CN208165242U - A kind of all-metal welded type unmanned aerial vehicle rack structure - Google Patents
A kind of all-metal welded type unmanned aerial vehicle rack structure Download PDFInfo
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- CN208165242U CN208165242U CN201820421772.6U CN201820421772U CN208165242U CN 208165242 U CN208165242 U CN 208165242U CN 201820421772 U CN201820421772 U CN 201820421772U CN 208165242 U CN208165242 U CN 208165242U
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- host arm
- reinforcing beam
- stringer
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Abstract
The utility model relates to air vehicle technique fields, and disclose a kind of all-metal welded type unmanned aerial vehicle rack structure, including the first host arm, stringer is fixedly installed on the right side of the first host arm, the second host arm is fixedly installed on the right side of the stringer, the bottom of the first host arm and the second host arm is fixedly installed with the first reinforcing beam, the bottom of the stringer is fixedly installed with the second reinforcing beam, the surface of first reinforcing beam is socketed with mounting plate, and the front of the mounting plate is plugged with installation bolt.The all-metal welded type unmanned aerial vehicle rack structure, by the way that stringer is arranged, stringer is welded between the first host arm and the second host arm, increase the intensity of the first host arm and the second host arm, by welding the first reinforcing beam in the first host arm and the second host arm bottom, the second reinforcing beam is welded in stringer bottom, the intensity of the first host arm and the second host arm can be made higher, and improve the strength and stability of unmanned aerial vehicle rack entirety.
Description
Technical field
The utility model relates to air vehicle technique field, specially a kind of all-metal welded type unmanned aerial vehicle rack structure.
Background technique
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft, or fully or intermittently automatically operated by car-mounted computer, compared with manned aircraft, nobody
Machine is often more suitable for executing the biggish task of risk, and unmanned plane presses application field, can be divided into it is military with civilian, military aspect,
Unmanned plane is divided into reconnaissance plane and target drone, civilian aspect, unmanned plane and industrial application, is that unmanned plane has really just needed, is navigating at present
Bat, agricultural, plant protection, miniature self-timer, express transportation, disaster relief, observation wild animal, monitoring infectious disease, mapping, Xin Wen Bao
The application in the fields such as road, electric inspection process, the disaster relief, movies-making and manufacture romance, has greatly expanded the purposes of unmanned plane itself,
Developed country also in actively extension industrial application and develops unmanned plane.
Unmanned plane assembles in splicing process, needs to use unmanned aerial vehicle rack structure, the stability of unmanned aerial vehicle rack structure is straight
Connect the stability for influencing entire unmanned plane, that there are stability is poor for traditional unmanned aerial vehicle rack structure, intensity is low and weight compared with
The defects of weight, heavier-weight can reduce the flight performance of unmanned plane, and the mounting portion fixation of unmanned aerial vehicle rack structure is unadjustable,
Be inconvenient to be installed on debugging, so propose that a kind of technical solution is set forth above to solve the problems, such as.
Utility model content
(1) the technical issues of solving
In view of the deficiencies of the prior art, the utility model provides a kind of all-metal welded type unmanned aerial vehicle rack structure, tool
Standby stability is high, intensity is high, it is light-weight can be improved unmanned plane during flying ability and mounting portion is adjustable, it is excellent to be easily installed debugging etc.
Point, solves that traditional unmanned aerial vehicle rack structural stability is low, intensity is low, heavier-weight reduces unmanned plane during flying ability and installation
The problem of portion is unadjustable, is not easy to installation and debugging.
(2) technical solution
For realize aforementioned stable is high, intensity is high, it is light-weight can be improved unmanned plane during flying ability and mounting portion is adjustable,
It is easily installed the purpose of debugging, the utility model provides the following technical solutions：A kind of all-metal welded type unmanned aerial vehicle rack structure,
Including the first host arm, it is fixedly installed with stringer on the right side of the first host arm, is fixedly installed on the right side of the stringer
The bottom of two host arms, the first host arm and the second host arm is fixedly installed with the first reinforcing beam, the bottom of the stringer
It is fixedly installed with the second reinforcing beam, the surface of first reinforcing beam is socketed with mounting plate, and the front of the mounting plate is plugged with
Bolt is installed, the left and right sides of the mounting plate offers adjustment hole, and the left and right sides of first reinforcing beam is plugged with
Bolt, the left side of first reinforcing beam and the top fixed installation support plate for being located at adjusting bolt are adjusted, the support plate
Top is fixedly installed with supporting block, and cross bar is movably installed on the right side of the supporting block, is fixedly installed on the right side of the cross bar
Arresting lever, the top of the support plate and be fixedly installed between supporting block and arresting lever one end run through cross bar vertical bar,
The surface of the vertical bar is socketed with the spring that both ends are fixedly connected with the bottom at the top of support plate and cross bar respectively.
