CN205931282U - Helicopter and machine carries equipment fixing platform thereof - Google Patents
Helicopter and machine carries equipment fixing platform thereof Download PDFInfo
- Publication number
- CN205931282U CN205931282U CN201620921658.0U CN201620921658U CN205931282U CN 205931282 U CN205931282 U CN 205931282U CN 201620921658 U CN201620921658 U CN 201620921658U CN 205931282 U CN205931282 U CN 205931282U
- Authority
- CN
- China
- Prior art keywords
- platform
- airborne equipment
- main shaft
- helicopter
- equipment mounting
- 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.)
- Active
Links
Landscapes
- Toys (AREA)
Abstract
The utility model discloses a helicopter and machine carries equipment fixing platform thereof, include with organism fixed connection's back shaft with be used for the mounting plate to carry the platform of equipment, the back shaft establish in hollow main shaft and with the coaxial setting of main shaft, the main shaft is stretched out on the top of back shaft, platform fixed mounting is on the top of back shaft, and the axis perpendicular to platform of back shaft, an equipment also is more convenient for installing and is dismantled, consequently that is used for the platform that the mounting plate carried equipment to establish directly over the main shaft, and keeps can not rotating at aircraft flight in -process platform, and then the platform can provide the installation space of full visual angle, multidimension degree for the airborne equipment, and the airborne equipment can not receive helicopter rotor's interference, also can not influence the center of gravity of airplane, because the organism headroom is well -to -do, install on the platform in addition the utility model provides a machine carries the flight performance that the equipment fixing platform can satisfy the user demand and not influence the helicopter.
Description
Technical field
This utility model is related to the installing area of airborne equipment, more particularly to a kind of airborne equipment mounting platform.Additionally,
This utility model further relates to a kind of helicopter including above-mentioned airborne equipment mounting platform.
Background technology
With scientific and technical development, helicopter taking pictures, image, explore, the field such as pesticide spraying is all widely used.
Using helicopter as an airflight platform, carry various related equipment it is possible to realize corresponding function.
Application apparatus on existing helicopter, such as radar, photoelectric nacelle, picture pick-up device etc. is arranged on helicopter head
Position, its shortcoming is that the visual field has limitation, can only observe the sector region of aircraft forward, equipment is produced with observation dead angle, no
Meet use demand；In addition the weight of airborne equipment is had nothing in common with each other, and on same frame helicopter, changes in switching task and accordingly sets
When standby, it will because of the center of gravity of the impact aircraft that varies in weight, thus the flight quality to aircraft and flight safety produce larger shadow
Ring.
Therefore how the installation of airborne equipment meets use demand and not affect the flying quality of helicopter be this area skill
The current technical issues that need to address of art personnel.
Utility model content
The purpose of this utility model is to provide a kind of airborne equipment mounting platform, and its structure design can make airborne equipment
The flying quality meeting use demand and not affecting helicopter is installed.Of the present utility model another object is that was provided on a kind of inclusion
State the helicopter of airborne equipment mounting platform.
For solving above-mentioned technical problem, this utility model provides a kind of airborne equipment mounting platform, fixes including with body
The support shaft connecting and the platform for installing airborne equipment, described support shaft is located in the main shaft of hollow and same with described main shaft
Axle is arranged, and described main shaft is stretched out on the top of described support shaft, and described platform is fixedly mounted on the top of described support shaft, and described
The axis of support shaft is perpendicular to described platform.
Preferably, described platform and described main shaft are rotatably connected.
Preferably, it is machined with the mounting groove for installing bearing below described platform, outside described main shaft, be fixedly connected with set
Cylinder, described sleeve is fixedly connected with the inner ring of described bearing, and described platform is fixedly connected with the outer ring of described bearing.
Preferably, the horizontal plane of described platform is provided with multiple hole slots.
Preferably, described platform is regular polygon.
Preferably, described support shaft is quill shaft.
This utility model also provides a kind of helicopter, including body and airborne equipment mounting platform, described airborne equipment peace
Assembling platform is specially the airborne equipment mounting platform described in above-mentioned any one.
