CN209223869U - A kind of wing support construction - Google Patents

A kind of wing support construction Download PDF

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Publication number
CN209223869U
CN209223869U CN201821254272.4U CN201821254272U CN209223869U CN 209223869 U CN209223869 U CN 209223869U CN 201821254272 U CN201821254272 U CN 201821254272U CN 209223869 U CN209223869 U CN 209223869U
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Prior art keywords
arm
rod
bar
support construction
sliding block
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Active
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CN201821254272.4U
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Chinese (zh)
Inventor
赖宇彬
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Chengdu Tiger Aerospace Technology Co Ltd
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Chengdu Tigers Aerospace Technology Co Ltd
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Priority to CN201821254272.4U priority Critical patent/CN209223869U/en
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Abstract

The utility model provides a kind of wing support construction, belong to secondary process field of tool, including pedestal, cursor, the first adjusting component and second adjust component, cursor includes the first arm and the second arm, first arm is connect with base rotation, and the second arm is connect with the first arm far from one end of pedestal;First adjusting component includes screw rod, nut and adjustment sheet, and screw rod is fixedly connected with one end of nearly first arm of the second arm rest, and adjustment sheet is connected in screw rod, and nut is bolted in screw rod, and the second arm is stretched out in one end of adjustment sheet;Second adjusting component includes control-rod, bolt, sliding block, connection strap and clamping sheet, and clamping sheet is slidably connected with the second arm, and clamping sheet is arranged towards the inside of the second arm.The first adjusting component and second that wing support construction provided by the utility model can manually adjust adjusts component, by slidable adjustment piece and clamping sheet, clamping can be carried out to various sizes of wing, to reduce the manufacturing cost improved because making fixture.

