CN203638095U - Unmanned mapping machine - Google Patents

Unmanned mapping machine Download PDF

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Publication number
CN203638095U
CN203638095U CN201320826112.3U CN201320826112U CN203638095U CN 203638095 U CN203638095 U CN 203638095U CN 201320826112 U CN201320826112 U CN 201320826112U CN 203638095 U CN203638095 U CN 203638095U
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CN
China
Prior art keywords
mapping machine
unmanned mapping
unmanned
machine
fuselage
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
CN201320826112.3U
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Chinese (zh)
Inventor
李国哲
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.)
HUNCHUN GUOYAOBOCHENG TECHNOLOGY Co Ltd
Original Assignee
HUNCHUN GUOYAOBOCHENG 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 HUNCHUN GUOYAOBOCHENG TECHNOLOGY Co Ltd filed Critical HUNCHUN GUOYAOBOCHENG TECHNOLOGY Co Ltd
Priority to CN201320826112.3U priority Critical patent/CN203638095U/en
Application granted granted Critical
Publication of CN203638095U publication Critical patent/CN203638095U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model discloses an unmanned mapping machine. The unmanned mapping machine comprises a machine body, wings and an empennage, wherein the machine body is connected with the wings through a first bolt; the machine body is connected with the empennage through a second bolt; the machine body is divided into an engine compartment, an equipment compartment, an umbrella compartment and a load compartment from front to back. The unmanned mapping machine provided by the utility model has the characteristics of convenience in carrying, simplicity in maintenance and use, low cost and reusability. The unmanned mapping machine has a high assembling speed in emergency rescue; the requirements of catapult-assisted take-off on a take-off field are low and the requirements of a parachute on an airplane landing field are low, so that the unmanned mapping machine has relatively strong advantages, wide market demands and easiness of popularization and application.

Description

Unmanned mapping machine
Technical field
The utility model relates to a kind of unmanned mapping machine.
Background technology
Traditional mapping machine is generally by manually manipulating.The structure of artificial mapping machine is comparatively complicated, carries comparatively difficulty, and productive costs is high.
Utility model content
The purpose of this utility model is to provide a kind of unmanned mapping machine, with one or more in addressing the above problem.
The utility model discloses a kind of unmanned mapping machine, it comprises fuselage, wing and empennage, between described fuselage and described wing, be connected by the first latch, described fuselage is connected by the second latch with described empennage, and described fuselage is divided into piggyback pod, equipment compartment, umbrella cabin and load cabin from front to back.
Preferably, the front end of described fuselage is provided with screw propeller.
Preferably, in described equipment compartment, be provided with autopilot.
Preferably, in described umbrella cabin, be provided with parachute.
Preferably, in described piggyback pod, be provided with driving engine and driving engine shock mount.
Preferably, in described load cabin, be provided with mapper.
Preferably, the below in described umbrella cabin is provided with fuel tank.
Unmanned mapping facility in the utility model have easy to carry. safeguard use simple. cost is low. the feature such as reusable.In the time of emergency repair, unmanned mapping machine assembling speed is fast, and catapult-assisted take-off requires low to take-off venue, and parachuting is to aircraft landing place, thereby it has stronger advantage, has the wide market demand, is easy to apply.
Brief description of the drawings
Fig. 1 shows unmanned mapping machine of the present utility model.
In accompanying drawing: 1, oar cover; 2, screw propeller; 3, driving engine; 4, driving engine shock mount; 5, equipment compartment; 6, umbrella cabin; 7, wing; 8, load cabin; 9, fuselage; 10, vertical fin; 11, empennage; 12, ventral winglet; 13, device security frame; 14, fuel tank; 15. alighting gears; 16, piggyback pod.
Detailed description of the invention
Below in conjunction with accompanying drawing, preferred embodiment of the present utility model is described in detail, thereby so that advantage of the present utility model and feature can be easier to be those skilled in the art will recognize that, protection domain of the present utility model is made to more explicit defining.
In the first embodiment of the present utility model, shown in Fig. 1, unmanned mapping machine comprises fuselage 9, wing 7 and empennage 11, between fuselage 9 and wing 7, is connected by the first latch, and fuselage 9 is connected by the second latch with empennage 11.Detachable between wing 7 and empennage 11 and fuselage 9.After host wing 7 or empennage 11 and fuselage 9 are separated, the size of this unmanned mapping machine is reduced to minimum, thereby unmanned mapping machine is now easy to carry.Whole unmanned mapping machine adopts modular design, and interface is type quick detaching, and more exchange device is very convenient.
Fuselage 9 is divided into piggyback pod 16, equipment compartment 5, umbrella cabin 6 and load cabin 8 from front to back.The front end that is piggyback pod 16 at the front end of fuselage 9 can also be provided with screw propeller 2 and oar cover 1.The rear portion of fuselage 9 is that the rear portion in load cabin 8 can be provided with ventral winglet 12 and vertical fin 10.Below fuselage 9, can also be provided with alighting gear 15.
Piggyback pod 16 is interior can be provided with driving engine 3, can also be provided with the driving engine shock mount 4 for damping, can also be covered with car bonnet in the outside of driving engine 3.In equipment compartment 5, being provided with autopilot etc. can be for the equipment of driving, measurement or data transmission.Load cabin 8 is interior can be provided with mapper and device security frame 13.In umbrella cabin 6, be provided with parachute.Complete machine intensity is high, has parachute buffering, has guaranteed aircraft safety landing, so can repeated usage.Below umbrella cabin 6, be provided with fuel tank 14, as the center of gravity of fuselage 9.
Unmanned mapping facility in the utility model have easy to carry. safeguard use simple. cost is low. the feature such as reusable.In the time of emergency repair, unmanned mapping machine assembling speed is fast, and catapult-assisted take-off requires low to take-off venue, and parachuting is to aircraft landing place, thereby it has stronger advantage, has the wide market demand, is easy to apply.
Each embodiment in this specification sheets all adopts the mode of going forward one by one to describe, and what each embodiment stressed is and the difference of other embodiment, between each embodiment identical similar part mutually referring to.
The foregoing is only preferred embodiment of the present utility model, be not limited to the utility model, for a person skilled in the art, the utility model can have various modifications and variations.All within spirit of the present utility model and principle, any amendment of doing, be equal to replacement, improvement etc., within all should being included in protection domain of the present utility model.

