CN205239889U - Locking mechanism is connected with wing to fuselage - Google Patents
Locking mechanism is connected with wing to fuselage Download PDFInfo
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- CN205239889U CN205239889U CN201521139019.0U CN201521139019U CN205239889U CN 205239889 U CN205239889 U CN 205239889U CN 201521139019 U CN201521139019 U CN 201521139019U CN 205239889 U CN205239889 U CN 205239889U
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- wing
- accommodation space
- fuselage
- socket
- connection board
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Abstract
The utility model belongs to the technical field of unmanned aerial vehicle, especially, relate to a locking mechanism is connected with wing to fuselage, include: socket, this socket include the socket connecting plate and set up the accommodation space in socket connecting plate one side, are equipped with the through -hole that communicates with the accommodation space on the socket connecting plate, are equipped with the slide rather than the intercommunication on the lateral wall of accommodation space, setting inserting in the slide, the lateral wall of following the relative one side of slide passes the threaded connection spare of being connected with the transmission of inserting, bolt, this bolt include the bolt connection board, set up the pin junction arm on bolt connection board one side, is equipped with the recess on the pin junction arm corresponds one side of through -hole, keeps away from one of bolt connection board at the pin junction arm and serve corresponding threaded connection spare department and be equipped with the portion of dodging, the locking mechanism is connected with wing to fuselage of this embodiment the be convenient for installation and the dismantlement of wing can reduce the operation degree of difficulty, use convenience very.
Description
Technical field
The utility model belongs to unmanned plane technical field, relates in particular to a kind of fuselage and is connected lockable mechanism with wing.
Background technology
At present, the fuselage of unmanned plane is connected fastening with wing be by the mode of being spirally connected substantially, and a kind of mode isTighten from fuselage the inside, another kind of mode is on wing, to open a little storehouse, in little storehouse, tighten, andAnd need on little storehouse, be provided with hatchcover. While needing installation, dismounting wing, need to first open corresponding hatchcoverCan install or dismantle, and be limited to its space size, operating difficulties, uses inconvenience.
Utility model content
The purpose of this utility model is to provide a kind of fuselage to be connected lockable mechanism with wing, is convenient to the peace of wingInstallation and dismantling are unloaded, and can reduce operation easier, use very convenient.
The utility model is achieved in that a kind of fuselage is connected lockable mechanism with wing, described fuselage and machineThe wing connects lockable mechanism and comprises: socket, described socket comprises socket connection board and is arranged on described socket and is connectedThe accommodation space of plate one side is provided with the through hole being communicated with described accommodation space on described socket connection board,The sidewall of described accommodation space is provided with the slideway being communicated with it; Be arranged on inserting in described slideway; From instituteThe sidewall of stating the relative side of slideway passes and the described threaded connector of inserting and being in transmission connection; Latch, described insertingPin comprises latch connecting plate, is arranged on the pin linking arm in described latch connecting plate one side, connects at described pinOne side of the corresponding described through hole of arm is provided with groove, at described pin linking arm away from one of described latch connecting plateOn end, corresponding described threaded connector place is provided with the portion of dodging.
Improve as one, on described socket connection board, be arranged at intervals with the first plate body, the second plate body, instituteState accommodation space and surrounded by described the first plate body, described the second plate body and described socket connection board, described slidewayBe arranged on described the second plate body, described threaded connector is through described the first plate body.
Improve as one, between described threaded connector and described the first plate body, be also provided with T-shaped axle sleeve,The stub end of described T-shaped axle sleeve is arranged in described accommodation space, and the little head end of described T-shaped axle sleeve is arranged onThe outside of described accommodation space is provided with jump ring on the little head end of described T-shaped axle sleeve.
Improve as one, described threaded connector is bolt; On described inserting, be provided with screwed hole, described inThreaded connector with described in insert and be threaded; Or on described inserting, be provided with the through hole passing through for bolt,On described side of inserting near described accommodation space outside, be fixed with plate nut, described bolt and instituteStating plate nut is threaded
As one improve, described in insert as wedge, what described groove was corresponding is set to wedge-shaped slot, described inThe inclined-plane gradient of wedge is consistent with the gradient of the sidewall of corresponding described groove.
As one improve, described in the portion of dodging serve as reasons described pin linking arm end to described latch connecting plate one sideThe groove extending.
