CN202417771U - Starter for unmanned helicopter - Google Patents

Starter for unmanned helicopter Download PDF

Info

Publication number
CN202417771U
CN202417771U CN201120483583XU CN201120483583U CN202417771U CN 202417771 U CN202417771 U CN 202417771U CN 201120483583X U CN201120483583X U CN 201120483583XU CN 201120483583 U CN201120483583 U CN 201120483583U CN 202417771 U CN202417771 U CN 202417771U
Authority
CN
China
Prior art keywords
gear
starter
electrical machinery
power output
starting electrical
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.)
Expired - Fee Related
Application number
CN201120483583XU
Other languages
Chinese (zh)
Inventor
罗军
魏光华
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.)
CHENGDU JINGSHI MODEL DEVELOPMENT CO LTD
Original Assignee
CHENGDU JINGSHI MODEL DEVELOPMENT 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 CHENGDU JINGSHI MODEL DEVELOPMENT CO LTD filed Critical CHENGDU JINGSHI MODEL DEVELOPMENT CO LTD
Priority to CN201120483583XU priority Critical patent/CN202417771U/en
Application granted granted Critical
Publication of CN202417771U publication Critical patent/CN202417771U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Images

Landscapes

  • Gear Transmission (AREA)

Abstract

The utility model discloses a starter for an unmanned helicopter. The starter comprises a starting motor, a starting motor connecting gear, a starting motor gear plate, a handle connecting column, a starter driven gear, a starting motor driven gear seat, a gear-fixed middle seat, an output fixed gear seat, a power output sleeve, a power output shaft, a starting switch, a handle and a gear power output shaft; the major part of the power output shaft is centered and arranged in the power output sleeve by a plurality of bearings; a plurality of one-way bearings are arranged between the upper bearing and the lower bearing to ensure that the power output shaft can only be rotated in one direction; the position at 1-2 cm of the top end of the power output shaft is machined into a cubic column; and the power output shaft is connected with a speed-increasing gear and a speed-reducing gear by the starting motor output shaft to increase output torque. The starter for the unmanned helicopter, disclosed by the utility model, is small and convenient to carry and is convenient for a user to start the unmanned helicopter by holding the starter through the handle.