Claims (7)

1. a unmanned mapping machine, it is characterized in that: it comprises fuselage, wing and empennage, between described fuselage and described wing, be connected by the first latch, described fuselage is connected by the second latch with described empennage, and described fuselage is divided into piggyback pod, equipment compartment, umbrella cabin and load cabin from front to back.
2. unmanned mapping machine according to claim 1, is characterized in that: the front end of described fuselage is provided with screw propeller.
3. unmanned mapping machine according to claim 1, is characterized in that: in described equipment compartment, be provided with autopilot.
4. unmanned mapping machine according to claim 1, is characterized in that: described umbrella is provided with parachute in cabin.
5. unmanned mapping machine according to claim 1, is characterized in that: in described piggyback pod, be provided with driving engine and driving engine shock mount.
6. unmanned mapping machine according to claim 1, is characterized in that: described load is provided with mapper in cabin.
7. unmanned mapping machine according to claim 1, is characterized in that: the below in described umbrella cabin is provided with fuel tank.
CN201320826112.3U 2013-12-13 2013-12-13 Unmanned mapping machine Expired - Fee Related CN203638095U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201320826112.3U CN203638095U (en) 2013-12-13 2013-12-13 Unmanned mapping machine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201320826112.3U CN203638095U (en) 2013-12-13 2013-12-13 Unmanned mapping machine

Publications (1)

Publication Number Publication Date
CN203638095U true CN203638095U (en) 2014-06-11

Family

ID=50869362

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201320826112.3U Expired - Fee Related CN203638095U (en) 2013-12-13 2013-12-13 Unmanned mapping machine

Country Status (1)

Country Link
CN (1) CN203638095U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107554753A (en) * 2017-09-21 2018-01-09 王莎莎 One kind building municipal administration mapping unmanned plane

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107554753A (en) * 2017-09-21 2018-01-09 王莎莎 One kind building municipal administration mapping unmanned plane

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
PE01 Entry into force of the registration of the contract for pledge of patent right

Denomination of utility model: Unmanned mapping machine and tail wing for same

Effective date of registration: 20150209

Granted publication date: 20140611

Pledgee: Hunchun Jilin rural commercial bank Limited by Share Ltd

Pledgor: HUNCHUN GUOYAOBOCHENG TECHNOLOGY CO., LTD.

Registration number: 2015990000120

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: 20140611

Termination date: 20201213