Owing to having adopted technique scheme, the fuselage that the utility model provides is connected lockable mechanism bag with wingDraw together: socket, this socket comprises socket connection board and is arranged on the accommodation space of socket connection board one side, insertingSeat connecting plate is provided with the through hole being communicated with accommodation space, is provided with and is communicated with it on the sidewall of accommodation spaceSlideway; Be arranged on inserting in slideway; Pass and the spiral shell of inserting and being in transmission connection from the sidewall of the relative side of slidewayLine connector; Latch, this latch comprises latch connecting plate, is arranged on the pin connection in latch connecting plate one sideArm is provided with groove in a side of the corresponding through hole of pin linking arm, at pin linking arm away from one of latch connecting plateOn end, corresponding threaded connector place is provided with the portion of dodging; When installation, socket is fixedly connected with wing, makes socketThe accommodation space of connecting plate sidepiece is positioned at the inner space of wing, and on wing, corresponding threaded connector place arrangesA handle hole; Latch is fixedly connected with fuselage, and pin linking arm is inserted into accommodation space through through holeIn, then, by the handle hole rotation threaded connector on wing, insert along threaded connector to accommodation spaceInterior movement until snap in the groove on pin linking arm, is tightened threaded connector to realize consolidating of socket and latchFixed connection, wing and fuselage can be fixed together fast; When dismounting, by the behaviour on wingMake hole reverse rotation threaded connector, move the outside of inserting along threaded connector to accommodation space, inserts de-From groove, then, by the other direction pin linking arm being deviate from accommodation space, socket separates with latch, canRealize the fast assembling-disassembling of wing and fuselage; The fuselage of the present embodiment is connected lockable mechanism and is convenient to wing with wingInstallation and removal, can reduce operation easier, use very convenient.
Brief description of the drawings
Fig. 1 is fuselage of the present utility model is connected lockable mechanism sectional structure schematic diagram with wing;
Fig. 2 is fuselage of the present utility model is connected lockable mechanism mounting structure schematic diagram with wing;
Fig. 3 is fuselage of the present utility model is connected the latch of lockable mechanism perspective view with wing;
Fig. 4 is fuselage of the present utility model is connected the socket of lockable mechanism perspective view with wing;
Wherein, 10, latch, 11, latch connecting plate, 12, pin linking arm, 13, groove, 14, dodgePortion, 20, socket, 21, socket connection board, 22, accommodation space, 221, the first plate body, 222, secondPlate body, 23, through hole, 24, slideway, 30, insert, 31, plate nut, 32, fastening bolt, 40,Threaded connector, 41, T-shaped axle sleeve, 42, jump ring.
Detailed description of the invention
In order to make the purpose of this utility model, technical scheme and advantage clearer, below in conjunction with accompanying drawingAnd embodiment, the utility model is further elaborated. Should be appreciated that described herein concreteEmbodiment is only in order to explain the utility model, and is not used in restriction the utility model.
From Fig. 1, Fig. 2, Fig. 3 and Fig. 4, this fuselage is connected lockable mechanism with wing and comprises: with wingThe socket 20 being fixedly connected with, this socket 20 comprises the socket connection board 21 for being connected with wing and is arranged onThe accommodation space 22 of socket connection board 21 1 sides, interval on the socket connection board 21 of accommodation space 22 peripheriesBe provided with four connecting holes, bolt is fixed together socket 20 and wing through connecting hole and wing sidewall,Certainly connecting hole also can be provided with other quantity as required, on socket connection board 21, is provided with accommodatingThe through hole 23 that space 22 is communicated with is provided with the slideway being communicated with accommodation space 22 on the sidewall of accommodation space 2224; Be arranged on and insert 30 in slideway 24; Pass and 30 transmissions of inserting from the sidewall of the relative side of slideway 24The threaded connector 40 connecting; The latch 10 being fixedly connected with fuselage, this latch 10 comprise for fuselageThe latch connecting plate 11 connecting, the pin linking arm 12 that is arranged on latch connecting plate 11 1 medium position places, side,In a side of the corresponding through hole 23 of pin linking arm 12, be provided with groove 13, connect away from latch at pin linking arm 12On one end of plate 11, corresponding threaded connector 40 places are provided with the portion of dodging 14, at the latch of pin linking arm 12 peripheriesOn connecting plate 11, be interval with four connecting holes, bolt through connecting hole and fuselage sidewall by latch 10 and machineBody is fixed together, and connecting hole also can be provided with other quantity as required certainly.
