CN106828898A - A kind of aircraft - Google Patents
A kind of aircraft Download PDFInfo
- Publication number
- CN106828898A CN106828898A CN201710007764.7A CN201710007764A CN106828898A CN 106828898 A CN106828898 A CN 106828898A CN 201710007764 A CN201710007764 A CN 201710007764A CN 106828898 A CN106828898 A CN 106828898A
- Authority
- CN
- China
- Prior art keywords
- fuselage
- rotor
- camera
- aircraft
- aircraft according
- 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.)
- Pending
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
Abstract
The present invention relates to technical field of aerospace, a kind of aircraft, including fuselage are referred in particular to, it is characterised in that：The bottom symmetrical of the fuselage is provided with support feet, and the fuselage is additionally provided with detector and camera；The support feet includes two connecting rods and balancing pole；The detector includes cylinder camera long, life-detection instrument and computer vision means, the cylinder camera long is connected to the bottom of the fuselage and is located between the support feet, and the life-detection instrument and the computer vision means are arranged on the fuselage interior；The camera is connected to the fuselage and is located at the lower section of the cylinder camera long.The present invention by being provided with camera and detector on board the aircraft, when aircraft enters scene of fire by camera and detector just can outwardly Real-time Feedback field data, so as to allow rescue personnel in time to determine the position of captive, Rapid Implementation rescue.
Description
Technical field
The present invention relates to technical field of aerospace, a kind of aircraft is referred in particular to.
Background technology
Increasingly faster with economic development, the city of current China has tended to build high buildings and large mansions and house is small
Area, the utilization rate of every inch of land is lifted with this, so as to more adapt to developing rapidly for city.
But, in this case, the density in house is very big, if a certain unit or a family occur fire, holds very much
Can easily grow in intensity, neighbouring unit or user be brought disaster to, so as to develop into conflagration.Once conflagration is developed into, due to dense
Cigarette is billowing and space that be related to is very big, therefore can cause that conflagration area becomes a piece of region that cannot be found out, so that very big
The rescue work of captive is have impact in degree.
The content of the invention
The present invention provides a kind of aircraft for problem of the prior art, by being equipped with identification equipment on board the aircraft and searching
Equipment is sought, after allowing aircraft smoothly can enter scene of fire, it is easier to find captive, shorten rescue time, from
And the low success rate for improving rescue of high degree.
In order to solve the above-mentioned technical problem, the present invention is adopted the following technical scheme that：
A kind of aircraft that the present invention is provided, including fuselage and the rotor mechanism being arranged on the fuselage, the fuselage bottom
Support feet is arranged with, the fuselage is additionally provided with detection device and camera；The support feet is connected to the fuselage including two
Connecting rod and be arranged on the balancing pole of the connecting rod bottom；The detection device includes cylinder camera long, life-detection instrument
And computer vision means, the cylinder camera long is connected to the bottom of the fuselage and is located between the support feet, described
Life-detection instrument and the computer vision means are arranged on the inside of the fuselage；The camera is connected to the fuselage and position
In the lower section of the cylinder camera long.
Further, the rotor mechanism includes six rotor assemblies being distributed along the fuselage even circumferential.
Further, the rotor assemblies include rotary blade, and rotary blade is made up of carbon-fiber composite material.
Further, the support feet is integrally formed, and the support feet two ends tilt upward to form hook.
Further, horizontal rotation head is provided between the camera and fuselage.
Further, it is provided with aviation flight logger between the fuselage and the horizontal rotation head.
Further, it is provided with communicator in the aviation flight logger.
Further, the rotor mechanism includes rotor and rotor connecting rod, and described rotor connecting rod one end is connected to
The fuselage, the other end is connected to the rotor, and the fuselage is provided with louvre with the rotor connecting rod junction.
Further, battery standing groove is provided with the middle part of the fuselage roof, is provided with the top of the battery standing groove
Bright protective cover.
Further, the fuselage interior is provided with control chip, and the control chip is made up of magnesium alloy；The fuselage by
Aluminium alloy is constituted.
Beneficial effects of the present invention：By being provided with camera and detector on board the aircraft, by detector, aircraft energy
It is enough to enter in scene of fire avoiding obstacles and find captive；By camera, aircraft can be the picture of scene of fire
Real-time Feedback, so as to allow the external world to formulate maximally effective rescue plan, is reduced as far as the loss that fire brings to extraneous.
