CN107878769A - A kind of unmanned plane mounting bracket and its unmanned plane - Google Patents
A kind of unmanned plane mounting bracket and its unmanned plane Download PDFInfo
- Publication number
- CN107878769A CN107878769A CN201710868195.5A CN201710868195A CN107878769A CN 107878769 A CN107878769 A CN 107878769A CN 201710868195 A CN201710868195 A CN 201710868195A CN 107878769 A CN107878769 A CN 107878769A
- Authority
- CN
- China
- Prior art keywords
- mounting bracket
- unmanned plane
- installing plate
- transmission system
- 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.)
- Pending
Links
- 230000005540 biological transmission Effects 0.000 claims abstract description 43
- 238000009434 installation Methods 0.000 claims abstract description 15
- 238000000034 method Methods 0.000 claims abstract description 6
- 239000002828 fuel tank Substances 0.000 claims description 10
- 238000004080 punching Methods 0.000 claims description 3
- 230000000930 thermomechanical effect Effects 0.000 abstract description 3
- 238000012423 maintenance Methods 0.000 description 5
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000003467 diminishing effect Effects 0.000 description 1
- 238000005183 dynamical system Methods 0.000 description 1
- 238000003384 imaging method Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
- B64D31/14—Transmitting means between initiating means and power plants
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D35/00—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D37/00—Arrangements in connection with fuel supply for power plant
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Wind Motors (AREA)
Abstract
The present invention provides a kind of unmanned plane mounting bracket and its unmanned plane, including：Mounting bracket body and be mechanical erection plate, the mechanical erection plate is vertically fixed on the mounting bracket body by auxiliary member, photoelectric nacelle mounting groove is provided with the mounting bracket body, and be arranged at the mechanical erection plate for installation site on transmission system mounting groove；The assembling of unmanned thermomechanical components is carried out by unmanned plane mounting bracket provided by the invention, all component on unmanned plane all can be realized fixation by the mounting bracket, fixed structure need not be designed on the shell of unmanned plane, only need mounting bracket being fixed on unmanned plane shell, which not only simplifies the structure design of shell, also reduce the assembling difficulty of unmanned plane, and assembled by the mounting bracket, substantially increase the difficulty of the process such as the efficiency of assembling and the maintaining in later stage.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, more particularly to unmanned plane mounting bracket and its unmanned plane.
Background technology
In the Small Civil unmanned aerial vehicle of Current Domestic, in order to the power drive more stablized, it is typically all
Using petrol engine as active force, the installation for fuel tank and dynamical system, the mounting means often used at present is straight
Connect in the inner space for being fixed on aircraft, and this kind of mounting means need it is extremely complex to the design of the interior spatial structure of aircraft,
It is required that it is also very high, and the structure of this mounting means can not realize general assembling, assembling, maintenance and phase in the later stage
When it is inconvenient.Therefore, being badly in need of one kind can realize to the installation of unmanned aerial vehicle component, and the simple unmanned plane peace of design structure
It is above-mentioned to solve the problems, such as to fill support.
The content of the invention
Above-mentioned technical problem is directed to, the present invention proposes a kind of unmanned plane mounting bracket and its unmanned plane, existing to solve
There is the problem of unmanned plane assembling in technology is difficult, maintenance is inconvenient and complicated.
In order to solve the above technical problems, the present invention provides a kind of unmanned plane mounting bracket, including：Mounting bracket body and machine
Tool installing plate, the mechanical erection plate are vertically fixed on the mounting bracket body by auxiliary member；
Photoelectric nacelle mounting groove is provided with the mounting bracket body, and is arranged at corresponding to the mechanical erection plate
Transmission system mounting groove in installation site.
In another embodiment of the invention, flange is additionally provided with the edge of the mounting bracket body, its
Described in mounting bracket body front and rear sides edge and right side edge on flange setting direction be along it is described installation branch
The surface of frame body upwardly extends, and the flange setting direction in left side edge is downward along the surface of the mounting bracket body
Extension.
In another embodiment of the invention, the photoelectric nacelle mounting groove includes being arranged on the mounting bracket body
A circular perforations, a hollow cylinder is additionally provided with the edge of the circular perforations.
