CN104153928A - Device and method for starting unmanned aerial vehicle - Google Patents

Device and method for starting unmanned aerial vehicle Download PDF

Info

Publication number
CN104153928A
CN104153928A CN201410339725.3A CN201410339725A CN104153928A CN 104153928 A CN104153928 A CN 104153928A CN 201410339725 A CN201410339725 A CN 201410339725A CN 104153928 A CN104153928 A CN 104153928A
Authority
CN
China
Prior art keywords
unmanned plane
starting
starter
aerial vehicle
unmanned aerial
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
CN201410339725.3A
Other languages
Chinese (zh)
Inventor
史国虎
张先为
于志路
崔涛
董一宏
李新锋
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.)
SHANDONG ZHENG-YUAN DIGITAL CITY CONSTRUCTION Co Ltd
Original Assignee
SHANDONG ZHENG-YUAN DIGITAL CITY CONSTRUCTION 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 SHANDONG ZHENG-YUAN DIGITAL CITY CONSTRUCTION Co Ltd filed Critical SHANDONG ZHENG-YUAN DIGITAL CITY CONSTRUCTION Co Ltd
Priority to CN201410339725.3A priority Critical patent/CN104153928A/en
Publication of CN104153928A publication Critical patent/CN104153928A/en
Pending legal-status Critical Current

Links

Abstract

The invention relates to a device and a method for starting an unmanned aerial vehicle. The device comprises a starting disc and a starter. The starting disc is mounted on the top of a head of the unmanned aerial vehicle, a groove is formed in the middle of the starting disc, and two notches which are symmetrical with each other about the center of the groove are formed in the wall of the groove; the starter comprises handles, a starting shaft, a motor casing, a connecting disc and a starting switch, the handles are arranged on two sides of the motor casing, the connecting disc is mounted at the upper end of the motor casing, a motor is mounted in the motor casing, the starting shaft is fixed onto a rotary shaft of the motor, and a fixing rod is arranged on the starting shaft. The method includes clamping the fixing rod of the starter on the starting disc of the unmanned aerial vehicle; pushing the starting switch; separating the starter from the head of the unmanned aerial vehicle when the rotation speed of the head of the unmanned aerial vehicle reaches a takeoff value. The device and the method for starting the unmanned aerial vehicle have the advantages that the device is simple in structure and convenient to operate, only the fixing rod on the starting shaft needs to be clamped on the starting disc of the head of the unmanned aerial vehicle when the unmanned aerial vehicle is about to be started, the starting success rate is high, consumption of a large quantity of time can be omitted, and the cost is low.

