
The positive terminal of capacitor batteries monomer uses integral type machine add-on type with capacitor batteries monomer shell, after each capacitor batteries monomer is by connecting sheet connection, on the one hand capacitor batteries monomer positive terminal uses as electrode, and the retention mechanism on the one hand fixed each other as capacitor batteries monomer uses.
Super capacitance cell module in the present embodiment is made up of 36 pieces of capacitor batteries monomers, and each capacitor batteries monomer is cylindrical 2.3V/40Ah super capacitance cell.
Connecting sheet 3 and use hollow out conduction aluminium sheet or hollow out conductive copper plate, thickness is 3mm, in the case of not reducing current-carrying capacity, reduces the overall weight of super capacitance cell module to greatest extent.
The positive pole of super capacitance cell module uses total positive strap 4 to connect, and the negative pole of super capacitance cell module uses total negative straps 5 to connect.Total positive strap 4 uses ear formula design and extend to outside housing with total negative straps 5.
Total positive strap 4 is jointly connected the output port that can externally export electric energy with total negative straps 5, helicopter can be powered by connecting cable or start by output port, makes total positive strap 4 and total negative straps 5 simultaneously as the bindiny mechanism between super capacitance cell module and helicopter charging inlet.Concrete, output port includes controlling relay the 6, first power supply interface 7 and the second power supply interface 8.Controlling relay 6 to be connected with total positive strap 4 and total negative straps 5, the first power supply interface 7 and the second power supply interface 8 are arranged on outside housing 1 and are connected with controlling relay 6.The wherein corresponding total positive strap 4 of the first power supply interface 7, the corresponding total negative straps 5 of the second power supply interface 8.
This utility model also include mating with helicopter for adapter helicopter being powered and start.Adapter includes that input connector and out connector, input connector and the first power supply interface 7 connect, and out connector and the second power supply interface 8 connect.On housing 1, the first power supply interface 7 is different with prompting user's polarity with the position labelling different colours of the second power supply interface 8, first power supply interface 7 and the second power supply interface 8 use concave-convex design simultaneously, remind user's the first power supply interface 7 and the difference of the second power supply interface 8 polarity further, prevent from being mistakenly inserted.
Refer to Fig. 3, Fig. 3 and show case inside face structural representation.The housing 1 of accommodating super capacitance cell module 2 includes lateral surface and medial surface 9, is coated with the clathrum 10 inwardly emptied and be made up of stiffener at medial surface 9.Use clathrum 10 design can realize being greatly reduced of case weight by local material reducing and by the way of leaving stiffener on the basis of not affecting housing load bearing stength.
The portable starter of helicopter that this utility model provides also has automatic control function, concrete, also includes controlling detector 11.Controlling detector 11 to be connected with super capacitance cell module 2, super capacitance cell module 2 carries out data acquisition, data store and judge from motion tracking, and realize charge and discharge control and data monitoring in super capacitance cell module charge and discharge process.
Control detector 11 can also connect a display 12, be used for showing super capacitance cell module 2 duty and running parameter.The such as discharge and recharge time, operating temperature, the information such as charging process, charging complete.
Control detector 11 and display 12 can also connect an alarm 13, alarm 13 can be made up of display lamp and buzzer, when detecting that super capacitance cell module 2 exists fault, display lamp, buzzer and display 12 can be passed through and carry out alarm indicator, such as temperature alarming shows, capacitor batteries monomer over voltage alarm shows.
In order to adjust between super capacitance cell module the voltage difference between each capacitor batteries monomer in real time, controlling to connect on detector 11 and super capacitance cell module 2 balance controller 14.Detected by balance controller 14 and control in super capacitance cell module voltage difference between each capacitor batteries monomer.
This utility model also includes and the power supply adaptor 15 of super capacitance cell module 2 adaptation, sees the structural representation of the power supply adaptor that Fig. 4, Fig. 4 show that this utility model provides.Power supply adaptor 15 is utilized can super capacitance cell module 2 to be charged.Super capacitance cell module can be charged by the power supply adaptor in the present embodiment by external alternating current 220V power supply.
Control detector 11 and can directly control the charging modes of super capacitance cell module, concrete, can control to use the charging modes of constant voltage after first constant current, output voltage can be by voltage feedback loop between 15～32.5V, output electric current is between 0-100A, output voltage and output electric current all can carry out pre-adjustment by controlling detector, and the total voltage controlling final charging is not more than 60 minutes total time at zone of reasonableness and charging.