As shown in Figure 2, when installation, socket 20 is fixedly connected with wing, makes socket connection board 21 sidepiecesAccommodation space 22 be positioned at the inner space of wing, on wing, corresponding threaded connector 40 places arrange oneHandle hole; Latch 10 is fixedly connected with fuselage, and by pin linking arm 12 according to the side of arrow A in Fig. 2To being inserted in accommodation space 22 through through hole 23, be then threaded by the handle hole rotation on wingPart 40, insert 30 according to the direction of arrow B in Fig. 2 along threaded connector 40 to the interior movement of accommodation space 22Until snap in the groove 13 on pin linking arm 12, threaded connector 40 is tightened and realized socket 20 and insertBeing fixedly connected with of pin 10, can be fixed together wing and fuselage fast; When dismounting, pass through machineHandle hole on wing reverse rotation threaded connector 40, insert 30 according to the opposite direction of arrow B in Fig. 2 along spiral shellLine connector 40 moves to the outside of accommodation space 22, and the 30 disengaging grooves 13 of inserting, then according in Fig. 2The opposite direction of arrow A is deviate from pin linking arm 12 in accommodation space 22, and socket 20 separates with latch 10,Can realize the fast assembling-disassembling of wing and fuselage; The fuselage of the present embodiment is connected lockable mechanism with wing and is convenient to machineThe installation and removal of the wing, can reduce operation easier, use very convenient.
Certainly, also socket 20 can be fixedly connected with fuselage, make the accommodating sky of socket connection board 21 sidepiecesBetween 22 inner spaces that are positioned at fuselage, on fuselage, corresponding threaded connector 40 places arrange a handle hole,Latch 10 is fixedly connected with wing, so also can realizes.
In the present embodiment, on socket connection board 21, establish spaced the first plate body 221 and the second plate body222, this accommodation space 22 is surrounded by the first plate body 221, the second plate body 222 and socket connection board 21, slidingRoad 24 is arranged on the second plate body 222, and threaded connector 40 is through the first plate body 221 and 30 transmissions of insertingConnect.
Certainly, accommodation space 22 can be also to be surrounded by tube-shaped tube and socket connection board 21, and slideway 24 arrangesOn the sidewall of tube-shaped tube, threaded connector 40 is through passing from the sidewall of tube-shaped tube and slideway 24 opposite sides30 be in transmission connection with inserting.
In the present embodiment, insert 30 for wedge, groove 13 correspondences be set to wedge-shaped slot, wedgeInclined-plane gradient consistent with the gradient of the sidewall of corresponding groove 13.
In the present embodiment, dodge portion 14 and serve as reasons pin linking arm 12 ends to the 11 1 sides extensions of latch connecting plateGroove.
In the present embodiment, threaded connector 40 is bolt, is provided with screwed hole inserting on 30, and screw thread connectsFitting 40 30 is threaded with inserting; Or be provided with the through hole passing through for bolt on 30 inserting, inserting30 are provided with plate nut 31 near the side in accommodation space 22 outsides, and bolt and plate nut 31 screw threads connectConnect, this plate nut 31 30 is fixedly connected with inserting by fastening bolt 32.
In the present embodiment, between threaded connector 40 and the sidewall of accommodation space 22, be also provided with T-shaped axleCover 41, the stub end of this T-shaped axle sleeve 41 is arranged in accommodation space 22, the little head end of this T-shaped axle sleeve 41Be positioned at the outside of accommodation space 22, on the little head end of T-shaped axle sleeve 41, be provided with jump ring 42, by T-shaped axle sleeve41 are fixed together with the sidewall of accommodation space 22, prevent that T-shaped axle sleeve 41 from dropping.
The foregoing is only preferred embodiment of the present utility model, not in order to limit the utility model,All any amendments of doing within spirit of the present utility model and principle, be equal to and replace and improvement etc., all shouldWithin being included in protection domain of the present utility model.
Claims (6)
1. a fuselage is connected lockable mechanism with wing, it is characterized in that, described fuselage is connected lockable mechanism with wing and comprises: socket, described socket comprises socket connection board and is arranged on the accommodation space of described socket connection board one side, on described socket connection board, be provided with the through hole being communicated with described accommodation space, on the sidewall of described accommodation space, be provided with the slideway being communicated with it; Be arranged on inserting in described slideway; Pass and the described threaded connector of inserting and being in transmission connection from the sidewall of the relative side of described slideway; Latch, described latch comprises latch connecting plate, is arranged on the pin linking arm in described latch connecting plate one side, in a side of the corresponding described through hole of described pin linking arm, be provided with groove, on the one end at described pin linking arm away from described latch connecting plate, corresponding described threaded connector place is provided with the portion of dodging.
