CN205366085U - Unmanned aerial vehicle engine all -in -one - Google Patents

Unmanned aerial vehicle engine all -in -one Download PDF

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Publication number
CN205366085U
CN205366085U CN201620134819.1U CN201620134819U CN205366085U CN 205366085 U CN205366085 U CN 205366085U CN 201620134819 U CN201620134819 U CN 201620134819U CN 205366085 U CN205366085 U CN 205366085U
Authority
CN
China
Prior art keywords
starter motor
connecting plate
electromotor
vehicle engine
generator
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
CN201620134819.1U
Other languages
Chinese (zh)
Inventor
陈超
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.)
Shanxi Weifeng Spring Unmanned System Co., Ltd.
Original Assignee
Shanxi Weifeng Unmanned Systems Technology 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 Shanxi Weifeng Unmanned Systems Technology Co Ltd filed Critical Shanxi Weifeng Unmanned Systems Technology Co Ltd
Priority to CN201620134819.1U priority Critical patent/CN205366085U/en
Application granted granted Critical
Publication of CN205366085U publication Critical patent/CN205366085U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)

Abstract

The utility model discloses an unmanned aerial vehicle engine all -in -one, include: the engine, the generator gear, an electric generator, the starter motor connecting plate, start the aircraft bonnet, starter motor board and starter motor, this kind of engine all -in -one is through installing the starter motor on the starter motor board, starter motor upper portion is provided with the start -up aircraft bonnet, the starter motor board is fixed on the starter motor connecting plate, the starter motor connecting plate is survived and is installed the generator, start to be provided with on the generator generator gear, still install the engine on the starter motor connecting plate, integrative simple structure, it is compact, thereby raise the efficiency, the failure rate is lowered.

Description

A kind of unmanned vehicle engine all-in-one
Technical field
This utility model relates to unmanned vehicle engine technical field, particularly relates to a kind of unmanned vehicle engine all-in-one.
Background technology
Along with modern science and technology is fast-developing, the application of unmanned aerial vehicle is more and more extensive, heavy-duty, during long boat, the demand of the unmanned aerial vehicle of high reliability is increasing, is arranged on the diverse location of helicopter owing to tradition depopulated helicopter startup device includes the parts such as electromotor, starter motor, electromotor, and structure is not compact, the safety of unmanned plane cause it may happen that fault is many, thus cannot be ensured.
Utility model content
In order to overcome above-mentioned the deficiencies in the prior art, this utility model provides a kind of unmanned vehicle engine all-in-one.
This utility model be the technical scheme is that a kind of unmanned vehicle engine all-in-one, including: electromotor, generator gear, electromotor, starter motor connecting plate, startup hood, starter motor plate and starter motor, described starter motor is arranged on starter motor plate, described starter motor top is provided with startup hood, described starter motor plate is fixed on starter motor connecting plate, described starter motor connecting plate also has electromotor is installed, electromotor is provided with generator gear, described starter motor connecting plate has installation electromotor.
The beneficial effects of the utility model are: integrative-structure is simple, compact, thus improving efficiency, reduce fault rate.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model.
In figure: 1. electromotor, 2. generator gear, 3. electromotor, 4. starter motor connecting plate, 5. startup hood, 6. starter motor plate, 7. starter motor.
Detailed description of the invention
In order to be able to be more clearly understood that the technical solution of the utility model, below in conjunction with accompanying drawing, this utility model is further illustrated.
Unmanned vehicle engine all-in-one as depicted, including: electromotor 1, generator gear 2, electromotor 3, starter motor connecting plate 4, startup hood 5, starter motor plate 6 and starter motor 7, starter motor 7 is arranged on starter motor plate 6, starter motor 7 top is provided with startup hood 5, starter motor plate 6 is fixed on starter motor connecting plate 4, starter motor connecting plate 4 also has electromotor 3 is installed, electromotor 3 is provided with generator gear 2, starter motor connecting plate 4 has installation electromotor 1.
Operation principle: electromotor 1 and each parts such as electromotor 3, starter motor 7 are assembled integrally machine by starter motor connecting plate 4, technical solutions of the utility model adopt integral structure simple, compact, connection member is few, can effectively reduce fault rate, thus economization expense.
The above is only better embodiment of the present utility model, therefore all equivalences done according to the structure described in this utility model patent claim, feature and principle change or modify, and are all included in this utility model patent claim.

Claims (1)

1. a unmanned vehicle engine all-in-one, it is characterized in that, including: electromotor (1), generator gear (2), electromotor (3), starter motor connecting plate (4), start hood (5), starter motor plate (6) and starter motor (7), described starter motor (7) is arranged on starter motor plate (6), described starter motor (7) top is provided with startup hood (5), described starter motor plate (6) is fixed on starter motor connecting plate (4), described starter motor connecting plate (4) is upper also installs electromotor (3), electromotor (3) is provided with generator gear (2), described starter motor connecting plate (4) there is installation electromotor (1).
CN201620134819.1U 2016-02-23 2016-02-23 Unmanned aerial vehicle engine all -in -one Expired - Fee Related CN205366085U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201620134819.1U CN205366085U (en) 2016-02-23 2016-02-23 Unmanned aerial vehicle engine all -in -one

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201620134819.1U CN205366085U (en) 2016-02-23 2016-02-23 Unmanned aerial vehicle engine all -in -one

Publications (1)

Publication Number Publication Date
CN205366085U true CN205366085U (en) 2016-07-06

Family

ID=56271030

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201620134819.1U Expired - Fee Related CN205366085U (en) 2016-02-23 2016-02-23 Unmanned aerial vehicle engine all -in -one

Country Status (1)

Country Link
CN (1) CN205366085U (en)

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
C56 Change in the name or address of the patentee
CP01 Change in the name or title of a patent holder

Address after: 033000 Shanxi city of Lvliang province Lishi District jujube forest Township ten Village

Patentee after: Shanxi Weifeng Spring Unmanned System Co., Ltd.

Address before: 033000 Shanxi city of Lvliang province Lishi District jujube forest Township ten Village

Patentee before: SHANXI WEIFENG UNMANNED SYSTEMS TECHNOLOGY CO., LTD.

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: 20160706

Termination date: 20210223