The portable starter of helicopter that this utility model provides, by arranging jumbo super capacitance cell module, and total positive strap and total negative straps are set on the positive pole and negative pole of super capacitance cell module, externally exported electric energy by output port, the energising inspection and the starter that are directly used in helicopter start.Meanwhile, in this utility model, capacitor batteries monomer capacitance is big, and multiple capacitor batteries monomers use series connection and parallel way central combination to become super capacitance cell module, and by super capacitance cell module, control detector, display, alarm, being arranged on enclosure interior in the part set such as balance controller, enclosure interior spatial design is reasonable, makes the portable starter of helicopter have charging rate fast, volume is little, lightweight, it is convenient for carrying, the simple advantage of Operation and Maintenance.Finally, by using hollow type connect sheet and be coated with the clathrum inwardly emptied and be made up of stiffener in case inside face, the weight of the portable starter of helicopter is significantly reduced, it is achieved that lightness.
Described above to the disclosed embodiments, makes professional and technical personnel in the field be capable of or uses this utility model.Multiple amendment to these embodiments will be apparent from for those skilled in the art, and generic principles defined herein can realize in the case of without departing from spirit or scope of the present utility model in other embodiments.Therefore, this utility model is not intended to be limited to the embodiments shown herein, and is to fit to the widest scope consistent with principles disclosed herein and features of novelty.
Claims (10)
1. the portable starter of helicopter, it is characterised in that including:
Housing；
It is placed in described housing, polylith capacitor batteries monomer links together and store the super capacitance cell module of electric energy；Each capacitor batteries monomer includes positive terminal and negative terminal, and the positive terminal of adjacent capacitor battery cell and the negative terminal of adjacent capacitor battery cell all use connection sheet to connect；
It is arranged on outside described housing, connects total positive strap of described super capacitance cell module positive pole；
Being arranged on outside described housing, connect total negative straps of described super capacitance cell module negative pole, described total positive strap and described total negative straps are ear formula structure；
It is connected with described total negative straps with described total positive strap respectively and externally exports the output port of electric energy.
The portable starter of helicopter the most according to claim 1, it is characterised in that described connection sheet is hollow out conduction aluminium sheet or hollow out conductive copper plate.
The portable starter of helicopter the most according to claim 1, it is characterised in that described super capacitance cell module is made up of 36 pieces of capacitor batteries monomers.
The portable starter of helicopter the most according to claim 1, it is characterised in that described housing includes the medial surface being coated with the clathrum inwardly emptied and be made up of stiffener.
The portable starter of helicopter the most according to claim 1, it is characterised in that described output port includes:
The control relay being connected with described total negative straps with described total positive strap respectively；
It is arranged on the first power supply interface and the second power supply interface being connected to described control relay outside described housing that helicopter is powered.
The portable starter of helicopter the most according to claim 1, it is characterised in that also include: be connected to be charged described super capacitance cell module controlling and the control detector of monitoring parameter with described super capacitance cell module.
The portable starter of helicopter the most according to claim 6, it is characterised in that also include: be connected to show the display of described super capacitance cell module duty with described control detector.
The portable starter of helicopter the most according to claim 7, it is characterised in that also include:
It is connected with described control detector and described display, the alarm reported to the police occurs when described super capacitance cell module duty exception.
The portable starter of helicopter the most according to claim 6, it is characterized in that, also include: be connected with described control detector and described super capacitance cell module, detect and control in described super capacitance cell module the balance controller of voltage difference between each capacitor batteries monomer.
The portable starter of helicopter the most according to claim 1, it is characterised in that also include:
The power supply adaptor being connected with described super capacitance cell module and super capacitance cell module is charged.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620211371.9U CN205418128U (en) | 2016-03-11 | 2016-03-11 | Portable starting drive of helicopter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620211371.9U CN205418128U (en) | 2016-03-11 | 2016-03-11 | Portable starting drive of helicopter |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205418128U true CN205418128U (en) | 2016-08-03 |
Family
ID=56519323
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620211371.9U Expired - Fee Related CN205418128U (en) | 2016-03-11 | 2016-03-11 | Portable starting drive of helicopter |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205418128U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106160117A (en) * | 2016-08-23 | 2016-11-23 | 四川长虹电源有限责任公司 | A kind of dynamic power system for helicopter and control method thereof |
| CN118040852A (en) * | 2024-04-12 | 2024-05-14 | 新乡北方车辆仪表有限公司 | Portable starting power supply of helicopter with invariable initial starting voltage |
-
2016
- 2016-03-11 CN CN201620211371.9U patent/CN205418128U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106160117A (en) * | 2016-08-23 | 2016-11-23 | 四川长虹电源有限责任公司 | A kind of dynamic power system for helicopter and control method thereof |
| CN106160117B (en) * | 2016-08-23 | 2018-07-24 | 四川长虹电源有限责任公司 | A kind of dynamic power system and its control method for helicopter |
| CN118040852A (en) * | 2024-04-12 | 2024-05-14 | 新乡北方车辆仪表有限公司 | Portable starting power supply of helicopter with invariable initial starting voltage |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160803 Termination date: 20190311 |