Description

A kind of wing support construction
Technical field
The utility model relates to secondary process field of tool, in particular to a kind of wing support construction.
Background technique
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, is using radio robot and to provide for oneself The not manned aircraft of presetting apparatus manipulation, or fully or intermittently automatically operated by car-mounted computer.Exist at present It takes photo by plane, agricultural, plant protection, miniature self-timer, express transportation, disaster relief, observation wild animal, monitoring infectious disease, mapping, Xin Wen Bao The application in road, electric inspection process, the disaster relief, movies-making, manufacture romance etc. field, has greatly expanded the use of unmanned plane itself On the way, developed country also in actively extension industrial application and develops unmanned air vehicle technique.Since the wing of unmanned plane is more special, usually It needs to design special fixture to carry out clamping, is processed with facilitating.
Inventor has found that existing fixture at least has the disadvantage in that existing unmanned plane clamp structure list under study for action One, various sizes of wing needs to carry out clamping, the manufacturing cost greatly improved using different fixtures.
Utility model content
The purpose of this utility model is to provide a kind of wing support constructions, to improve existing unmanned plane clamp structure list One, the problem of various sizes of wing needs to carry out clamping using different fixture, the manufacturing cost greatly improved.
The utility model is realized in this way:
Based on above-mentioned purpose, the utility model provides a kind of wing support construction, including pedestal, cursor, first It adjusts component and second and adjusts component, the cursor includes the first arm and the second arm, first arm and the base rotation Connection, second arm is arc-shaped, and second arm is connect with first arm far from one end of the pedestal;Described first adjusts Save component include screw rod, nut and adjustment sheet, sliding slot is provided on the adjustment sheet, the sliding slot is linear, the screw rod with One end of nearly first arm of second arm rest is fixedly connected, and the adjustment sheet is connected in the screw rod by the sliding slot, The nut is bolted in the screw rod, and second arm is stretched out in one end of the adjustment sheet, and the adjustment sheet is towards described the The inside of two arms is arranged;The second adjusting component includes control-rod, bolt, sliding block, connection strap and clamping sheet, the bolt spiral shell It is connected to the control-rod, the sliding block is slidably connected with the control-rod, direction of axis line of the sliding block along the control-rod It is slided relative to the control-rod, and the sliding block is between the bolt and second arm, one end of the connection strap It is rotatablely connected with the sliding block, the other end of the connection strap is slidably connected with the clamping sheet, and the connection strap is relative to institute The axis parallel that the axial line and the connection strap for stating sliding block rotation are rotated relative to the clamping sheet, and the connection strap phase Vertical with the axial line of the control-rod for the axial line of sliding block rotation, the clamping sheet and second arm sliding connect It connects, and the clamping sheet is arranged towards the inside of second arm.
The first adjusting component and second that wing support construction provided by the utility model can manually adjust adjusts component, By slidable adjustment piece and clamping sheet, clamping can be carried out to various sizes of wing, be improved to reduce because making fixture Manufacturing cost.
In an embodiment of the present embodiment: the adjusting component further includes elastic component, and the elastic component is installed on Between second arm and the sliding block, the elastic component enables the sliding block have the direction sliding for being directed away from second arm Trend.
Elastic component can allow sliding block to abut together with bolt always, so that convenient control the position of clamping sheet.
In an embodiment of the present embodiment: the elastic component is the spring in compressive state, the elastic component set Set on the control-rod.
Spring is set on control-rod, the stationarity of elastic component can be increased, meanwhile, spring is also cheap and easy In the thing of acquisition, cost can be reduced.
In an embodiment of the present embodiment: the clamping sheet include first and second, the connection strap and First rotation connection, described first is vertically arranged with described second, and described second is located at described first far One end from the connection strap, and the axis parallel of described second and the control-rod is arranged.
When making second, it can allow second there is slight radian, and second arcuate directions and the second arm Arcuate directions it is identical, in this way can it is more convenient to wing carry out clamping, meanwhile, second arc-shaped energy preferably with Wing fitting, increases second and the contact area of wing, avoids causing to damage to wing.
In an embodiment of the present embodiment: it is provided with the first and second card slots on second arm, described second Card slot is located at the one end of second arm far from first arm, and second card slot is located at the inside of second arm, institute It states the first card slot to be connected to second card slot, described first is connected in first card slot, and described second is located at institute It states in the second card slot.