In another embodiment of the invention, the transmission system mounting groove includes two interconnected grooves, described
Groove is to carry out punching press on the surface of the mounting bracket body by mechanical stamping process so that the surface is to recessed institute's shape
Into.
In another embodiment of the invention, a perforation is additionally provided with the bottom of the groove, described perforate is used for
Power transmission shaft in the transmission system is installed.
In another embodiment of the invention, be additionally provided with the symmetrical both sides of the edge of transmission system mounting groove with
The first mounting hole that the auxiliary member cooperates.
In another embodiment of the invention, the mechanical erection plate includes the first installing plate and the second installing plate, in institute
State and the symmetrical neck being engaged with the drive system structure is provided with the first installing plate and the second installing plate；
In assembling, first installing plate and second installing plate are parallel to each other admittedly by the auxiliary member
It is scheduled on the first mounting hole of the transmission system mounting groove.
In another embodiment of the invention, the mechanical erection plate also includes the 3rd installing plate, the 3rd installing plate
It is vertically installed in the transmission system mounting groove on a side in the installing plate body centre position, for supporting
State the first installing plate and the second installing plate.
In another embodiment of the invention, the installing plate body also includes the second mounting hole, second mounting hole
It is arranged on the edge position of the installing plate body, for the fuel tank of unmanned plane to be fixed on into the installing plate body
On lower surface.
In order to solve upper technical problem, the present invention also provides a kind of unmanned plane, including：Camera, transmission system, fuel tank and
As above the unmanned plane mounting bracket described in any one, the camera are arranged on the photoelectric nacelle mounting groove, the transmission
System is arranged on the transmission system mounting groove, and the fuel tank is arranged on the lower surface of the mounting bracket body.
The beneficial effects of the invention are as follows：
According to unmanned plane mounting bracket provided by the invention and its unmanned plane, including：Mounting bracket body and be mechanical peace
Loading board, the mechanical erection plate are vertically fixed on the mounting bracket body by auxiliary member, in the mounting bracket body
Be provided with photoelectric nacelle mounting groove, and be arranged at the mechanical erection plate for installation site on transmission system install
Groove；The assembling of unmanned thermomechanical components is carried out by unmanned plane mounting bracket provided by the invention, can be by all groups on unmanned plane
Part all realizes fixation by the mounting bracket, it is not necessary to designs fixed structure on the shell of unmanned plane, it is only necessary to will install
Support is fixed on unmanned plane shell, and which not only simplifies the structure design of shell, also reduces the assembling of unmanned plane
Difficulty, and assembled by the mounting bracket, substantially increase the process such as the efficiency of assembling and the maintaining in later stage
Difficulty.
Brief description of the drawings
Fig. 1 is the structural representation of unmanned plane mounting bracket provided in an embodiment of the present invention；
Fig. 2 is the lateral plan of mounting bracket body provided in an embodiment of the present invention；
Fig. 3 is the structural representation of mounting bracket body provided in an embodiment of the present invention；
Fig. 4 is the lateral plan of mounting bracket body provided in an embodiment of the present invention；
Fig. 5 is the structural representation of unmanned plane provided in an embodiment of the present invention.
Embodiment
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is carried out clear, complete
Site preparation describes, it is clear that described embodiment is part of the embodiment in the present invention, rather than whole embodiments.It is based on
Embodiment in the present invention, those of ordinary skill in the art are obtained every other under the premise of creative work is not made
Embodiment, belong to the scope of protection of the invention.
Further annotation explanation is now made to the present invention by way of embodiment combination accompanying drawing.
Fig. 1 is the structural representation of unmanned plane mounting bracket provided in an embodiment of the present invention, from Fig. 1,2, this implementation
The unmanned plane mounting bracket 1 that example provides includes：Mounting bracket body 11 and mechanical erection plate 12, wherein the mechanical erection plate 12
It is to realize to be vertically fixed on the mounting bracket body 11 by auxiliary member 13, specifically, first passing through auxiliary member described in screw
13 are fixed on the mechanical erection plate 12, and the auxiliary member 13 then is being fixed on into the installation branch by another screw
On screwed hole on frame 11, it is achieved thereby that assembling of the mechanical erection plate 12 on mounting bracket body 11, it is preferred that the spiral shell
Nail can be rivet or drive screw.
In the present embodiment, photoelectric nacelle mounting groove 111 and transmission system are additionally provided with the mounting bracket body 11
Mounting groove 112, wherein the photoelectric nacelle mounting groove 111 is arranged on the left end position of the mounting bracket body 11,
And the photoelectric nacelle refers to imaging the supervising device of first-class classification；The set location of the transmission system mounting groove 112 and institute
Fixed position of the mechanical erection plate 12 on mounting bracket body 11 is stated to corresponding to, the transmission system mounting groove 112 is used for group
The transmission system of the unmanned plane is filled, and with reference to the mechanical erection plate 12 come the assembling that interfixes.
As shown in Figure 3,4, the present embodiment provides mounting bracket body 11 and is additionally provided with flange 113, and the flange 113 is mainly
It is arranged on the edge position of the mounting bracket body 11, specifically, when setting by the flange on four edges
The direction of one side flange 113 be arranged in opposite direction with the flange on other three sides 113, it is preferred that by the mounting bracket
The setting direction of flange 113 on the front and rear sides edge and right side edge of body 11 is along the mounting bracket body 11
Surface upwardly extends, and the setting direction of flange 113 in left side edge is along the surface of the mounting bracket body 11 to downward
Stretch, left side edge here is referred to close to a side of photoelectric nacelle mounting groove 111, it is preferred that can be by the installation branch
Frame body 11 is designed as the installing plate of " tadpole " shape, and " tadpole " shape refers to that this size change turns in installation
One end of installing plate is to the diminishing variation tendency of the other end.
In actual applications, the unmanned plane mounting bracket 1 is fixed on the unmanned plane for the ease of staff
On shell, screwed hole 114 is also set up on the flange 113 of the mounting bracket body 11, in assembling, institute is passed through by rivet
Stating screwed hole 114 can be assembled in the unmanned plane mounting bracket 1 on the shell of unmanned plane, and such structure design is not only big
The big assembling difficulty for reducing unmanned plane, it is also convenient for later maintenance maintenance of the staff to unmanned plane.Staff is safeguarding
When, it is only necessary to take the various assemblies that the part enclosure of unmanned plane can be clear from mounting bracket 1 apart, it is very convenient, also contract
The short maintenance duration of staff.
In the present embodiment, the photoelectric nacelle mounting groove 111 includes a circular perforations 111a and hollow cylinder
111b, the circular perforations 111a are specifically provided in a through hole on the mounting bracket body 11, the hollow circle
Cylinder 111b be with the edge of the circular perforations 111a；In actual applications, when in the photoelectric nacelle mounting groove
When camera is installed on 111, the main body of the camera is fixed on the hollow cylinder 111b, the letter of the camera
Number line then sequentially passes through the cylinder 111b and circular perforations 111a and the control being fixed on the mounting bracket body 11
Device connects.
In the present embodiment, the transmission system of the unmanned plane includes uni-drive gear box and reduction gear box, in order to adapt to
The installation of the transmission system, the structure specific design of the transmission system mounting groove is by two interconnected grooves, is respectively
First groove 112a and the second groove 112b, in actual applications, the first groove 112a are used to place in transmission system
Uni-drive gear box, the second groove 112b are used to place the reduction gear box in transmission system.
Preferably, the shape after the first groove 112a and the second groove 112b connections is similar to I-shaped, is adding
Described in work during the first groove 112a and the second groove 112b, particular by mechanical stamping process in the mounting bracket body 11
Surface carry out punching press so that the surface of mounting bracket body 11 is formed to recessed；Further, due in uni-drive gear box
It is middle to have prominent power transmission shaft, therefore, the 112c that perforates is additionally provided with the bottom of the first groove 112a, it is described to wear
Hole 112c is used to install the power transmission shaft in the transmission system.
In the present embodiment, be additionally provided with the 113 symmetrical both sides of the edge of transmission system mounting groove with it is described auxiliary
The first mounting hole 113d that assistant piece 13 cooperates；The mechanical erection plate 12 includes the first installing plate 121 and the second installing plate
122, in assembling, the installing plate 122 of the first installing plate 121 and second is arranged in parallel, and passes through the auxiliary member 13
It is fixed on the first mounting hole 112d of the mounting bracket body 11；In actual applications, in order to coordinate the knot of transmission system
Structure designs, and is provided with and symmetrical is engaged with the drive system structure on first installing plate and the second installing plate
Neck 12a.
In the present embodiment, the mechanical erection plate 12 also includes the 3rd installing plate 123, and the 3rd installing plate 123 hangs down
Directly it is arranged in the transmission system mounting groove 112 on a side in the centre position of installing plate body 11, for propping up
Support the installing plate 122 of the first installing plate 121 and second, it is preferred that the 3rd installed part 123 is " people " font.
In the present embodiment, the installing plate body 11 also includes the second mounting hole 115, and second mounting hole 115 is set
It is placed on the edge position of the installing plate body 11, for the fuel tank of unmanned plane to be fixed on into the installing plate body 11
Lower surface on.
Accordingly, present invention also offers a kind of unmanned plane, the unmanned plane to include：Camera 21, transmission system 22,
Fuel tank 23 and the unmanned plane mounting bracket 1 described in example is performed as described above, the camera 21 is arranged at the photoelectric nacelle mounting groove
On 111, the transmission system 22 is arranged on the transmission system mounting groove 112, and the fuel tank 23 is arranged at the installation branch
On the lower surface of frame body 11.
As shown in figure 5, the transmission system 22 is specifically provided in the installing plate 122 of the first installing plate 121 and second
Between position, and uni-drive gear box in the transmission system 21 and reduction gear box be respectively placed in the first groove 112a and
In second groove 112b；The avionics system 24 and propeller control dress of unmanned plane are additionally provided with the mounting bracket body 11
25 are put, the avionics system 24 gathers the ambient parameter on unmanned plane during flying direction, the avionics system 24 by camera 21
The elevation angle of blade in the propeller control device 25 according to the environment parameter control collected, so as to control the flight of unmanned plane
Direction and avoiding barrier etc..
In summary, unmanned plane mounting bracket provided by the invention and its unmanned plane, including：Mounting bracket body and be machine
Tool installing plate, the mechanical erection plate is vertically fixed on the mounting bracket body by auxiliary member, in the mounting bracket
Body is provided with photoelectric nacelle mounting groove, and be arranged at the mechanical erection plate for installation site on transmission system pacify
Tankage；The assembling of unmanned thermomechanical components is carried out by unmanned plane mounting bracket provided by the invention, can will be on unmanned plane it is all
Component all realizes fixation by the mounting bracket, it is not necessary to designs fixed structure on the shell of unmanned plane, it is only necessary to will pacify
Dress support is fixed on unmanned plane shell, which not only simplifies the structure design of shell, also reduces the group of unmanned plane
Difficulty is filled, and is assembled by the mounting bracket, substantially increases the work such as the efficiency of assembling and the maintaining in later stage
The difficulty of sequence.
Above content is to combine specific embodiment further description made for the present invention, it is impossible to assert this hair
Bright specific implementation is confined to these explanations.For general technical staff of the technical field of the invention, do not taking off
On the premise of from present inventive concept, some simple deduction or replace can also be made, should all be considered as belonging to the protection of the present invention
Scope.
Claims (10)
1. a kind of unmanned plane mounting bracket, its spy are characterised by, including：Mounting bracket body and mechanical erection plate, the machinery
Installing plate is vertically fixed on the mounting bracket body by auxiliary member；
Photoelectric nacelle mounting groove is provided with the mounting bracket body, and is arranged at corresponding to the mechanical erection plate and installs
Transmission system mounting groove on position.
2. unmanned plane mounting bracket as claimed in claim 1, it is characterised in that in the edge of the mounting bracket body
On be additionally provided with flange, wherein the flange setting direction in the front and rear sides edge of the mounting bracket body and right side edge
To be upwardly extended along the surface of the mounting bracket body, the flange setting direction in left side edge is along the installation branch
The surface of frame body extends downwardly.
3. unmanned plane mounting bracket as claimed in claim 2, it is characterised in that the photoelectric nacelle mounting groove includes being arranged on
A circular perforations on the mounting bracket body, be additionally provided with the edge of the circular perforations one it is hollow
Cylinder.
4. unmanned plane mounting bracket as claimed in claim 1, it is characterised in that the transmission system mounting groove includes two phases
Intercommunicated groove, the groove are to carry out punching press on the surface of the mounting bracket body by mechanical stamping process so that
The surface is formed to recessed.
5. unmanned plane mounting bracket as claimed in claim 4, it is characterised in that be additionally provided with one in the bottom of the groove
Perforation, the power transmission shaft perforated for installing in the transmission system.
6. the unmanned plane mounting bracket as described in claim any one of 1-5, it is characterised in that in the transmission system mounting groove
The first mounting hole to be cooperated with the auxiliary member is additionally provided with symmetrical both sides of the edge.
7. unmanned plane mounting bracket as claimed in claim 6, it is characterised in that the mechanical erection plate includes the first installing plate
With the second installing plate, it is provided with first installing plate and the second installing plate symmetrical with the drive system structure
The neck being engaged；
In assembling, first installing plate and second installing plate are parallel to each other and be fixed on by the auxiliary member
On first mounting hole of the transmission system mounting groove.
8. unmanned plane mounting bracket as claimed in claim 7, it is characterised in that the mechanical erection plate also includes the 3rd installation
Plate, the 3rd installing plate are vertically installed in the transmission system mounting groove close to the one of the installing plate body centre position
On side, for supporting first installing plate and the second installing plate.
9. unmanned plane mounting bracket as claimed in claim 8, it is characterised in that the installing plate body also includes the second installation
Hole, second mounting hole are arranged on the edge position of the installing plate body, for the fuel tank of unmanned plane to be fixed
In on the lower surface of the installing plate body.
A kind of 10. unmanned plane, it is characterised in that including：Camera, transmission system, fuel tank and such as any one of claim 1-9 institutes
The unmanned plane mounting bracket stated, the camera are arranged on the photoelectric nacelle mounting groove, and the transmission system is arranged at institute
State on transmission system mounting groove, the fuel tank is arranged on the lower surface of the mounting bracket body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710868195.5A CN107878769A (en) | 2017-09-22 | 2017-09-22 | A kind of unmanned plane mounting bracket and its unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710868195.5A CN107878769A (en) | 2017-09-22 | 2017-09-22 | A kind of unmanned plane mounting bracket and its unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107878769A true CN107878769A (en) | 2018-04-06 |
Family
ID=61780706
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710868195.5A Pending CN107878769A (en) | 2017-09-22 | 2017-09-22 | A kind of unmanned plane mounting bracket and its unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107878769A (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2920344Y (en) * | 2005-12-06 | 2007-07-11 | 杜大森 | Remote controled helicopter fuselage cradle structure |
| CN203001967U (en) * | 2012-12-06 | 2013-06-19 | 林庆浩 | Large-body type toy helicopter |
| CN103803070A (en) * | 2014-01-24 | 2014-05-21 | 兰州神龙航空科技有限公司 | Engineering rotor-type unmanned aircraft |
| US9456185B2 (en) * | 2009-08-26 | 2016-09-27 | Geotech Environmental Equipment, Inc. | Helicopter |
-
2017
- 2017-09-22 CN CN201710868195.5A patent/CN107878769A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2920344Y (en) * | 2005-12-06 | 2007-07-11 | 杜大森 | Remote controled helicopter fuselage cradle structure |
| US9456185B2 (en) * | 2009-08-26 | 2016-09-27 | Geotech Environmental Equipment, Inc. | Helicopter |
| CN203001967U (en) * | 2012-12-06 | 2013-06-19 | 林庆浩 | Large-body type toy helicopter |
| CN103803070A (en) * | 2014-01-24 | 2014-05-21 | 兰州神龙航空科技有限公司 | Engineering rotor-type unmanned aircraft |
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Legal Events
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|---|---|---|---|
| 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 |
Application publication date: 20180406 |
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| RJ01 | Rejection of invention patent application after publication |