CN104908944A - Accident recordable unmanned aerial vehicle - Google Patents

Accident recordable unmanned aerial vehicle Download PDF

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Publication number
CN104908944A
CN104908944A CN201510316813.6A CN201510316813A CN104908944A CN 104908944 A CN104908944 A CN 104908944A CN 201510316813 A CN201510316813 A CN 201510316813A CN 104908944 A CN104908944 A CN 104908944A
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CN
China
Prior art keywords
engine
processing unit
connecting rod
steady
cloud terrace
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Granted
Application number
CN201510316813.6A
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Chinese (zh)
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CN104908944B (en
Inventor
姜振
张斌斐
汪万里
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Zhejiang Null Vehicle Technology Co Ltd
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Zhejiang Null Vehicle Technology Co Ltd
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Filing date
Publication date
Application filed by Zhejiang Null Vehicle Technology Co Ltd filed Critical Zhejiang Null Vehicle Technology Co Ltd
Priority to CN201510316813.6A priority Critical patent/CN104908944B/en
Publication of CN104908944A publication Critical patent/CN104908944A/en
Application granted granted Critical
Publication of CN104908944B publication Critical patent/CN104908944B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The invention discloses an accident recordable unmanned aerial vehicle which comprises a vehicle body, wherein a processing unit and an engine are arranged in the vehicle body; the processing unit is electrically connected with the engine; rotor wings are arranged on the vehicle body, and are connected with the engine in a transmission way; a stability augmentation pan-tilt is arranged below the vehicle body; a camera is arranged on the stability augmentation pan-tilt; the stability augmentation pan-tilt is connected with the engine in the vehicle body by a connecting rod; the engine can drive the connecting rod to move along the direction parallel to a rotating shaft of the rotor wings; one end of the connecting rod is connected with the engine; a bending part extending linearly is arranged at the other end of the connecting rod, and is articulated with the connecting rod; a stepping motor is arranged at an articulated part and electrically connected with the processing unit; the stability augmentation pan-tilt is fixed on the bending part; the shooting direction of the camera on the stability augmentation pan-tilt is perpendicular to the length direction of the bending part; an accelerated speed inductor is arranged in the vehicle body; the processing unit is electrically connected with the accelerated speed inductor; and the camera can shoot the vehicle body of the unmanned aerial vehicle in a direction changing manner, so as to record scene images in real time when an accident happens.