Before carrying out clamping to wing, second is in being located at the second card slot, this can be to avoid clamping sheet in cursor Wing is scratched during rotation, after cursor is fixed, is adjusted to clamping sheet, can preferably be completed to machine The fixation of the wing.
In an embodiment of the present embodiment: the screw rod includes the first bar and the second bar, the cross of first bar Rectangular in cross-section, the circular in cross-section of second bar are provided with external screw thread on second bar, first bar with it is described Second arm is fixedly connected, and second bar is located at the one end of first bar far from second arm;It is provided on the nut Threaded hole, the internal screw thread with external screw thread cooperation is provided in the threaded hole, and the nut passes through the screw hole In second bar.
Cross section is connected in sliding slot in the second bar of rectangle, can be formed certain limitation to adjustment sheet, be avoided adjusting Piece rotation, so as to which wing is fixed well.
In an embodiment of the present embodiment: the length of first bar is less than the thickness of the adjustment sheet.
Nut can be allowed smoothly to contact with adjustment sheet in this way, thus by adjustment sheet to fixation.
In an embodiment of the present embodiment: the pedestal includes bottom plate and two transverse slats, two transverse slats point It is not installed on the bottom plate, two transverse slat interval settings, and two transverse slats are arranged in parallel, between two transverse slats Mounting groove is formed, is bolted between the transverse slat, first arm and the bolt are rotatablely connected, and first arm can To be caught in the mounting groove.
In an embodiment of the present embodiment: two bolts, two bolts point are installed on the transverse slat Not Wei Yu the transverse slat both ends, one end of first arm is provided with through-hole, and the other end setting of first arm is jagged, The notch is located at side of first arm far from second arm, and the through-hole is sheathed on the bolt, when described After first arm is caught in the mounting groove, another described bolt is located in the notch.
After turning to cursor on wing, the first arm has major part to be all located in mounting groove, is turning two bolts When, cursor can be fixed stronger.
In an embodiment of the present embodiment: the junction of the transverse slat and first arm is provided with an installation Hole, the other end of the transverse slat are provided with multiple mounting holes, and multiple mounting holes positioned at described transverse slat the same end are described in The short transverse interval of transverse slat is arranged, and the bolt is installed in the mounting hole.
When encountering various sizes of wing, by the way that bolt to be mounted in different mounting holes, wing can also be allowed Clamping enhanced convenience is secured, when carrying out clamping to biggish wing, bolt can be mounted in uppermost mounting hole, When carrying out clamping to lesser wing, bolt can be mounted in nethermost mounting hole.
Compared with prior art, beneficial effect of the utility model is:
The first adjusting component and second that wing support construction provided by the utility model can manually adjust adjusts component, By slidable adjustment piece and clamping sheet, clamping can be carried out to various sizes of wing, be improved to reduce because making fixture Manufacturing cost.
Detailed description of the invention
It, below will be right in order to illustrate more clearly of specific embodiment of the present invention or technical solution in the prior art Required practical attached drawing is briefly described in specific embodiment or description of the prior art, it should be apparent that, it is described below Attached drawing be that some embodiments of the utility model are not paying creative labor for those of ordinary skill in the art Under the premise of dynamic, it is also possible to obtain other drawings based on these drawings.
Fig. 1 shows the schematic diagram of the wing support construction of the offer of the utility model embodiment 1;
Fig. 2 shows the schematic diagrames for the cursor that the utility model embodiment 1 provides;
Fig. 3 shows the schematic diagram of the first adjusting component of the offer of the utility model embodiment 1;
Fig. 4 shows the schematic diagram of the screw rod of the offer of the utility model embodiment 1;
Fig. 5 shows the schematic diagram of the second adjusting component of the offer of the utility model embodiment 1;
Fig. 6 shows the schematic diagram of the clamping sheet of the offer of the utility model embodiment 1;
Fig. 7 shows schematic diagram of the pedestal at the first visual angle of the offer of the utility model embodiment 1;
Fig. 8 shows schematic diagram of the pedestal at the second visual angle of the offer of the utility model embodiment 1
In figure: 101- pedestal;102- cursor;103- first adjusts component;104- second adjusts component;105- first Arm;The second arm of 106-;107- through-hole;108- notch;109- adjustment sheet;110- screw rod;111- nut;112- sliding slot;113- One bar;The second bar of 114-;115- clamping sheet;116- control-rod;117- bolt;118- sliding block;119- connection strap;120- elasticity Part;121- first;122- second;123- transverse slat;124- bottom plate;125- mounting hole.
Specific embodiment