Preferably, the quantity of the stringer, the first reinforcing beam and the second reinforcing beam is two, the first host arm and
Second host arm is symmetrical as line of symmetry using the vertical centerline of stringer.
Preferably, first reinforcing beam and the second reinforcing beam are U-shaped, the both ends of the stringer respectively with the first host
The right side of arm and the welding of the left side of the second host arm.
Preferably, the top of first reinforcing beam is welded with the bottom of the first host arm and the second host arm respectively, institute
It is welded respectively with the bottom of two stringers at the top for stating the second reinforcing beam.
Preferably, the quantity of the installation bolt is four, and installs the positive quadrangle that bolt is distributed in the plate of installation, institute
The quantity for stating adjustment hole is no less than 20, and adjustment hole is distributed in the left and right sides of mounting plate in a ring, the mounting plate
Front offers locking groove.
Preferably, the spring is in tensional state, and the width of the locking groove is adapted with the width of arresting lever.
(3) beneficial effect
Compared with prior art, the utility model provides a kind of all-metal welded type unmanned aerial vehicle rack structure, have with
Lower beneficial effect：The all-metal welded type unmanned aerial vehicle rack structure, by the way that stringer is arranged, in the first host arm and the second host arm
Between weld stringer, the intensity of the first host arm and the second host arm is increased, by the first host arm and the second host arm
The first reinforcing beam is welded in bottom, welds the second reinforcing beam in stringer bottom, can make the strong of the first host arm and the second host arm
Du Genggao, and the strength and stability of unmanned aerial vehicle rack entirety is improved, the first host arm, the second host arm, stringer, first add
Brutal and the second reinforcing beam are all made of high-strength aluminum alloy, greatly reduce the weight of unmanned aerial vehicle rack, improve unmanned plane
Flying quality, by be arranged mounting plate, unmanned aerial vehicle rack installation when, can according to installation engaging member come adjust installation
Unmanned aerial vehicle rack is fixed on installation engaging member by plate to suitable angle, by installation bolt, is adjusted bolt and is inserted into adjustment hole,
The effect of fixed mounting plate can be played, for arresting lever in the case where spring is because replying the pulling force that deformation generates, moving down makes arresting lever
It is caught in locking groove, further fixes mounting plate, keep entire unmanned aerial vehicle rack more firm, because of mounting plate adjustable angle, make nobody
The installation and debugging of machine rack are more convenient, and applicability is also wider.
Detailed description of the invention
Fig. 1 is the utility model schematic perspective view；
Fig. 2 is the utility model mounting plate positive structure schematic；
Fig. 3 is the utility model mounting plate side structure schematic diagram.
In figure：1 first host arm, 2 stringers, 3 second host arms, 4 first reinforcing beams, 5 second reinforcing beams, 6 mounting plates, 7
Bolt, 8 adjustment holes, 9 adjusting bolts, 10 support plates, 11 supporting blocks, 12 cross bars, 13 arresting levers, 14 vertical bars, 15 springs, 16 are installed
Locking groove.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
Please refer to Fig. 1-3, a kind of all-metal welded type unmanned aerial vehicle rack structure, including the first host arm 1, the first host arm
1 right side is fixedly installed with stringer 2, and the right side of stringer 2 is fixedly installed with the second host arm 3, the first host arm 1 and the second host
The bottom of arm 3 is fixedly installed with the first reinforcing beam 4, and the bottom of stringer 2 is fixedly installed with the second reinforcing beam 5, the first reinforcing beam 4
Surface is socketed with mounting plate 6, and the front of mounting plate 6 is plugged with installation bolt 7, and the left and right sides of mounting plate 6 offers adjusting
Hole 8, the left and right sides of the first reinforcing beam 4, which is plugged with, adjusts bolt 9, the left side of the first reinforcing beam 4 and is located at and adjusts bolt 9
Support plate 10 is fixedly mounted in top, and the top of support plate 10 is fixedly installed with supporting block 11, the right side activity installation of supporting block 11
There is a cross bar 12, the right side of cross bar 12 is fixedly installed with arresting lever 13, the top of support plate 10 and is located at supporting block 11 and arresting lever
Be fixedly installed between 13 one end run through cross bar 12 vertical bar 14, the surface of vertical bar 14 be socketed with both ends respectively with support plate 10