Brief description of the drawings
Fig. 1 is overall structure diagram of the invention.
Fig. 2 is rearview of the invention.
Fig. 3 is top view of the invention.
Reference：1-fuselage, 2-support feet, 3-cylinder camera long, 4-camera, 5-aviation flight logger,
11-fuselage, 12-rotor, 14-horizontal rotation head, 21-connecting rod, 22-balancing pole, 111-louvre, 112-rotation
Wing connecting rod, 113-transparent protective shield.
Specific embodiment
For the ease of the understanding of those skilled in the art, the present invention is made further with reference to embodiment and accompanying drawing
It is bright, the content that implementation method is referred to not limitation of the invention.The present invention is described in detail below in conjunction with accompanying drawing.
As depicted in figs. 1 and 2, a kind of aircraft that the present invention is provided, including fuselage 1 and be arranged on the fuselage 1
Rotor mechanism, the bottom symmetrical of the fuselage 1 is provided with support feet 2, and the fuselage 1 is additionally provided with detection device and camera 4；The support
Pin 2 is connected to the connecting rod 21 of the fuselage 1 and is arranged on the balancing pole 22 of the bottom of the connecting rod 21 including two；The spy
Surveying device includes cylinder camera 3, life-detection instrument long and computer vision means, and the cylinder camera 3 long is connected to the machine
The bottom of body 1 is simultaneously located between the support feet, and the life-detection instrument and the computer vision means are arranged on the machine
The inside of body 1；The camera 4 is connected to the fuselage 1 and is located at the lower section of the cylinder camera 3 long.It should be noted that
In this aircraft, life detectors and computer vision means are all the equipment that can have been bought in the market, can be by peripheral hardware
Remote control and feedback-related information, are used to obtain and use very much；This aircraft uses life when scene of fire is entered
The wall that detector can pass through building searches captive by vital sign；Computer vision means can then allow this flight
Device independently avoids barrier, and without artificial operation, the aircraft for reducing artificial operational error and causing is damaged, and cylinder long is imaged
First 3 is that the function of life detectors and computer vision means is united, and can either carry out life detection, can be allowed again
The identification of this aircraft and avoiding obstacles.Meanwhile, support feet 2 is provided with this aircraft, can both allow this aircraft security, peace
Quietly land on the ground, can also be when this aircraft enters scene of fire toward hanging the things such as some towels, water in support feet 2
Product, captive can be saved oneself, so that when rescue personnel shows up.In addition, this aircraft is additionally provided with camera 4, with the external world
By wireless connection, for outwardly providing the situation inside scene of fire, be easy to find captive when rescue personnel can
The picture fed back by camera 4 formulates optimal rescue circuit.Cylinder camera 3 long and phase are provided with as on this aircraft simultaneously
Machine 4, then while being to allow this aircraft to be capable of identify that simultaneously avoiding obstacles, will not also lead because camera lens is only directed at barrier
Cause is not fed back to useful photo.
Further, the rotor mechanism includes six rotor assemblies being distributed along the even circumferential of the fuselage 1, due to
Scene of fire has too many uncertainty, and aircraft enters in it can meet various destabilizing factors, in some instances it may even be possible to meeting
There is the damage on rotor；Although and six rotorcraft is higher compared to common quadrotor cost, due to many
Two rotors thus redundancy more than quadrotor, with the stability and wind resistance more increased.
Further, the rotor 12 is made up of carbon-fiber composite material, necessary, and the composite has good resistance to height
Warm nature, can ensure that this aircraft being capable of normal work after entering fire rescue scene；Meanwhile, carbon-fiber composite material weight compared with
Small, rotor 12 makes the weight for being conducive to mitigating this aircraft using this material, so as to save energy consumption；Certainly, rotor 12 is more
Gently, the speed to be rotated just faster, effectively lifts the flying speed of this aircraft.
Further, the support feet 2 is integrally formed, and the two ends of the balancing pole 22 tilt upward to form hook.Balancing pole 22
Upwarping can allow the article hung on balancing pole 22 safer, will not easily this aircraft in flight course due to heat
Wave and drop.