Description

A kind of unmanned plane starting drive and method
Technical field
The present invention relates to unmanned plane design field, particularly relate to a kind of unmanned plane starting drive and method.
Background technique
Unmanned plane because its volume is little, cost is low, easy to operate, be widely used in life, production and military affairs flexibly.Unmanned plane start-up course is complicated, conventionally need to expend larger manpower and materials, and during startup, success rate is low.The startup of existing unmanned plane coordinates with head front end by starter conventionally, makes starter drive head rotating.Starter front end is provided with rotary head conventionally, and the front end of rotary head is provided with rubber sleeve, during startup, rubber sleeve is aimed to the propeller cowling on unmanned plane head, starts starter, and rotary head drives propeller cavitation to rotate.During due to startup, rotating speed is very fast, and rubber sleeve and the propeller cowling of starter easily depart from, and because frictional force is larger, the two contact position can produce a large amount of heats, and rubber sleeve very easily damages, and replacement cost is high, very inconvenient.
As can be seen here, above-mentioned existing a kind of unmanned plane starting drive and method, in structure and use, obviously still have inconvenience and defect, and are urgently further improved.How to found a kind of simple in structure, be difficult for departing from head while starting, without often changing the new unmanned plane starter of accessory, real one of the current important research and development problem that belongs to.
Summary of the invention
The technical problem to be solved in the present invention is to provide a kind of unmanned plane starting drive and method, make that it is simple in structure, while starting starter be difficult for departing from head, without often changing accessory, thereby the rubber sleeve and the propeller cowling that overcome existing starter easily depart from, rubber sleeve very easily damages, the deficiency that replacement cost is high.
For solving the problems of the technologies described above, the invention provides a kind of unmanned plane starting drive, comprise boot disk and starter, described boot disk is arranged on unmanned plane head top, the centre of boot disk is provided with groove, has two about the centrosymmetric notch of groove on the cell wall of groove; Described starter comprises handle, starts axle, motor casing, land and enable switch, described handle is located at the both sides of motor casing, land is arranged on the upper end of motor casing, in described motor casing, motor is installed, described startup axle is fixedly mounted in the rotating shaft of motor, starts axle and is provided with fixing rod.
Further, described notch is inclined notch.
Described fixing rod is double-screw bolt.
Described enable switch is arranged on handle top.
The present invention also provides a kind of method of using above-mentioned unmanned plane starting drive, the fixing rod of described starter is stuck in the boot disk of unmanned plane, presses enable switch, and when the rotating speed of unmanned plane head reaches the value of taking off, starter departs from unmanned plane head.
Further, the inrush current of described starter is greater than 100A.
Adopt after such design, the present invention at least has the following advantages:
Starting drive of the present invention is simple in structure, easy to operate, during startup, only the fixing rod starting on axle need be stuck in the boot disk of unmanned plane head, can open starter, after unmanned plane successfully starts, under the centrifugal action that starter can produce when starting, depart from unmanned plane head, start-up course is fast, and without expending the plenty of time, cost is low.
Starter and boot disk are difficult for departing from, and start success rate high.Time that rubber pad causes and waste on cost have been avoided changing.
The processing of boot disk is simple, only original head need be changed a little, and cost of production is low, simple to operate.
Accompanying drawing explanation
Above-mentioned is only the general introduction of technical solution of the present invention, and in order to better understand technological means of the present invention, below in conjunction with accompanying drawing and embodiment, the present invention is described in further detail.
Fig. 1 is the structural representation of boot disk of the present invention.
Fig. 2 is the side structure schematic diagram of boot disk of the present invention.
Fig. 3 is the structural representation of starter of the present invention.
Fig. 4 is the structural representation of startup axle of the present invention.
Embodiment
Shown in Fig. 1-4, the invention provides a kind of unmanned plane starting drive, comprise boot disk 1 and starter 2, described boot disk 1 is arranged on unmanned plane head top, the centre of boot disk 1 is provided with groove 11, has two about the centrosymmetric notch 12 of groove on the cell wall of groove 11; Described starter comprises handle 24, starts axle 21, motor casing 23 and land 22, described handle 24 is located at the both sides of motor casing 23, land 22 is arranged on the upper end of motor casing 23, in described motor casing 23, motor is installed, on starter, be also provided with enable switch 27, described startup axle 21 is fixedly mounted in the rotating shaft 27 of motor, starts axle and is provided with fixing rod 26.
Described notch 12 is inclined notch.
The cylindrical structural that described startup axle 21 is hollow, starts axle 21 upper ends and is provided with perforate, and fixing rod 26 is arranged in perforate, and described fixing rod 26 can be double-screw bolt.
Enable switch 27 is arranged on handle 24 tops.
The present invention also provides a kind of method that starts unmanned plane with said apparatus, first, the fixing rod of starter 26 is stuck in the boot disk 1 of unmanned plane head, hold with a firm grip the handle 24 of starter of both hands, then press enable switch 27, start axle 21 High Rotation Speed under the drive of motor, when rotating speed reaches the value of taking off, unmanned plane can take off smoothly, under the centrifugal action that starter can produce when starting, departs from unmanned plane head.
The motor of described starter is heavy-duty motor, and inrush current is greater than 100A.
Starting drive of the present invention can be used for the startup of piston aviation engine, has wide range of applications.
The above; it is only preferred embodiment of the present invention; not the present invention is done to any pro forma restriction, those skilled in the art utilize the technology contents of above-mentioned announcement to make a little simple modification, equivalent variations or modification, all drop in protection scope of the present invention.

Claims (6)

1. a unmanned plane starting drive, is characterized in that: comprise boot disk and starter, described boot disk is arranged on unmanned plane head top, and the centre of boot disk is provided with groove, has two about the centrosymmetric notch of groove on the cell wall of groove; Described starter comprises handle, starts axle, motor casing, land and enable switch, described handle is located at the both sides of motor casing, land is arranged on the upper end of motor casing, in described motor casing, motor is installed, described startup axle is fixedly mounted in the rotating shaft of motor, starts axle and is provided with fixing rod.
2. a kind of unmanned plane starting drive according to claim 1, is characterized in that: described notch is inclined notch.
3. a kind of unmanned plane starting drive according to claim 1, is characterized in that: described fixing rod is double-screw bolt.
4. a kind of unmanned plane starting drive according to claim 1, is characterized in that: described enable switch is arranged on handle top.
5. a right to use requires the method for the unmanned plane starting drive described in 1, it is characterized in that: the fixing rod of described starter is stuck in the boot disk of unmanned plane, press enable switch, when the rotating speed of unmanned plane head reaches the value of taking off, starter departs from unmanned plane head.
6. a kind of unmanned plane starting method according to claim 5, is characterized in that: the inrush current of described starter is greater than 100A.
CN201410339725.3A 2014-07-16 2014-07-16 Device and method for starting unmanned aerial vehicle Pending CN104153928A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410339725.3A CN104153928A (en) 2014-07-16 2014-07-16 Device and method for starting unmanned aerial vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410339725.3A CN104153928A (en) 2014-07-16 2014-07-16 Device and method for starting unmanned aerial vehicle