Description

A kind of starter that is used for depopulated helicopter
Technical field
The utility model relates to technical field of engines, is specifically related to a kind of starter that is used for depopulated helicopter.
Background technique
Because the engine power of depopulated helicopter is big, rotating speed is fast, and the starter outputting torsion of general model plane is too little, can't ato unit.And the big back of engine speed, also can't re-use because of the impact force behind the engine start causes starter even started motor also bigger, the general model plane starter of impact force of the pto of starter.
The model utility content
To above-mentioned existing technology, the technical problem that the utility model will solve is: starter is the key technology that starts helicopter, and general model plane starter can't start depopulated helicopter, want starter can start depopulated helicopter at present, and starter can use repeatedly again.
In order to solve the problems of the technologies described above, the utility model adopts following technological scheme:
A kind of starter that is used for depopulated helicopter; Comprise that starting electrical machinery, starting electrical machinery connect tooth, short fixed plate supporting post, starting electrical machinery gear plate, handle link post, starter driven tooth, the driven toothholder of starting electrical machinery, the fixing middle seat of gear, output fixing tooth wheel seat, power output cover, pto, enable switch, handle, gear transmission output shaft; It is characterized in that; Said pto is most of to place power output cover with several bearing centering; Several unilateral bearings are set between metal (upper guarantee that pto can only rotate to a direction, pto top 1-2cm is processed into cube rod; Pto connects overdrive gear through the starting electrical machinery output shaft and deceleration gear increases its outputting torsion.
Said starting electrical machinery, gear transmission output shaft, power output cover and pto link the post position of center line at handle, and are in coaxial inner conductor.
Said starting electrical machinery output power is at least 12V-80A.
Said enable switch places on the handle.
Said enable switch is relay switch or air-break switch.
Compared with prior art, the utlity model has following beneficial effect:
The utility model is small and exquisite, easy to carry, and the user utilizes handle to hold starter to start depopulated helicopter very easily.
Description of drawings
Fig. 1 is the main TV structure schematic representation of the utility model;
Fig. 2 is the plan view of the utility model;
Fig. 3 is the A phantom of Fig. 1;
1 is starting electrical machinery among the figure; 2 are starting electrical machinery connection tooth; 3 are short fixed plate supporting post; 4 is the starting electrical machinery gear plate; 5 are handle link post; 6 is the starting electrical machinery driven tooth; 7 is the driven toothholder of starting electrical machinery; 8 are the fixing middle seat of gear; 9 are long fixed plate supporting post; 10 is the output gear wheel seat; 11 is that secondary output gear shaft 12 is output fixed gear seat strut; 13 are output fixing tooth wheel seat; 14 are power output cover; 15 is pto; 16 is enable switch; 17 is handle; 18 is the gear transmission output shaft; 19 is bearing; 20 is unilateral bearing.
Embodiment
To combine accompanying drawing and embodiment that the utility model is done further to describe below.
Embodiment
A kind of starter that is used for depopulated helicopter; Comprise starting electrical machinery (1), starting electrical machinery connect tooth (2), short fixed plate supporting post (3), starting electrical machinery gear plate (4), handle link post (5), starter driven tooth (6), the driven toothholder of starting electrical machinery (7), gear fixing in seat (8), long fixed plate supporting post (9), output gear wheel seat (10), secondary output gear shaft (11), output fixed gear wheel seat strut (12), output fixing tooth wheel seat (13), power output overlap (14), pto (15), enable switch (16), handle (17) and gear transmission output shaft (18); It is characterized in that; Said pto is most of to place power output cover with several bearing centering; Several unilateral bearings (20) are set between metal (upper (19) guarantee that pto can only rotate to a direction, pto top 1-2cm is processed into cube rod; Pto connects overdrive gear through the starting electrical machinery output shaft and deceleration gear increases its outputting torsion.
Starting electrical machinery (1) and starting electrical machinery gear plate are fixedly mounted on handle link post central position; One handle is respectively installed in handle link post both sides; Short fixed plate supporting post (3) is installed between starting electrical machinery gear plate (4) and the fixing middle seat of gear (8), and starting electrical machinery connects tooth (2) and is connected on the starting electrical machinery output shaft, and is installed in short fixed plate supporting post (3) below; Starting electrical machinery driven tooth and secondary output gear link together through the secondary output gear shaft; Welding one long fixing branch dagger between output fixing tooth wheel seat and starting electrical machinery gear plate; Between seat (8) output gear wheel seat (10) is set during output fixing tooth wheel seat (13) and gear are fixing, output gear and fixing with power output cover is set on the output gear wheel seat.
When opening enable switch; Motor rotates and drives starting electrical machinery connection tooth (2) rotation, and starting electrical machinery connection tooth drives starting electrical machinery driven tooth (6) and rotates, while secondary output gear rotation; The output gear that the secondary output gear drives on the output gear wheel seat (10) rotates; Further drive output cover rotates, and power is exported pto (15) is rotated, and pto drives the engine start axle and rotates.Behind engine start, the rotating speed of engine start axle is during greater than the rotating speed of pto (15), and the engine start axle drives pto and rotates at faster speed, this moment parallel taking-up starter.