Description

A kind of unmanned plane recording accident
Technical field
The present invention relates to unmanned plane field, particularly a kind of unmanned plane recording accident.
Background technology
Agricultural development trend must be intensive Quantity production pattern, and using mechanized tool to substitute manual work is in such a mode one of necessary condition, and wherein a kind of approach of spraying insecticide uses unmanned plane to carry agricultural chemicals aloft to spray.In the operation process that existing unmanned plane is sprayed insecticide, because some unforeseen circumstancess may be wounded by exotic, or self produces mechanical breakdown, under this state may there is air crash accident in unmanned plane, and due to unmanned plane during flying distant, once unmanned plane crash after, ex-post analysis accident causation difficulty, not accurate enough according to the conclusion that crash site draws, do not have very first time data to be difficult to for follow-up improvement is offered help.
Summary of the invention
The object that the present invention will reach is to provide a kind of unmanned plane recording accident, and the data that can record the accident very first time is that follow-up improvement is offered help.
In order to achieve the above object, the present invention adopts following technical scheme: a kind of unmanned plane recording accident, comprise body, processing unit and engine is provided with in body, processing unit is electrically connected with engine, body is provided with rotor, rotor is connected with engine transmission, body has and increases steady The Cloud Terrace, increase steady The Cloud Terrace and be provided with pick up camera, increase steady The Cloud Terrace to be connected with the engine in body by connecting rod, engine can drive link along being parallel to the square upward movement of rotorshaft, connecting rod one end is connected with engine, the connecting rod other end is provided with linearly extended kink, kink and rod hinge connection, hinged place is provided with stepping motor, stepping motor is electrically connected with processing unit, increasing steady The Cloud Terrace is fixed on kink, increase the length direction of shooting direction perpendicular to kink of the pick up camera on steady The Cloud Terrace, be provided with acceleration induction device in body, processing unit is electrically connected with acceleration induction device.
The acceleration/accel of acceleration induction device Real-Time Monitoring unmanned plane, when unmanned plane receives installation damage, the acceleration be not inconsistent with regular flight condition will inevitably be there is, processing unit obtains this information by acceleration induction device and contrasts with the data of normal flight, show that unmanned plane is in air crash state once analyze, processing unit controls engine drive link and stretches out in body, after the distance that reaches capacity, processing unit control step electric motor starting, thus kink is bent on connecting rod, after kink 90-degree bent, increase steady The Cloud Terrace half-twist thereupon, make the pick up camera in shooting unmanned plane front originally then take to increase above steady The Cloud Terrace, thus can the state of real time recording unmanned plane when having an accident, by increasing steady The Cloud Terrace, pick up camera is installed, the unstable unmanned plane that flies under can making accident condition reduces the impact of the shooting quality of pick up camera.
Further, the steady The Cloud Terrace of described increasing is electrically connected with processing unit.After the data that acceleration induction device obtains transfer to processing unit analyzing and processing, processing unit can control to increase steady The Cloud Terrace and act accordingly, thus improves shooting quality.
After adopting technique scheme, tool of the present invention has the following advantages:
Pick up camera can turn shooting unmanned plane body, thus can the field image of real time recording when having an accident.
Accompanying drawing explanation
Below in conjunction with accompanying drawing, the invention will be further described:
Fig. 1 is the schematic diagram of an embodiment of the present invention;
Fig. 2 is the schematic diagram after the steady The Cloud Terrace of increasing of Fig. 1 embodiment moves downward;
Fig. 3 is the schematic diagram of the increasing steady The Cloud Terrace of pick up camera upwards under shooting state of Fig. 1 embodiment.
Detailed description of the invention
Fig. 1-3 is depicted as a kind of embodiment of the present invention.
A kind of unmanned plane recording accident, comprise body 1, processing unit and engine is provided with in body 1, processing unit is electrically connected with engine, body 1 is provided with rotor 2, rotor 2 is connected with engine transmission, body 1 has and increases steady The Cloud Terrace 3, increase steady The Cloud Terrace 3 and be provided with pick up camera 4, increase steady The Cloud Terrace 3 to be connected with the engine in body 1 by connecting rod 5, engine can drive link 5 along the square upward movement being parallel to rotor 2 rotating shaft, connecting rod 5 one end is connected with engine, connecting rod 5 other end is provided with linearly extended kink, kink and connecting rod 5 hinged, hinged place is provided with stepping motor 7, stepping motor 7 is electrically connected with processing unit, increasing steady The Cloud Terrace 3 is fixed on kink, increase the length direction of shooting direction perpendicular to kink of the pick up camera 4 on steady The Cloud Terrace 3, acceleration induction device is provided with in body 1, processing unit is electrically connected with acceleration induction device, increases steady The Cloud Terrace 3 and is electrically connected with processing unit, after the data that acceleration induction device obtains transfer to processing unit analyzing and processing, processing unit can control to increase steady The Cloud Terrace 3 and act accordingly, thus improves shooting quality.
The acceleration/accel of acceleration induction device Real-Time Monitoring unmanned plane, when unmanned plane receives installation damage, the acceleration be not inconsistent with regular flight condition will inevitably be there is, processing unit obtains this information by acceleration induction device and contrasts with the data of normal flight, show that unmanned plane is in air crash state once analyze, processing unit controls engine drive link 5 and stretches out in body 1, after the distance that reaches capacity, processing unit control step motor 7 starts, thus kink is bent on connecting rod 5, after kink 90-degree bent, increase steady The Cloud Terrace 3 half-twist thereupon, make the pick up camera 4 in shooting unmanned plane front originally then take to increase above steady The Cloud Terrace 3, thus can the state of real time recording unmanned plane when having an accident, by increasing steady The Cloud Terrace 3, pick up camera 4 is installed, the unstable unmanned plane that flies under can making accident condition reduces the impact of the shooting quality of pick up camera 4.Pick up camera 4 can turn shooting unmanned plane body 1, thus can the field image of real time recording when having an accident.
Except above preferred embodiment, the present invention also has other embodiment, and those skilled in the art can make various change and distortion according to the present invention, only otherwise depart from spirit of the present invention, all should belong to the scope that claims of the present invention define.