Publications (1)

Publication Number Publication Date
CN104153928A true CN104153928A (en) 2014-11-19

Family

ID=51879524

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410339725.3A Pending CN104153928A (en) 2014-07-16 2014-07-16 Device and method for starting unmanned aerial vehicle

Country Status (1)

Country Link
CN (1) CN104153928A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105351135A (en) * 2015-11-27 2016-02-24 颜原方 Separating type external force starter

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2065247U (en) * 1990-03-19 1990-11-07 王克然 Hand safety means of automobile engine
US20070240664A1 (en) * 2006-04-18 2007-10-18 Thomas Edmund R Device for use in starting a model airplane engine
CN202657250U (en) * 2012-06-08 2013-01-09 无锡汉和航空技术有限公司 Internally-arranged type starting system of unmanned helicopter
CN203623969U (en) * 2013-12-20 2014-06-04 海鹰航空通用装备有限责任公司 Portable high-power starter of small unmanned aerial vehicle
CN203946282U (en) * 2014-07-16 2014-11-19 山东正元数字城市建设有限公司 A kind of unmanned plane actuator

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2065247U (en) * 1990-03-19 1990-11-07 王克然 Hand safety means of automobile engine
US20070240664A1 (en) * 2006-04-18 2007-10-18 Thomas Edmund R Device for use in starting a model airplane engine
CN202657250U (en) * 2012-06-08 2013-01-09 无锡汉和航空技术有限公司 Internally-arranged type starting system of unmanned helicopter
CN203623969U (en) * 2013-12-20 2014-06-04 海鹰航空通用装备有限责任公司 Portable high-power starter of small unmanned aerial vehicle
CN203946282U (en) * 2014-07-16 2014-11-19 山东正元数字城市建设有限公司 A kind of unmanned plane actuator

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105351135A (en) * 2015-11-27 2016-02-24 颜原方 Separating type external force starter
CN105351135B (en) * 2015-11-27 2018-04-20 珠海霄鹰科技发展有限公司 Separate type external force starter

Similar Documents

Publication Publication Date Title
CN202664196U (en) Sugarcane husking machine
CN203357487U (en) Paper tube cutting device
CN104153928A (en) Device and method for starting unmanned aerial vehicle
CN104260892A (en) Electric control separation mechanism of unmanned aerial vehicle and parachute
CN203914548U (en) A kind of soya-bean milk mixer
CN202147192U (en) Flywheel bur removing device
CN203946282U (en) A kind of unmanned plane actuator
CN204548482U (en) A kind of folded form propeller mechanism locating expansion and the state of recovery
CN205199745U (en) Panel beating cleaning oil mixture separator
CN204110362U (en) The automatically controlled separation device of unmanned plane and parachute
CN204197008U (en) A kind of drive type cleaning equipment turning deceleration safety system
CN103934751B (en) A kind of disc type pre-mill clamping device
CN203019307U (en) Dismounting device for torque rheometer mixer rotor
CN204471450U (en) A kind of bar cutting machine
CN202640394U (en) Shaving device of vibrissa machine
CN204055184U (en) The stripping off device of a kind of abandoned car tire and wheel hub
CN205291030U (en) Fruit vegetables cutting box
CN204886592U (en) Extracting tool of rearmounted exciter rotor in micromotor
GB2531437A (en) Ticket scraping device
CN203817236U (en) Cutting machine used for microelement machining
Nakamura et al. Development of the eLen regulation database to support legislation of municipalities
CN203997155U (en) Two-dimension code label is printed sticker
CN206177611U (en) Device is got to automatic shelling of film
CN203460243U (en) Longitudinal cutter device of stretch film packaging machine
CN204340504U (en) A kind of multi-functional automatic rotation lead pencil knife

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication
RJ01 Rejection of invention patent application after publication

Application publication date: 20141119