Claims (5)

1. starter that is used for depopulated helicopter; Comprise that starting electrical machinery, starting electrical machinery connect tooth, short fixed plate supporting post, starting electrical machinery gear plate, handle link post, starter driven tooth, the driven toothholder of starting electrical machinery, the fixing middle seat of gear, output fixing tooth wheel seat, power output cover, pto, enable switch, handle, gear transmission output shaft; It is characterized in that; Said pto is most of to place power output cover with several bearing centering; Several unilateral bearings are set between metal (upper guarantee that pto can only rotate to a direction, pto top 1-2cm is processed into cube rod; Pto connects overdrive gear through the starting electrical machinery output shaft and deceleration gear increases its outputting torsion.
2. the starter that is used for depopulated helicopter according to claim 1 is characterized in that, said starting electrical machinery, gear transmission output shaft, power output cover and pto link the post position of center line at handle, and are in coaxial inner conductor.
3. the starter that is used for depopulated helicopter according to claim 1 is characterized in that, said starting electrical machinery output power is at least 12V-80A.
4. the starter that is used for depopulated helicopter according to claim 1 is characterized in that said enable switch places on the handle.
5. the starter that is used for depopulated helicopter according to claim 1 is characterized in that, said enable switch is relay switch or air-break switch.
CN201120483583XU 2011-11-29 2011-11-29 Starter for unmanned helicopter Expired - Fee Related CN202417771U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201120483583XU CN202417771U (en) 2011-11-29 2011-11-29 Starter for unmanned helicopter

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201120483583XU CN202417771U (en) 2011-11-29 2011-11-29 Starter for unmanned helicopter

Publications (1)

Publication Number Publication Date
CN202417771U true CN202417771U (en) 2012-09-05

Family

ID=46742542

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201120483583XU Expired - Fee Related CN202417771U (en) 2011-11-29 2011-11-29 Starter for unmanned helicopter

Country Status (1)

Country Link
CN (1) CN202417771U (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103925060A (en) * 2014-03-26 2014-07-16 沈阳天之翼航空科技有限公司 Water-cooling power device of small unmanned helicopter
CN104554737A (en) * 2013-10-24 2015-04-29 安阳全丰航空植保科技有限公司 Helicopter electric starting power supply device
CN105351135A (en) * 2015-11-27 2016-02-24 颜原方 Separating type external force starter
CN113586306A (en) * 2021-09-29 2021-11-02 北京中航智科技有限公司 Electric starter

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104554737A (en) * 2013-10-24 2015-04-29 安阳全丰航空植保科技有限公司 Helicopter electric starting power supply device
CN103925060A (en) * 2014-03-26 2014-07-16 沈阳天之翼航空科技有限公司 Water-cooling power device of small unmanned helicopter
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
CN113586306A (en) * 2021-09-29 2021-11-02 北京中航智科技有限公司 Electric starter

Similar Documents

Publication Publication Date Title
CN202449162U (en) Harmonic speed reducing driver for electric bicycle
CN2894047Y (en) Electric bicycle harmonic reducing speed driving device
CN202417771U (en) Starter for unmanned helicopter
CN103070576B (en) Swing swing mechanism and baby's swing
CN202260849U (en) Coaxial double-motor transmission structure for stage lamp
CN102658852A (en) Double-driving double-power device of electro-tricycle
CN203181874U (en) Automatic rotation type bird repelling thorn device
CN203236176U (en) Overturning and welding device for ocean shipping frame blade root
CN202121441U (en) Motor main shaft positioning device of solar energy tracker
CN204652135U (en) Solid rotor box hat brake motor
CN107293140A (en) The traffic lights of urban construction
CN207720005U (en) A kind of list stator and double-rotor coaxial motor
CN202138225U (en) Wheel driving device
CN206082747U (en) Multifunctional meat grinder
CN201406259Y (en) Escalator driving device
CN202588929U (en) Rocking chair
CN202054138U (en) Lifting pod propeller driven by permanent magnet motor
CN203486142U (en) Two-stage transmission mechanism for single super-light type helicopter
CN201045012Y (en) Electric vehicle driving structure
CN201658846U (en) Coaxial planetary transmission case of model helicopter
CN202557728U (en) Double-drive double-power equipment of electric tricycle
CN201161698Y (en) Drive device of tricycle
CN202054129U (en) Dual driving device for motor vehicle
CN201346718Y (en) Combined type motor base of machining centre
CN209218547U (en) Improved loosenning tiller

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: 20120905

Termination date: 20191129