Claims (2)

1. one kind can be recorded the unmanned plane of accident, it is characterized in that: comprise body (1), processing unit and engine is provided with in body, processing unit is electrically connected with engine, body is provided with rotor (2), rotor is connected with engine transmission, body has and increases steady The Cloud Terrace (3), increase steady The Cloud Terrace and be provided with pick up camera (4), increase steady The Cloud Terrace to be connected with the engine in body by connecting rod (5), engine can drive link along being parallel to the square upward movement of rotorshaft, connecting rod one end is connected with engine, the connecting rod other end is provided with linearly extended kink (6), kink and rod hinge connection, hinged place is provided with stepping motor (7), stepping motor is electrically connected with processing unit, increasing steady The Cloud Terrace is fixed on kink, increase the length direction of shooting direction perpendicular to kink of the pick up camera on steady The Cloud Terrace, be provided with acceleration induction device in body, processing unit is electrically connected with acceleration induction device.
2. according to claim 1, it is characterized in that: the steady The Cloud Terrace of described increasing is electrically connected with processing unit.
CN201510316813.6A 2015-06-10 2015-06-10 A kind of unmanned plane of recordable accident Expired - Fee Related CN104908944B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201510316813.6A CN104908944B (en) 2015-06-10 2015-06-10 A kind of unmanned plane of recordable accident

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Application Number Priority Date Filing Date Title
CN201510316813.6A CN104908944B (en) 2015-06-10 2015-06-10 A kind of unmanned plane of recordable accident

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CN104908944A true CN104908944A (en) 2015-09-16
CN104908944B CN104908944B (en) 2017-03-01

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108227740A (en) * 2017-12-29 2018-06-29 北京臻迪科技股份有限公司 Aircraft chain rupture control method and aircraft

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201287830Y (en) * 2008-10-14 2009-08-12 西安展翼航空科技有限公司 Stabilising bracket for aerial photography camera
WO2010140082A1 (en) * 2009-06-04 2010-12-09 Cape Peninsula University Of Technology Unmanned aerial vehicle
WO2013033924A1 (en) * 2011-09-09 2013-03-14 深圳市大疆创新科技有限公司 Dual-axis ball head for use in unmanned aerial vehicle, triple-axis ball head for use in unmanned aerial vehicle, and multi-rotor aerial vehicle
US20140145026A1 (en) * 2012-11-28 2014-05-29 Hans Skjersaa Unmanned Aerial Device
CN104149982A (en) * 2014-04-11 2014-11-19 陕西科技大学 Air quality detector based on quadcopter
CN204688416U (en) * 2015-06-10 2015-10-07 浙江空行飞行器技术有限公司 A kind of unmanned plane recording accident

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201287830Y (en) * 2008-10-14 2009-08-12 西安展翼航空科技有限公司 Stabilising bracket for aerial photography camera
WO2010140082A1 (en) * 2009-06-04 2010-12-09 Cape Peninsula University Of Technology Unmanned aerial vehicle
WO2013033924A1 (en) * 2011-09-09 2013-03-14 深圳市大疆创新科技有限公司 Dual-axis ball head for use in unmanned aerial vehicle, triple-axis ball head for use in unmanned aerial vehicle, and multi-rotor aerial vehicle
US20140145026A1 (en) * 2012-11-28 2014-05-29 Hans Skjersaa Unmanned Aerial Device
CN104149982A (en) * 2014-04-11 2014-11-19 陕西科技大学 Air quality detector based on quadcopter
CN204688416U (en) * 2015-06-10 2015-10-07 浙江空行飞行器技术有限公司 A kind of unmanned plane recording accident

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108227740A (en) * 2017-12-29 2018-06-29 北京臻迪科技股份有限公司 Aircraft chain rupture control method and aircraft

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Inventor after: Zhang Binfei

Inventor after: Wang Weiyuan

Inventor after: Wang Wanli

Inventor before: Jiang Zhen

Inventor before: Zhang Binfei

Inventor before: Wang Wanli

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: 20170301

Termination date: 20180610