Further, horizontal rotation head 14 is provided between the camera 4 and fuselage 1 so that camera 4 is in the horizontal direction
It is arbitrarily angled to be shot so that the picture for being transmitted to the external world becomes apparent from, and allows rescue personnel to become more apparent upon inside scene of fire
Situation, so as to make optimal plan, reduces the loss that fire brings.
Further, aviation flight logger 5 is additionally provided between the fuselage 1 and the horizontal rotation head 14, also
It is the black box being commonly called as.Black box is able to record that various data of the lower aircraft in flight course, if this aircraft
Except accident in scene of fire, then the reason for aircraft meets with an accidet can be would know that black box being taken out afterwards,
To summarize and making the measure for avoiding related accidents afterwards.
Further, communicator is additionally provided with the aviation flight logger 5, when aircraft can directly and captive
During contact, extraneous personnel can pacify captive by communicator, and guide captive to be saved oneself, it is to avoid captive is because of evil
Be afraid of and cause the situation of oneself further to deteriorate.
Further, as shown in figure 3, the rotor mechanism includes rotor 12 and rotor connecting rod 112, the rotor connects
The one end of extension bar 112 is connected to the fuselage 1, and the other end is connected to the rotor 12, the fuselage 1 and the rotor connecting rod
112 junctions are provided with louvre 111.Because rescue site flame spreads all over, the condition of high temperature is necessarily in, along with this aircraft
The heat that each part is produced during work so that this aircraft interior is in a condition of high temperature, if radiating not in time, it is easy to make
The working life for obtaining this aircraft is significantly reduced.And louvre 111 is arranged on the vicinity of rotor 12, can either ensure that and
When radiate, the air-flow for producing can be rotated by rotor 12 again and is entered in fuselage 11, reach the purpose of cooling, be effectively ensured this
The working life of aircraft.
Further, the middle at the top of the fuselage 11 is provided with battery standing groove, is set at the top of the battery standing groove
There is transparent protective shield 113.Battery standing groove is arranged on the top of fuselage 11, in addition to being convenient for changing, also helps battery
Radiating, prevent battery from being exploded because temperature is too high.And be provided with transparent protective shield 113, then observed when being advantageous for usually detecting
The situation of battery, if battery has exception the very first time can also to find and solve.
Further, the chip for controlling the aircraft is provided with inside the fuselage 1, the chip has magnesium alloy structure
Into；The fuselage 1 is made up of aluminium alloy.The part of the chip of this aircraft maneuvers is controlled to be magnesium alloy, due to magnesium alloy
Weight is very light, therefore this structure can effectively reduce the weight of aircraft, reduces the electricity needed for driving this aircraft, so that
Enable that battery is continued a journey the longer time；The fuselage of this aircraft uses aluminium alloy, and aluminium alloy is not only with outstanding resistance to height
Warm nature, additionally it is possible to prevent the vapor of scene of fire from entering in the fuselage of this aircraft so that this aircraft can be existing in fire
Field by temperature interference and normal work.
The above, is only present pre-ferred embodiments, and any formal limitation is not made to the present invention, although
The present invention is disclosed as above with preferred embodiment, but is not limited to the present invention, any those skilled in the art,
Do not depart from the range of technical solution of the present invention, when making a little change using the technology contents of the disclosure above or be modified to equivalent change
The Equivalent embodiments of change, as long as it, without departing from technical solution of the present invention content, refers to above example according to the technology of the present invention to be
Any simple modification, equivalent variations and the modification made, belong in the range of technical solution of the present invention.
Claims (10)
1. a kind of aircraft, including fuselage and the rotor mechanism being arranged on the fuselage, it is characterised in that：The bottom of the fuselage
Portion is arranged with support feet, and the fuselage is additionally provided with detection device and camera；The support feet is connected to the machine including two
The connecting rod of body and the balancing pole for being arranged on the connecting rod bottom；The detection device includes cylinder camera long, life detection
Instrument and computer vision means, the cylinder camera long are connected to the bottom of the fuselage and are located between the support feet, institute
State life-detection instrument and the computer vision means are arranged on the inside of the fuselage；The camera is connected to the fuselage simultaneously
Positioned at the lower section of the cylinder camera long.
2. a kind of aircraft according to claim 1, it is characterised in that：The rotor mechanism includes justifying along the fuselage
All equally distributed six rotor assemblies.
