CN204688437U - A kind of amphibious unmanned plane recording accident - Google Patents

A kind of amphibious unmanned plane recording accident Download PDF

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Publication number
CN204688437U
CN204688437U CN201520398979.2U CN201520398979U CN204688437U CN 204688437 U CN204688437 U CN 204688437U CN 201520398979 U CN201520398979 U CN 201520398979U CN 204688437 U CN204688437 U CN 204688437U
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CN
China
Prior art keywords
engine
processing unit
cloud terrace
steady
unmanned plane
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Withdrawn - After Issue
Application number
CN201520398979.2U
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Chinese (zh)
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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Priority to CN201520398979.2U priority Critical patent/CN204688437U/en
Application granted granted Critical
Publication of CN204688437U publication Critical patent/CN204688437U/en
Withdrawn - After Issue legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a kind of amphibious 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 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 provided with kink, kink and rod hinge connection, hinged place is provided with stepping motor, 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, organism bottom is provided with alighting gear, alighting gear comprises air bag and support body, air bag covering shelf surface, gas filled device is also had in body, gas filled device is connected with engine transmission, and gas filled device is electrically connected with processing unit, and the air extractor duct of gas filled device is communicated with air bag, can the field image of real time recording when having an accident, the amphibious function of unmanned plane is provided simultaneously.

Description

A kind of amphibious unmanned plane recording accident
Technical field
The utility model relates to unmanned plane field, particularly a kind of amphibious 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.After having an accident, unmanned plane may fall into the water, and because unmanned plane is sophisticated electronics, once water inlet, may cause the loss that cannot retrieve, and some special operations also need unmanned plane to possess the function of hovering in level in addition.
Summary of the invention
The object that the utility model will reach is to provide a kind of amphibious unmanned plane recording accident, and the data that can record the accident very first time is that follow-up improvement is offered help, and provides the amphibious function of unmanned plane simultaneously.
In order to achieve the above object, the utility model adopts following technical scheme: a kind of amphibious 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, organism bottom is provided with alighting gear, and alighting gear comprises air bag and support body, air bag covering shelf surface, and also have gas filled device in body, gas filled device is connected with engine transmission, and gas filled device is electrically connected with processing unit, and the air extractor duct of gas filled device is communicated with air bag.
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.
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 and drives gas filled device, control gas filled device is airbag aeration simultaneously, when covering after the air bag on alighting gear surface fills gas, may also be unmanned plane bubble through the water column even if unmanned plane falls within the water surface.Except faulty condition, the order that processing unit also can receive operator as required makes airbag aeration, thus provides the amphibious function of unmanned plane.
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, the utility model tool 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, and provides the amphibious function of unmanned plane simultaneously.
Accompanying drawing explanation
Below in conjunction with accompanying drawing, the utility model is described in further detail:
Fig. 1 is the schematic diagram of a kind of embodiment of the utility model;
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;
Fig. 4 is the schematic diagram of the airbag aeration of Fig. 1 embodiment.
Detailed description of the invention
Fig. 1-4 is depicted as a kind of embodiment of the present utility model.
A kind of amphibious 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.Be provided with alighting gear 8 bottom body 1, alighting gear 8 comprises air bag 9 and support body 10, and air bag 9 covers support body 10 surface, gas filled device is also had in body 1, gas filled device is connected with engine transmission, and gas filled device is electrically connected with processing unit, and the air extractor duct of gas filled device is communicated with air bag 9.
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.
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 and drives gas filled device, control gas filled device is that air bag 9 is inflated simultaneously, when covering after the air bag 9 on alighting gear 8 surface fills gas, may also be unmanned plane bubble through the water column even if unmanned plane falls within the water surface.Except faulty condition, the order that processing unit also can receive operator as required makes air bag 9 inflate, thus provides the amphibious function of unmanned plane.
Except above preferred embodiment, the utility model also has other embodiment, those skilled in the art can make various change and distortion according to the utility model, only otherwise depart from spirit of the present utility model, all should belong to the scope that the utility model claims define.

Claims (2)

1. one kind can be recorded the amphibious 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, organism bottom is provided with alighting gear (8), alighting gear comprises air bag (9) and support body (10), air bag covering shelf surface, gas filled device is also had in body, gas filled device is connected with engine transmission, gas filled device is electrically connected with processing unit, and the air extractor duct of gas filled device is communicated with air bag.
2. a kind of amphibious unmanned plane recording accident according to claim 1, is characterized in that: the steady The Cloud Terrace of described increasing is electrically connected with processing unit.
CN201520398979.2U 2015-06-10 2015-06-10 A kind of amphibious unmanned plane recording accident Withdrawn - After Issue CN204688437U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201520398979.2U CN204688437U (en) 2015-06-10 2015-06-10 A kind of amphibious unmanned plane recording accident

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201520398979.2U CN204688437U (en) 2015-06-10 2015-06-10 A kind of amphibious unmanned plane recording accident

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CN204688437U true CN204688437U (en) 2015-10-07

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104890891A (en) * 2015-06-10 2015-09-09 浙江空行飞行器技术有限公司 Amphibious unmanned plane capable of recording accident

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104890891A (en) * 2015-06-10 2015-09-09 浙江空行飞行器技术有限公司 Amphibious unmanned plane capable of recording accident

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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: 20151007

Termination date: 20160610

AV01 Patent right actively abandoned
AV01 Patent right actively abandoned

Granted publication date: 20151007

Effective date of abandoning: 20171222