The quantity of the spring 15 that top is fixedly connected with the bottom of cross bar 12, stringer 2, the first reinforcing beam 4 and the second reinforcing beam 5 is two
A, the first host arm 1 and the second host arm 3 are symmetrical as line of symmetry using the vertical centerline of stringer 2, the first reinforcing beam 4 with
Second reinforcing beam 5 is U-shaped, and the both ends of stringer 2 are welded with the right side of the first host arm 1 and the left side of the second host arm 3 respectively,
The top of first reinforcing beam 4 is welded with the bottom of the first host arm 1 and the second host arm 3 respectively, the top part of the second reinforcing beam 5
It is not welded with the bottom of two stringers 2, the quantity of installation bolt 7 is four, and installs bolt 7 and be distributed in the plate 6 of installation just
Face quadrangle, the quantity of adjustment hole 8 is no less than 20, and adjustment hole 8 is distributed in the left and right sides of mounting plate 6 in a ring, installation
The front of plate 6 offers locking groove 16, and spring 15 is in tensional state, and the width of locking groove 16 is mutually fitted with the width of arresting lever 13
Match, by the way that stringer 2 is arranged, stringer 2 is welded between the first host arm 1 and the second host arm 3, increases 1 He of the first host arm
The intensity of second host arm 3, by welding the first reinforcing beam 4 in the first host arm 1 and 3 bottom of the second host arm, at 2 bottom of stringer
The second reinforcing beam 5 is welded in portion, the intensity of the first host arm 1 and the second host arm 3 can be made higher, and improve unmanned aerial vehicle rack
Whole strength and stability, the first host arm 1, the second host arm 3, stringer 2, the first reinforcing beam 4 and the second reinforcing beam 5 are adopted
With high-strength aluminum alloy, the weight of unmanned aerial vehicle rack is greatly reduced, improves the flying quality of unmanned plane, is pacified by setting
Loading board 6 can adjust mounting plate 6 to suitable angle according to installation engaging member, pass through when unmanned aerial vehicle rack installation
Unmanned aerial vehicle rack is fixed on installation engaging member by installation bolt 7, is adjusted bolt 9 and is inserted into adjustment hole 8, can play fixed installation
The effect of plate 6, for arresting lever 13 in the case where spring 15 is because replying the pulling force that deformation generates, moving down makes arresting lever 13 be caught in locking groove
In 16, mounting plate 6 is further fixed, keeps entire unmanned aerial vehicle rack more firm, because of 6 adjustable angle of mounting plate, makes unmanned aerial vehicle rack
Installation and debugging it is more convenient, applicability is also wider.
In conclusion the all-metal welded type unmanned aerial vehicle rack structure, by the way that stringer 2 is arranged, in the first host arm 1 and the
Stringer 2 is welded between two host arms 3, the intensity of the first host arm 1 and the second host arm 3 is increased, by the first host arm 1
The first reinforcing beam 4 is welded with 3 bottom of the second host arm, the second reinforcing beam 5 is welded in 2 bottom of stringer, the first host arm 1 can be made
It is higher with the intensity of the second host arm 3, and the strength and stability of unmanned aerial vehicle rack entirety is improved, the first host arm 1, second
Host arm 3, stringer 2, the first reinforcing beam 4 and the second reinforcing beam 5 are all made of high-strength aluminum alloy, greatly reduce unmanned plane machine
The weight of frame improves the flying quality of unmanned plane, by the way that mounting plate 6 is arranged, when unmanned aerial vehicle rack installation, and Ke Yigen
Mounting plate 6 is adjusted according to installation engaging member to suitable angle, and unmanned aerial vehicle rack is fixed on by installation by installation bolt 7 and is combined
It on part, adjusts bolt 9 and is inserted into adjustment hole 8, the effect of fixed mounting plate 6 can be played, arresting lever 13 is in spring 15 because replying shape
Sell of one's property under raw pulling force, moving down is caught in arresting lever 13 in locking groove 16, further fixes mounting plate 6, make it is entire nobody
Machine rack is more firm, because of 6 adjustable angle of mounting plate, keeps the installation of unmanned aerial vehicle rack and debugging more convenient, applicability is also wider, solution
Having determined, traditional unmanned aerial vehicle rack structural stability is low, intensity is low, heavier-weight reduces unmanned plane during flying ability and mounting portion not
The problem of being adjusted, being not easy to installation and debugging.
It should be noted that, in this document, relational terms such as first and second and the like are used merely to a reality
Body or operation are distinguished with another entity or operation, are deposited without necessarily requiring or implying between these entities or operation
In any actual relationship or order or sequence.Moreover, the terms "include", "comprise" or its any other variant are intended to
Non-exclusive inclusion, so that the process, method, article or equipment including a series of elements is not only wanted including those
Element, but also including other elements that are not explicitly listed, or further include for this process, method, article or equipment
Intrinsic element.In the absence of more restrictions, the element limited by sentence "including a ...", it is not excluded that
There is also other identical elements in process, method, article or equipment including the element.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired
Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.
Claims (6)
1. a kind of all-metal welded type unmanned aerial vehicle rack structure, including the first host arm (1), it is characterised in that：Described first is main
It is fixedly installed on the right side of horn (1) stringer (2), the second host arm (3) is fixedly installed on the right side of the stringer (2), it is described
The bottom of first host arm (1) and the second host arm (3) is fixedly installed with the first reinforcing beam (4), and the bottom of the stringer (2) is solid
Dingan County is equipped with the second reinforcing beam (5), and the surface of first reinforcing beam (4) is socketed with mounting plate (6), the mounting plate (6)
Front is plugged with installation bolt (7), and the left and right sides of the mounting plate (6) offers adjustment hole (8), first reinforcing beam
(4) the left and right sides be plugged with adjust bolt (9), the left side of first reinforcing beam (4) and be located at adjust bolt (9) it is upper
Support plate (10) are fixedly mounted in side, are fixedly installed with supporting block (11) at the top of the support plate (10), the supporting block (11)
Right side be movably installed with cross bar (12), be fixedly installed with arresting lever (13), the support plate on the right side of the cross bar (12)
(10) top and the vertical bar that cross bar (12) are run through in one end is fixedly installed between supporting block (11) and arresting lever (13)
(14), the surface of the vertical bar (14) is socketed with both ends and fixes respectively with the top of support plate (10) and the bottom of cross bar (12) and connects
The spring (15) connect.
2. a kind of all-metal welded type unmanned aerial vehicle rack structure according to claim 1, it is characterised in that：The stringer
(2), the quantity of the first reinforcing beam (4) and the second reinforcing beam (5) is two, the first host arm (1) and the second host arm
(3) symmetrical as line of symmetry using the vertical centerline of stringer (2).
3. a kind of all-metal welded type unmanned aerial vehicle rack structure according to claim 1, it is characterised in that：Described first adds
Brutal (4) and the second reinforcing beam (5) are U-shaped, the both ends of the stringer (2) respectively with the right side of the first host arm (1) and
It welds in the left side of two host arms (3).
4. a kind of all-metal welded type unmanned aerial vehicle rack structure according to claim 1, it is characterised in that：Described first adds
The top of brutal (4) is welded with the bottom of the first host arm (1) and the second host arm (3) respectively, second reinforcing beam (5)
It is welded respectively with the bottom of two stringers (2) at top.
5. a kind of all-metal welded type unmanned aerial vehicle rack structure according to claim 1, it is characterised in that：The installation spiral shell
The quantity of bolt (7) is four, and installs the positive quadrangle that bolt (7) are distributed in the plate (6) of installation, the number of the adjustment hole (8)
Amount no less than 20, and adjustment hole (8) is distributed in the left and right sides of mounting plate (6), the front of the mounting plate (6) in a ring
Offer locking groove (16).
6. a kind of all-metal welded type unmanned aerial vehicle rack structure according to claim 1, it is characterised in that：The spring
(15) it is in tensional state, the width of the locking groove (16) is adapted with the width of arresting lever (13).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820421772.6U CN208165242U (en) | 2018-03-27 | 2018-03-27 | A kind of all-metal welded type unmanned aerial vehicle rack structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820421772.6U CN208165242U (en) | 2018-03-27 | 2018-03-27 | A kind of all-metal welded type unmanned aerial vehicle rack structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208165242U true CN208165242U (en) | 2018-11-30 |
Family
ID=64376000
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820421772.6U Active CN208165242U (en) | 2018-03-27 | 2018-03-27 | A kind of all-metal welded type unmanned aerial vehicle rack structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208165242U (en) |
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2018
- 2018-03-27 CN CN201820421772.6U patent/CN208165242U/en active Active
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