3. a kind of aircraft according to claim 2, it is characterised in that：The rotor assemblies include rotary blade, rotary blade
It is made up of carbon-fiber composite material.
4. a kind of aircraft according to claim 1, it is characterised in that：The support feet is integrally formed, the support feet
Tilt upward to form hook in two ends.
5. a kind of aircraft according to claim 1, it is characterised in that：Level rotation is provided between the camera and fuselage
Turn head.
6. a kind of aircraft according to claim 5, it is characterised in that：Between the fuselage and the horizontal rotation head
It is provided with aviation flight logger.
7. a kind of aircraft according to claim 6, it is characterised in that：Communication dress is provided with the aviation flight logger
Put.
8. a kind of aircraft according to claim 1, it is characterised in that：The rotor mechanism includes that rotor and rotor connect
Extension bar, described rotor connecting rod one end is connected to the fuselage, and the other end is connected to the rotor, the fuselage and the rotor
Connecting rod junction is provided with louvre.
9. a kind of aircraft according to claim 1, it is characterised in that：Battery placement is provided with the middle part of the fuselage roof
Groove, transparent protective shield is provided with the top of the battery standing groove.
10. a kind of aircraft according to claim 1, it is characterised in that：The fuselage interior is provided with control chip, described
Control chip is made up of magnesium alloy；The fuselage is made up of aluminium alloy.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710007764.7A CN106828898A (en) | 2017-01-05 | 2017-01-05 | A kind of aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710007764.7A CN106828898A (en) | 2017-01-05 | 2017-01-05 | A kind of aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106828898A true CN106828898A (en) | 2017-06-13 |
Family
ID=59117056
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710007764.7A Pending CN106828898A (en) | 2017-01-05 | 2017-01-05 | A kind of aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106828898A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110065627A (en) * | 2019-04-30 | 2019-07-30 | 中北大学 | A kind of bionical unmanned vehicle of multifunctional rescue |
| CN112766692A (en) * | 2021-01-12 | 2021-05-07 | 深圳市信拓网络科技有限公司 | Fire-fighting scheduling system for smart city and scheduling method thereof |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2009153588A1 (en) * | 2008-06-16 | 2009-12-23 | Middlesex University Higher Education Corporation | Compact unmanned aerial vehicle |
| CN202170018U (en) * | 2011-07-15 | 2012-03-21 | 东华大学 | Small-sized perpendicular taking off and landing unmanned plane for monitoring and fire fighting |
| CN102707724A (en) * | 2012-06-05 | 2012-10-03 | 清华大学 | Visual localization and obstacle avoidance method and system for unmanned plane |
| CN204895852U (en) * | 2015-08-12 | 2015-12-23 | 润泰救援装备科技河北有限公司 | Rescue investigation unmanned aerial vehicle |
| KR20160103586A (en) * | 2015-02-24 | 2016-09-02 | 주식회사 공간정보 | Unmanned Aerial Vehicle System For Broadcasting Distress Research And Emergency Guide |
-
2017
- 2017-01-05 CN CN201710007764.7A patent/CN106828898A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2009153588A1 (en) * | 2008-06-16 | 2009-12-23 | Middlesex University Higher Education Corporation | Compact unmanned aerial vehicle |
| CN202170018U (en) * | 2011-07-15 | 2012-03-21 | 东华大学 | Small-sized perpendicular taking off and landing unmanned plane for monitoring and fire fighting |
| CN102707724A (en) * | 2012-06-05 | 2012-10-03 | 清华大学 | Visual localization and obstacle avoidance method and system for unmanned plane |
| KR20160103586A (en) * | 2015-02-24 | 2016-09-02 | 주식회사 공간정보 | Unmanned Aerial Vehicle System For Broadcasting Distress Research And Emergency Guide |
| CN204895852U (en) * | 2015-08-12 | 2015-12-23 | 润泰救援装备科技河北有限公司 | Rescue investigation unmanned aerial vehicle |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110065627A (en) * | 2019-04-30 | 2019-07-30 | 中北大学 | A kind of bionical unmanned vehicle of multifunctional rescue |
| CN112766692A (en) * | 2021-01-12 | 2021-05-07 | 深圳市信拓网络科技有限公司 | Fire-fighting scheduling system for smart city and scheduling method thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20170613 |