The utility model is further described in detail below through specific implementation examples and in conjunction with the accompanying drawings.
To keep the objectives, technical solutions, and advantages of the embodiments of the present invention clearer, above in conjunction with the utility model Attached drawing in embodiment clearly and completely describes the technical scheme in the embodiment of the utility model, it is clear that retouched The embodiment stated is the utility model a part of the embodiment, instead of all the embodiments.Usually here in attached drawing description and The component of the utility model embodiment shown can be arranged and be designed with a variety of different configurations.
Therefore, the above detailed description to the embodiments of the present invention provided in the accompanying drawings is not intended to limit requirement The scope of the utility model of protection, but it is merely representative of the selected embodiment of the utility model.Based in the utility model Embodiment, every other embodiment obtained by those of ordinary skill in the art without making creative efforts, all Belong to the range of the utility model protection.
It should also be noted that similar label and letter indicate similar terms in following attached drawing, therefore, once a certain Xiang Yi It is defined in a attached drawing, does not then need that it is further defined and explained in subsequent attached drawing.
In the description of the present invention, it should be understood that indicating position or the term of positional relationship are based on attached drawing Shown in orientation or positional relationship, be merely for convenience of describing the present invention and simplifying the description, rather than indication or suggestion institute The equipment or element of finger must have a particular orientation, is constructed and operated in a specific orientation, therefore should not be understood as to this reality With novel limitation.
In the present invention unless specifically defined or limited otherwise, term " installation ", " connected ", " connection ", " Gu It is fixed " etc. terms shall be understood in a broad sense, for example, it may be being fixedly connected, or integral;It can be mechanical connection, be also possible to electricity Connection;It can be directly connected, the connection inside two elements or two can also be can be indirectly connected through an intermediary The interaction relationship of element.For the ordinary skill in the art, above-mentioned term can be understood as the case may be Concrete meaning in the present invention.
In the present invention unless specifically defined or limited otherwise, fisrt feature is on or below second feature It may include that the first and second features directly contact, also may include that the first and second features are not direct contacts but pass through it Between other characterisation contact.Moreover, fisrt feature is on second feature, top and above include fisrt feature the Right above two features and oblique upper, or first feature horizontal height is merely representative of higher than second feature.Fisrt feature is in the second spy Under sign, lower section and fisrt feature included below be directly below and diagonally below the second feature, or be merely representative of fisrt feature level Height is less than second feature.
It should be noted that in the absence of conflict, the feature in the embodiments of the present invention and embodiment can To be combined with each other.
Embodiment 1
Referring to figs. 1 to Fig. 8, the utility model provides a kind of wing support construction, including pedestal 101, cursor 102, First adjusts component 103 and the second adjusting component 104, and cursor 102 includes the first arm 105 and the second arm 106, the first arm 105 It is rotatablely connected with pedestal 101, the second arm 106 is arc-shaped, and the second arm 106 is connect with the first arm 105 far from one end of pedestal 101; First, which adjusts component 103, includes screw rod 110, nut 111 and adjustment sheet 109, is provided with sliding slot 112, sliding slot on adjustment sheet 109 112 linearly, and screw rod 110 is fixedly connected with the second arm 106 close to one end of the first arm 105, and adjustment sheet 109 passes through sliding slot 112 It is connected in screw rod 110, nut 111 is bolted in screw rod 110, and the second arm 106, and 109 court of adjustment sheet are stretched out in one end of adjustment sheet 109 It is arranged to the inside of the second arm 106;Second, which adjusts component 104, includes control-rod 116, bolt 117, sliding block 118, connection strap 119 With clamping sheet 115, bolt 117 is bolted in control-rod 116, and sliding block 118 is slidably connected with control-rod 116, and sliding block 118 is along control-rod 116 direction of axis line is slided relative to control-rod 116, and sliding block 118 is located between bolt 117 and the second arm 106, connection strap 119 one end and sliding block 118 are rotatablely connected, and the other end and the clamping sheet 115 of connection strap 119 are slidably connected, and connection strap 119 is opposite In axial line and the axis parallel that is rotated relative to clamping sheet 115 of connection strap 119 that sliding block 118 rotates, and 119 phase of connection strap The axial line rotated for sliding block 118 is vertical with the axial line of control-rod 116, and clamping sheet 115 is slidably connected with the second arm 106, And clamping sheet 115 is arranged towards the inside of the second arm 106.
The the first adjusting component 103 and the second adjusting group that wing support construction provided by the utility model can manually adjust Part 104 can carry out clamping to various sizes of wing, to reduce because of system by slidable adjustment piece 109 and clamping sheet 115 The manufacturing cost making fixture and improving.
Adjusting component further includes elastic component 120, and elastic component 120 is installed between the second arm 106 and sliding block 118, elastic component 120 trend for enabling sliding block 118 that there is the direction for being directed away from the second arm 106 to slide.Elastic component 120 can allow sliding block 118 always It is abutted together with bolt 117, so that convenient control the position of clamping sheet 115.
Elastic component 120 is the spring in compressive state, and elastic component 120 is sheathed on control-rod 116.Spring is set in control On bar 116, the stationarity of elastic component 120 can be increased, meanwhile, spring is also thing that is cheap and being easily obtained, can be with Reduce cost.
Clamping sheet 115 includes first 121 and second 122, connection strap 119 and first 121 rotation connection, and first 121 are vertically arranged with second 122, and second 122 is located at first 121 one end far from connection strap 119, and second 122 It is arranged with the axis parallel of control-rod 116.When making second 122, can allow second 122 has slight radian, And second 122 arcuate directions are identical as the arcuate directions of the second arm 106, more convenient can fill in this way to wing Folder, meanwhile, arc-shaped second 122 can preferably be bonded with wing, increase the contact area of second 122 with wing, keep away Exempt from that wing is caused to damage.
The first and second card slots are provided on second arm 106, the second card slot is located at one of the second arm far from the first arm 105 End, and the second card slot is located at the inside of the second arm 106, the first card slot is connected to the second card slot, and first 121 is connected in the first card In slot, second 122 is located in the second card slot.Before carrying out clamping to wing, second 122 is in being located at card slot, this can Wing is scratched during cursor 102 rotates to avoid clamping sheet 115, after cursor 102 is fixed, to clamping Piece 115 is adjusted, and can preferably complete the fixation to wing.
Screw rod 110 includes the first bar 113 and the second bar 114, and the cross section of the first bar 113 is in rectangle, the cross of the second bar 114 Section is rounded, and external screw thread is provided on the second bar 114, and the first bar 113 is fixedly connected with the second arm 106, and the second bar 114 is located at The one end of first bar 113 far from the second arm 106;It is provided with threaded hole on nut 111, is provided in threaded hole and cooperates with external screw thread Internal screw thread, nut 111 by screw hole in the second bar 114.Cross section is connected to sliding slot in the second bar 114 of rectangle In 112, certain limitation can be formed to adjustment sheet 109, avoid adjustment sheet 109 rotate, so as to well to wing into Row is fixed.
The length of first bar 113 is less than the thickness of adjustment sheet 109.Can allow in this way nut 111 smoothly with adjustment sheet 109 Contact, thus by adjustment sheet 109 to fixation.
Pedestal 101 includes bottom plate 124 and two transverse slats 123, and two transverse slats 123 are respectively arranged in bottom plate 124, two transverse slats 123 interval settings, and two transverse slats 123 are arranged in parallel, and form mounting groove between two transverse slats 123, pass through spiral shell between transverse slat 123 Bolt 117 connects, and the first arm 105 is rotatablely connected with bolt 117, and the first arm 105 can be caught in mounting groove.
Two bolts 117 are installed, two bolts 117 are located at the both ends of transverse slat 123, the first arm 105 on transverse slat 123 One end is provided with through-hole 107, and the other end setting jagged 108 of the first arm 105, notch 108 is located at the first arm 105 far from second The side of arm 106, through-hole 107 are sheathed on a bolt 117, after the first arm 105 is caught in mounting groove, 117, another bolt In in notch 108.After turning to cursor 102 on wing, the first arm 105 has major part to be all located in mounting groove, is twisting When moving two bolts 117, cursor 102 can be fixed stronger.
The junction of transverse slat 123 and the first arm 105 is provided with a mounting hole 125, and the other end of transverse slat 123 is provided with more A mounting hole 125, multiple mounting holes 125 positioned at 123 the same end of transverse slat are arranged along the short transverse interval of transverse slat 123, bolt 117 are installed in mounting hole 125.When encountering various sizes of wing, by the way that bolt 117 to be mounted on to different mounting holes In 125, the clamping enhanced convenience of wing can also be allowed secured, it, can be by bolt 117 when carrying out clamping to biggish wing It is mounted in uppermost mounting hole 125, when carrying out clamping to lesser wing, bolt 117 can be mounted on bottom Mounting hole 125 in.
The above descriptions are merely preferred embodiments of the present invention, is not intended to limit the utility model, for this For the technical staff in field, various modifications and changes may be made to the present invention.It is all in the spirit and principles of the utility model Within, any modification, equivalent replacement, improvement and so on should be included within the scope of protection of this utility model.

Claims (10)

1. a kind of wing support construction, which is characterized in that component and second, which is adjusted, including pedestal, cursor, first adjusts component, The cursor includes the first arm and the second arm, and first arm is connect with the base rotation, and second arm is arc-shaped, institute It states the second arm and is connect with first arm far from one end of the pedestal;The first adjusting component includes screw rod, nut and tune Nodal plate is provided with sliding slot on the adjustment sheet, and the sliding slot is linear, the screw rod and nearly first arm of second arm rest One end be fixedly connected, the adjustment sheet is connected in the screw rod by the sliding slot, and the nut is bolted in the screw rod, institute Second arm is stretched out in the one end for stating adjustment sheet, and the adjustment sheet is arranged towards the inside of second arm;Described second adjusts Section component includes control-rod, bolt, sliding block, connection strap and clamping sheet, and the bolt is bolted in the control-rod, the sliding block with The control-rod is slidably connected, and the sliding block is slided along the direction of axis line of the control-rod relative to the control-rod, and institute Sliding block is stated between the bolt and second arm, one end of the connection strap and the sliding block are rotatablely connected, the company The other end of narrow bars is slidably connected with the clamping sheet, the axial line and the company that the connection strap is rotated relative to the sliding block The axis parallel that narrow bars are rotated relative to the clamping sheet, and the axial line that rotates relative to the sliding block of the connection strap with The axial line of the control-rod is vertical, and the clamping sheet is slidably connected with second arm, and the clamping sheet is towards described The inside of two arms is arranged.
2. wing support construction according to claim 1, which is characterized in that the adjusting component further includes elastic component, institute It states elastic component to be installed between second arm and the sliding block, the elastic component enables the sliding block have and is directed away from described the The trend of the direction sliding of two arms.
3. wing support construction according to claim 2, which is characterized in that the elastic component is the bullet in compressive state Spring, the elastic component are sheathed on the control-rod.
4. wing support construction according to claim 3, which is characterized in that the clamping sheet includes first and second Piece, the connection strap and described first rotation connection, described first is vertically arranged with described second, second position In described first one end far from the connection strap, and described second with the axis parallel setting of the control-rod.
5. wing support construction according to claim 4, which is characterized in that be provided with first and second on second arm Card slot, second card slot are located at the one end of second arm far from first arm, and second card slot is located at described the The inside of two arms, first card slot are connected to second card slot, and described first is connected in first card slot, described Second is located in second card slot.
6. wing support construction according to claim 1, which is characterized in that the screw rod includes the first bar and the second bar, The cross section of first bar is in rectangle, and the circular in cross-section of second bar is provided with external screw thread on second bar, institute It states the first bar to be fixedly connected with second arm, second bar is located at the one end of first bar far from second arm;Institute It states and is provided with threaded hole on nut, the internal screw thread with external screw thread cooperation is provided in the threaded hole, the nut passes through The screw hole is in second bar.
7. wing support construction according to claim 6, which is characterized in that the length of first bar is less than the adjusting The thickness of piece.
8. wing support construction according to claim 1, which is characterized in that the pedestal includes bottom plate and two transverse slats, Two transverse slats are respectively arranged in the bottom plate, two transverse slat interval settings, and two transverse slats are arranged in parallel, and two Mounting groove is formed between a transverse slat, is bolted between the transverse slat, and first arm and bolt rotation connect It connects, first arm can be caught in the mounting groove.
9. wing support construction according to claim 8, which is characterized in that two bolts are installed on the transverse slat, Two bolts are located at the both ends of the transverse slat, and one end of first arm is provided with through-hole, first arm it is another One end setting is jagged, and the notch is located at side of first arm far from second arm, and the through-hole is sheathed on one The bolt, after first arm is caught in the mounting groove, another described bolt is located in the notch.
10. wing support construction according to claim 9, which is characterized in that the connection of the transverse slat and first arm Place is provided with a mounting hole, and the other end of the transverse slat is provided with multiple mounting holes, positioned at the multiple of described transverse slat the same end The mounting hole is arranged along the short transverse interval of the transverse slat, and the bolt is installed in the mounting hole.
CN201821254272.4U 2018-08-03 2018-08-03 A kind of wing support construction Active CN209223869U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201821254272.4U CN209223869U (en) 2018-08-03 2018-08-03 A kind of wing support construction

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201821254272.4U CN209223869U (en) 2018-08-03 2018-08-03 A kind of wing support construction

Publications (1)

Publication Number Publication Date
CN209223869U true CN209223869U (en) 2019-08-09

Family

ID=67497402

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201821254272.4U Active CN209223869U (en) 2018-08-03 2018-08-03 A kind of wing support construction

Country Status (1)

Country Link
CN (1) CN209223869U (en)

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GR01 Patent grant
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Address after: No. 688, West Section of Kechuang Road, Chengdu Cross-Strait Science and Technology Industry Development Park, Wenjiang District, Chengdu, Sichuan 610000

Patentee after: Chengdu Tiger Aerospace Technology Co., Ltd.

Address before: No. 688, West Section of Kechuang Road, Chengdu Cross-Strait Science and Technology Industry Development Park, Wenjiang District, Chengdu, Sichuan 610000

Patentee before: CHENGDU TEGEL AEROSPACE TECHNOLOGY CO.,LTD.

CP01 Change in the name or title of a patent holder