2. fuselage according to claim 1 is connected lockable mechanism with wing, it is characterized in that, on described socket connection board, be arranged at intervals with the first plate body, the second plate body, described accommodation space is surrounded by described the first plate body, described the second plate body and described socket connection board, described installation of slide track is on described the second plate body, and described threaded connector is through described the first plate body.
3. fuselage according to claim 2 is connected lockable mechanism with wing, it is characterized in that, between described threaded connector and described the first plate body, be also provided with T-shaped axle sleeve, the stub end of described T-shaped axle sleeve is arranged in described accommodation space, the little head end of described T-shaped axle sleeve is arranged on the outside of described accommodation space, on the little head end of described T-shaped axle sleeve, is provided with jump ring.
4. be connected lockable mechanism according to the fuselage described in claims 1 to 3 any one with wing, it is characterized in that, described threaded connector is bolt; On described inserting, be provided with screwed hole, described threaded connector with described in insert and be threaded; Or on described inserting, be provided with the through hole passing through for bolt, on described side of inserting near described accommodation space outside, be fixed with plate nut, described bolt is threaded with described plate nut.
5. fuselage according to claim 4 is connected lockable mechanism with wing, it is characterized in that, described in insert as wedge, what described groove was corresponding is set to wedge-shaped slot, the inclined-plane gradient of described wedge is consistent with the gradient of the sidewall of corresponding described groove.
6. fuselage according to claim 5 is connected lockable mechanism with wing, it is characterized in that, described in the portion's of dodging groove that described pin linking arm end extends to described latch connecting plate one side of serving as reasons.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521139019.0U CN205239889U (en) | 2015-12-31 | 2015-12-31 | Locking mechanism is connected with wing to fuselage |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521139019.0U CN205239889U (en) | 2015-12-31 | 2015-12-31 | Locking mechanism is connected with wing to fuselage |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205239889U true CN205239889U (en) | 2016-05-18 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201521139019.0U Active CN205239889U (en) | 2015-12-31 | 2015-12-31 | Locking mechanism is connected with wing to fuselage |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205239889U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106061190A (en) * | 2016-08-05 | 2016-10-26 | 陈开红 | Ventilating electrical cabinet with dismountable latch fixed column assembly |
| CN106061191A (en) * | 2016-08-05 | 2016-10-26 | 陈开春 | Electrical cabinet convenient to dismount and provided with latch fixed column assembly |
| CN106231831A (en) * | 2016-08-05 | 2016-12-14 | 李常明 | A kind of have dismountable breech lock and fix the safety electric cabinet of column assembly |
| CN106304720A (en) * | 2016-08-05 | 2017-01-04 | 桐乡市恩曼进出口有限公司 | A kind of have breech lock and fix column assembly and can the regulator cubicle of dedusting |
| CN106300042A (en) * | 2016-08-05 | 2017-01-04 | 桐乡市恩曼进出口有限公司 | A kind of dispel the heat and there is breech lock fix the regulator cubicle of column assembly |
-
2015
- 2015-12-31 CN CN201521139019.0U patent/CN205239889U/en active Active
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106061190A (en) * | 2016-08-05 | 2016-10-26 | 陈开红 | Ventilating electrical cabinet with dismountable latch fixed column assembly |
| CN106061191A (en) * | 2016-08-05 | 2016-10-26 | 陈开春 | Electrical cabinet convenient to dismount and provided with latch fixed column assembly |
| CN106231831A (en) * | 2016-08-05 | 2016-12-14 | 李常明 | A kind of have dismountable breech lock and fix the safety electric cabinet of column assembly |
| CN106304720A (en) * | 2016-08-05 | 2017-01-04 | 桐乡市恩曼进出口有限公司 | A kind of have breech lock and fix column assembly and can the regulator cubicle of dedusting |
| CN106300042A (en) * | 2016-08-05 | 2017-01-04 | 桐乡市恩曼进出口有限公司 | A kind of dispel the heat and there is breech lock fix the regulator cubicle of column assembly |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |