CN110155310A - A kind of minute vehicle multifunctional compact control device - Google Patents
A kind of minute vehicle multifunctional compact control device Download PDFInfo
- Publication number
- CN110155310A CN110155310A CN201811338122.6A CN201811338122A CN110155310A CN 110155310 A CN110155310 A CN 110155310A CN 201811338122 A CN201811338122 A CN 201811338122A CN 110155310 A CN110155310 A CN 110155310A
- Authority
- CN
- China
- Prior art keywords
- control device
- circuit board
- shell
- minute vehicle
- piece
- 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.)
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C19/00—Aircraft control not otherwise provided for
- B64C19/02—Conjoint controls
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Cooling Or The Like Of Electrical Apparatus (AREA)
Abstract
The present invention provides a kind of minute vehicle multifunctional compact control devices, including preceding connection ring, back clevis, shell, preceding connection ring, back clevis are mounted on shell both ends, it include muti-piece circuit board in shell, every piece of circuit board integrates different function, adjacent circuit plate is connected by Coupled Rigid-flexible plate, and muti-piece circuit board is fixed by fixed block.The functions such as flight management, navigator fix, infrared seeker on minute vehicle are distributed on multiple circuit boards by the present invention, form a kind of compact cylindricality control device, its largest enveloping size can do corresponding change according to Flight Vehicle Structure size, especially suitable for micro air vehicle, the solution of minute vehicle control device is effectively given.
Description
Technical field
The present invention relates to flying vehicles control fields, and in particular to a kind of minute vehicle multifunctional compact control device.
Background technique
With the fast development of military science and technology, the direction of following war towards cluster attack and precision strike is developed, small
Type, high-performance, low cost aircraft increasingly by the concern of scientific research personnel.In general, minute vehicle control dress
The functions such as the flight management for being integrated with aircraft, navigator fix, aerofoil control, infrared seeker, power management are set, are aircraft
Core component.The characteristics of minute vehicle is small in size, conventional aircraft control device topology layout small using space
It can not be applied on minute vehicle, it is extremely urgent to develop a kind of minute vehicle multifunctional compact control device.
Summary of the invention
Aiming at the problem that existing flying vehicles control device is dfficult to apply to minute vehicle, the present invention proposes a kind of miniature winged
Row device multifunctional compact control device, the control device contain minute vehicle flight control, navigator fix, infrared lead
Draw, each function such as aerofoil control, and each function is distributed on multiple concatenated circuit boards, realizes that minute vehicle is effectively controlled
System.
A kind of minute vehicle multifunctional compact control device provided by the invention, including preceding connection ring, back clevis,
Shell, preceding connection ring, back clevis are mounted on shell both ends, include muti-piece circuit board in the shell, and every piece of circuit board is integrated
Different function；It is connected between adjacent circuit plate with Coupled Rigid-flexible plate, at least one electricity is mounted on two pieces of circuit boards of outermost
Connector；And 2 pieces of fixed blocks are at least set between adjacent circuit plate, in shell after the assembling of each component by fixed block and shell into
Row is fixedly connected.
Further, the muti-piece circuit board is arranged in any angle.
Further, the muti-piece circuit board is fixed by studs and stop nut.
Further, one piece of cooling fin is at least installed on each circuit board.
Further, the cylindrical structure of control device overall structure.
Further, the control device overall structure is cylindrical structure.
The present invention provides a kind of minute vehicle multifunctional compact control device, by flight management on aircraft, lead
The functions such as boat positioning, infrared seeker are distributed on each circuit board, and circuit board is in align at random angles, are connected by Coupled Rigid-flexible plate
Adjacent circuit board is connect, muti-piece circuit board is fixed by fixed block, a kind of compact cylindricality control device is formed, realizes miniature
Aircraft effectively controls.
Apparatus of the present invention shape is in the form of a column, compact-sized, and function is complete, and largest enveloping size can be according to flight
Device structure size does corresponding change, especially suitable for micro air vehicle, effectively gives minute vehicle control device
Solution.
Detailed description of the invention
Included attached drawing is used to provide to be further understood from the embodiment of the present invention, and which constitute one of specification
Point, for illustrating the embodiment of the present invention, and come together to illustrate the principle of the present invention with verbal description.It should be evident that below
Attached drawing in description is only some embodiments of the present invention, for those of ordinary skill in the art, is not paying creation
Property labour under the premise of, be also possible to obtain other drawings based on these drawings.
Fig. 1 is minute vehicle multifunctional compact control device construction profile in the embodiment of the present invention；
Fig. 2 is minute vehicle multifunctional compact control device Structure explosion diagram in the embodiment of the present invention；
Fig. 3 is minute vehicle multifunctional compact control device exemplary internal configuration figure in the embodiment of the present invention；
Fig. 4 is the arrangement schematic diagram of circuit board in another embodiment of the present invention.
The component that each label represents in attached drawing is as follows:
1 is preceding connection ring, 2 be back clevis, 3 be shell, 4 be circuit board, 5 be Coupled Rigid-flexible plate, 7 be preceding electrical connection
Device, 8 be rear electric connector, 9 be fixed block, 10 be studs, 11 be stop nut, 12 be cooling fin.
Specific embodiment
Specific embodiments of the present invention are described in detail below in conjunction with attached drawing.In the following description, for solution
Purpose and not restrictive is released, elaborates detail, to help to be apparent from the present invention.However, to those skilled in the art
It is readily apparent that the present invention can also be practiced in the other embodiments departing from these details for member.
The present invention provides a kind of minute vehicle multifunctional compact control device, the cylindrical structure of overall structure, such as Fig. 1
It is shown comprising preceding connection ring 1, back clevis 2, shell 3, preceding connection ring 1, back clevis 2 are fixedly mounted on 3 front and back two of shell
End is installed for front and back equipment.
As shown in Fig. 2, include in the shell 3 circuit board 4, Coupled Rigid-flexible plate 5, preceding electric connector 7, rear electric connector 8,
Fixed block 9, studs 10, stop nut 11, cooling fin 12.Wherein, circuit board 4 and Coupled Rigid-flexible plate 5, which use, is integrally machined
For ease of illustration description is dismantled in molding.
Muti-piece circuit board 4 is in shell 3 with certain spacing parallel arrangement, by flight management, navigator fix, infrared seeker,
The functions such as aerofoil control are integrated in various boards respectively.With the connection of Coupled Rigid-flexible plate 5, adjacent electricity between adjacent circuit plate 4
Information exchange between the plate of road is realized by Coupled Rigid-flexible plate 5.
It is mounted at least one electric connector on two pieces of circuit boards of outermost, as shown in Figure 2,3, front end, back-end circuit
Preceding electric connector 7, rear electric connector 8 are installed respectively, preceding electric connector 7, rear electric connector 8 is respectively used to and headend equipment on plate
Communication between rear end equipment.
Muti-piece circuit board 4 is connected by fixed block 9, studs 10, stop nut 11, between adjacent circuit plate 4 at least
2 pieces of fixed blocks 9 are set, more studs 10 pass through the preformed hole on muti-piece circuit board 4, and both ends are fixed with stop nut 11,
Guarantee that muti-piece circuit board 4 stablizes installation.
It is fixedly connected by fixed block 9 with shell 3 after each component assembling in shell 3.
It is also equipped with cooling fin 12 on the circuit board 4, is used for heat dissipation for circuit board.It is at least installed on general each circuit board
One piece of cooling fin.
The fixed installation occurred in the present invention can be fixed using screw, nut combination, convenient for assembling, maintenance.
Control device is at column construction in the present invention, can be it is cylindrical, prismatic, for the ease of installation, the present embodiment
Selection is cylindrical, while circuit board 4 is also configured as circle, and 4 diameter of circuit board is determined by aircraft internal diameter.
In other embodiments, muti-piece circuit board can arrange in any angle.As shown in figure 4, having one between circuit board
Clamp angle is easily installed other equipment, i.e. circuit board can carry out position adjusting, realizes spatial flexible layout.The shape of fixed block
Shape matches between shape and circuit board.
The many features and advantage of embodiment are clear according to the detailed description, therefore appended claims are intended to cover
The all these feature and advantage of these embodiments fallen into its true spirit and range.Further, since the technology of this field
Personnel are readily apparent that many modifications and changes, therefore are not meant to for the embodiment of the present invention to be limited to illustrated and description accurate knot
Structure and operation, but all suitable modifications and the equivalent fallen within the scope of its can be covered.
Unspecified part of the present invention is known to the skilled person technology.
Claims (6)
1. a kind of minute vehicle multifunctional compact control device, which is characterized in that including preceding connection ring, back clevis, shell
Body, the preceding connection ring, back clevis are mounted on the shell both ends, include muti-piece circuit board, every piece of circuit in the shell
Plate integrates different function；
With the connection of Coupled Rigid-flexible plate between adjacent circuit plate, circuit board and Coupled Rigid-flexible plate are integrally machined molding, and two pieces of outermost
At least one electric connector is mounted on circuit board；
2 pieces of fixed blocks are at least set between the adjacent circuit plate, in shell after each component assembling by fixed block and shell into
Row is fixedly connected.
2. minute vehicle multifunctional compact control device as described in claim 1, which is characterized in that the muti-piece circuit
Plate is arranged in any angle.
3. minute vehicle multifunctional compact control device as described in claim 1, which is characterized in that the muti-piece circuit
Plate also passes through studs and stop nut is fixed.
4. minute vehicle multifunctional compact control device as described in claim 1, which is characterized in that each circuit
One piece of cooling fin is at least installed on plate.
5. minute vehicle multifunctional compact control device as described in claim 1, which is characterized in that the control device
The cylindrical structure of overall structure.
6. minute vehicle multifunctional compact control device as claimed in claim 5, which is characterized in that the control device
Overall structure is cylindrical structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811338122.6A CN110155310A (en) | 2019-01-24 | 2019-01-24 | A kind of minute vehicle multifunctional compact control device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811338122.6A CN110155310A (en) | 2019-01-24 | 2019-01-24 | A kind of minute vehicle multifunctional compact control device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110155310A true CN110155310A (en) | 2019-08-23 |
Family
ID=67645224
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811338122.6A Pending CN110155310A (en) | 2019-01-24 | 2019-01-24 | A kind of minute vehicle multifunctional compact control device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110155310A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN205028162U (en) * | 2015-09-22 | 2016-02-10 | 北京行易道科技有限公司 | Unmanned aerial vehicle initiative safety device |
| CN105739515A (en) * | 2016-05-06 | 2016-07-06 | 陈龙 | Novel unmanned aerial vehicle flight controller module |
| CN205384513U (en) * | 2016-01-11 | 2016-07-13 | 致导科技（北京）有限公司 | Flight controller |
| US20170094792A1 (en) * | 2015-09-28 | 2017-03-30 | TBS Avionics Co. Ltd. | Electronic Component |
| CN107539454A (en) * | 2016-06-29 | 2018-01-05 | 北京臻迪机器人有限公司 | A kind of unmanned plane frame main frame |
-
2019
- 2019-01-24 CN CN201811338122.6A patent/CN110155310A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN205028162U (en) * | 2015-09-22 | 2016-02-10 | 北京行易道科技有限公司 | Unmanned aerial vehicle initiative safety device |
| US20170094792A1 (en) * | 2015-09-28 | 2017-03-30 | TBS Avionics Co. Ltd. | Electronic Component |
| CN205384513U (en) * | 2016-01-11 | 2016-07-13 | 致导科技（北京）有限公司 | Flight controller |
| CN105739515A (en) * | 2016-05-06 | 2016-07-06 | 陈龙 | Novel unmanned aerial vehicle flight controller module |
| CN107539454A (en) * | 2016-06-29 | 2018-01-05 | 北京臻迪机器人有限公司 | A kind of unmanned plane frame main frame |
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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 | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20190823 |
|
| WD01 | Invention patent application deemed withdrawn after publication |