The airborne equipment mounting platform that this utility model provides, including the support shaft being fixedly connected with body be used for installing
The platform of airborne equipment, support shaft is located in the main shaft of hollow and is coaxially disposed with main shaft, and main shaft is stretched out on the top of support shaft, puts down
Platform is fixedly mounted on the top of support shaft, and the axis of support shaft is perpendicular to platform；Platform for installing airborne equipment is located at
The surface of main shaft, and platform keeps rotating in aircraft flight, then platform can provide for airborne equipment and entirely regard
Angle, the installing space of various dimensions, and airborne equipment will not be disturbed by lifting airscrew, also do not interfere with the center of gravity of airplane, separately
Outward because body headroom is well-to-do, the equipment being arranged on platform is also more convenient for installing and dismounting, and therefore this utility model carries
For airborne equipment mounting platform disclosure satisfy that use demand and do not affect the flying quality of helicopter.
The helicopter that this utility model provides includes above-mentioned airborne equipment mounting platform, is installed due to above-mentioned airborne equipment and puts down
Platform has above-mentioned technique effect, and above-mentioned helicopter also should have same technique effect, and here is no longer discussed in detail.
Brief description
Fig. 1 is a kind of structural representation of specific embodiment of airborne equipment mounting platform provided by the utility model
Figure；
Fig. 2 is the Section A-A schematic diagram of Fig. 1；
Fig. 3 is the top view of Fig. 1.
Specific embodiment
Core of the present utility model is to provide a kind of airborne equipment mounting platform, and its structure design can make airborne equipment
The flying quality meeting use demand and not affecting helicopter is installed.Another core of the present utility model is to provide on a kind of inclusion
State the helicopter of airborne equipment mounting platform.
In order that those skilled in the art more fully understand this utility model scheme, below in conjunction with the accompanying drawings and be embodied as
The utility model is described in further detail for mode.
Refer to Fig. 1 to Fig. 3, Fig. 1 is that one kind of airborne equipment mounting platform provided by the utility model is embodied as
The structural representation of mode；Fig. 2 is the Section A-A schematic diagram of Fig. 1；Fig. 3 is the top view of Fig. 1.
The airborne equipment mounting platform that this utility model specific embodiment provides, including the support being fixedly connected with body
Axle 1 and for installing the platform 2 of airborne equipment, main shaft adopts hollow structure, and the support shaft 1 for mounting platform 2 is arranged on
In empty main shaft 5, and support shaft 1 is coaxially disposed with main shaft 5, and main shaft 5 is stretched out on the top of support shaft 1, and platform 2 is fixedly mounted on and props up
The top of support axle 1, and the axis of support shaft 1 is perpendicular to platform 2.
Support shaft 1 is fixedly connected with body, for airborne equipment is installed platform 2 with main shaft 5 in vertical direction, then be used for
The platform 2 installing airborne equipment is located at the surface of main shaft 5, and in aircraft flight, platform 2 keeps rotating, then put down
Platform 2 can provide the installing space of full visual angle, various dimensions for airborne equipment, and airborne equipment will not be done by lifting airscrew
Disturb, also do not interfere with the center of gravity of airplane, well-to-do additionally, due to body headroom, the equipment being arranged on platform 2 is also more convenient for pacifying
Dress and dismounting, the airborne equipment mounting platform that therefore this utility model provides disclosure satisfy that use demand and do not affect helicopter
Flying quality.
The airborne equipment mounting platform that this utility model specific embodiment provides, main shaft 5 is with engine drive mechanism even
Connect, main shaft 5 can rotate in flight course, rock for reducing platform 2, and ensure that platform 2 will not rotate with main shaft 5 and rotates,
Platform 2 is preferably rotatably connected with main shaft 5.
Being rotatably connected between platform 2 and main shaft 5 has various ways it is achieved that platform 2 and main shaft 5 can pass through axle
Hold 3 to be rotatably connected, bearing 3 frictional resistance is little, easy for installation；Specifically, can be machined with for installation axle below platform 2
Hold 3 mounting groove, that is, bearing 3 is located in mounting groove, be fixedly connected with sleeve 4 outside main shaft 5, and make the interior of sleeve 4 and bearing 3
Circle is fixedly connected, and platform 2 is fixedly connected with the outer ring of bearing 3, so both can ensure that platform 2 will not rotate with main shaft 5, and might be used again
Will not be swung in horizontal direction because of the work of aircraft with guarantee platform 2, so that the horizontal plane of platform 2 is kept with main shaft 5 all the time
Vertically.
On the basis of any of the above-described specific embodiment, for the ease of the installation of airborne equipment, in the horizontal plane of platform 2
On can be provided with multiple hole slots 6, for airborne equipment provide mount point, simultaneously can also for mitigate platform 2 weight；Hole slot 6 exists
Can be uniformly distributed around platform 2 center on the horizontal plane of platform 2, be conducive to platform 2 and support shaft 1 stress balance.Hole slot 6
Quantity, shape and the concrete set-up mode on platform 2 all can designed, designed and processing as needed, all in this utility model
Protection domain within.
In addition, platform 2 is specifically as follows regular polygon structure, in order to process, it is easy to the positioning of hole slot 6, specifically, put down
Platform 2 can be octagon.Certainly the concrete shape of platform 2 is not limited to this, can voluntarily adjust as needed, all in this reality
Within new protection domain.
On the basis of any of the above-described specific embodiment, support shaft 1 can be quill shaft, as hollow axle, so, peace
It is contained in power line needed for the airborne equipment on platform 2, data wire etc., all can pass through inside support shaft 1, be connected to machine
Body, is connected with device power supply (DPS) etc., facilitates line facility and ensure safety, and in addition support shaft 1 adopts hollow structure acceptable
Mitigate weight, increase aircraft motility.Support shaft 1 can not also be using hollow structure it is also possible to realize line by other means
The setting on road and connection, all within protection domain of the present utility model.
Except above-mentioned airborne equipment mounting platform, specific embodiment of the present utility model also provides a kind of inclusion above-mentioned machine
The helicopter of load equipment mounting platform, the structure of this other each several part of helicopter refer to prior art, repeats no more herein.
Above helicopter provided by the utility model and its airborne equipment mounting platform are described in detail.Herein
In apply specific case principle of the present utility model and embodiment be set forth, the explanation of above example is to use
Understand method of the present utility model and its core concept in help.It should be pointed out that for those skilled in the art
For, on the premise of without departing from this utility model principle, this utility model can also be carried out with some improvement and modify, these
Improve and modification also falls in this utility model scope of the claims.
Claims (7)
1. a kind of airborne equipment mounting platform it is characterised in that include is fixedly connected with body support shaft (1) and be used for installing
The platform (2) of airborne equipment, described support shaft (1) is located in the main shaft (5) of hollow and is coaxially disposed with described main shaft (5), institute
Described main shaft (5) is stretched out on the top stating support shaft (1), and described platform (2) is fixedly mounted on the top of described support shaft (1), and
The axis of described support shaft (1) is perpendicular to described platform (2).
2. airborne equipment mounting platform according to claim 1 is it is characterised in that described platform (2) and described main shaft (5)
It is rotatably connected.
3. airborne equipment mounting platform according to claim 2 is it is characterised in that be machined with use below described platform (2)
It is fixedly connected with sleeve (4), described sleeve (4) and described bearing (3) outside the mounting groove installing bearing (3), described main shaft (5)
Inner ring be fixedly connected, described platform (2) is fixedly connected with the outer ring of described bearing (3).
4. airborne equipment mounting platform according to claim 1 is it is characterised in that set on the horizontal plane of described platform (2)
There are multiple hole slots (6).
5. airborne equipment mounting platform according to claim 4 is it is characterised in that described platform (2) is regular polygon.
6. the airborne equipment mounting platform according to claim 1 to 5 any one is it is characterised in that described support shaft (1)
For quill shaft.
7. a kind of helicopter, including body and airborne equipment mounting platform it is characterised in that described airborne equipment mounting platform has
Body is the airborne equipment mounting platform described in claim 1 to 6 any one.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620921658.0U CN205931282U (en) | 2016-08-23 | 2016-08-23 | Helicopter and machine carries equipment fixing platform thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620921658.0U CN205931282U (en) | 2016-08-23 | 2016-08-23 | Helicopter and machine carries equipment fixing platform thereof |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205931282U true CN205931282U (en) | 2017-02-08 |
Family
ID=57950937
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620921658.0U Active CN205931282U (en) | 2016-08-23 | 2016-08-23 | Helicopter and machine carries equipment fixing platform thereof |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205931282U (en) |
-
2016
- 2016-08-23 CN CN201620921658.0U patent/CN205931282U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN103287587B (en) | A kind of vertical take-off and landing aircraft (VTOL aircraft) ground simulated flight test platform | |
| CN209458620U (en) | Multiple degrees of freedom ground motion simulator for aerial camera test | |
| CN104881049B (en) | Unmanned plane pan-shot head in the confined space | |
| CN110261057A (en) | A kind of lifting airscrew, fuselage and tail-rotor built-up pattern wind tunnel test system | |
| CN102779438B (en) | Flight simulated mechanical execution system simulating full-motion of airplane | |
| CN105857628A (en) | Self-balancing anti-collision aircraft | |
| CN209455024U (en) | A kind of mixed connection multiple degrees of freedom rotor wing unmanned aerial vehicle ground simulation platform | |
| CN207670659U (en) | A kind of upper and lower six rotor wing unmanned aerial vehicles of three-axis stability augmentation | |
| CN103112587A (en) | Aircraft | |
| CN205931282U (en) | Helicopter and machine carries equipment fixing platform thereof | |
| CN103473363A (en) | Base station high-altitude inspection system based on aircraft and inspection method of base station high-altitude inspection system | |
| CN209700924U (en) | A kind of unmanned plane during flying body with cage shape shielded frame | |
| CN108725817A (en) | A kind of four axis unmanned planes with stabilization function | |
| CN205469808U (en) | Photovoltaic power plant detection device | |
| CN108248849A (en) | A kind of improved double-deck rotor wing unmanned aerial vehicle | |
| CN209209056U (en) | Portable multifunctional unmanned plane landing platform | |
| CN205931255U (en) | Spherical unmanned aerial vehicle based on ARM | |
| CN206782043U (en) | A kind of Rapid Combination multi-rotor unmanned aerial vehicle structure | |
| CN205642790U (en) | Aircraft strutting arrangement | |
| CN206427280U (en) | Become more meticulous the unmanned plane of inspection for power network conveying circuit shaft tower | |
| CN205971822U (en) | Unmanned aerial vehicle's delivery host computer | |
| CN213502887U (en) | Unmanned aerial vehicle flight platform capable of accurately throwing aerial materials | |
| CN108100276A (en) | A kind of multiple degrees of freedom error-compensating apparatus | |
| CN108557094A (en) | A kind of multi-functional unmanned plane | |
| CN207751666U (en) | A kind of double rotating shaft supporting mechanisms for wind tunnel test |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20211216 Address after: 410000 room 52, door 5, building 30, No. 114, xinkaipu Road, Tianxin District, Changsha City, Hunan Province Patentee after: Li Jun Address before: 410000 carton factory of nantuoling community, NANTUO street, Tianxin District, Changsha City, Hunan Province Patentee before: HUNAN KUTA TECHNOLOGY Co.,Ltd. |
|
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20230719 Address after: 110000 Shenyang General Aviation Industrial Base, Liaoning Province Patentee after: Faku Zhongjun Wing UAV Technology Co.,Ltd. Address before: 410000 room 52, door 5, building 30, No. 114, xinkaipu Road, Tianxin District, Changsha City, Hunan Province Patentee before: Li Jun |