CN203996922U - A kind of mooring grid, airborne mooring mast and quick mooring gear - Google Patents
A kind of mooring grid, airborne mooring mast and quick mooring gear Download PDFInfo
- Publication number
- CN203996922U CN203996922U CN201420410387.3U CN201420410387U CN203996922U CN 203996922 U CN203996922 U CN 203996922U CN 201420410387 U CN201420410387 U CN 201420410387U CN 203996922 U CN203996922 U CN 203996922U
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- Prior art keywords
- mooring
- flase floor
- airborne
- grid
- mast
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Abstract
The utility model embodiment discloses a kind of mooring grid, airborne mooring mast and quick mooring gear, and this mooring gear comprises airborne mooring mast and mooring grid.Airborne mooring mast comprises connecting device, elastic rod and spheroid; Wherein, connecting device is for being arranged on airborne mooring mast the mounting base of unmanned plane.Mooring grid comprises upper grid plate, bottom flase floor, support and driven unit; Wherein, upper grid plate is fixed on support, and bottom flase floor is arranged on the below of upper grid plate; Upper grid plate is provided with multiple entrance holes; Bottom flase floor is provided with multiple hole clippings, and when in the first mode of operation, described driven unit drives the flase floor operation of described bottom, and entrance hole and hole clipping form and meet the passage that airborne mooring mast turnover requires; When in the second mode of operation, described driven unit drives the flase floor operation of described bottom, and entrance hole and hole clipping are blocked airborne mooring mast it cannot be extracted.
Description
Technical field
The utility model relates to aerocraft technical field, more particularly, relates to a kind of mooring grid, airborne mooring mast and quick mooring gear.
Background technology
Mooring gear comprises airborne mooring mast and mooring grid.Wherein, airborne mooring mast is arranged on unmanned plane, and mooring grid is arranged on flight deck (platform that unmanned plane is shut down maybe can be realized in hardstand).Mooring gear is most important for the landing of unmanned plane, this device can make unmanned plane fast, safety warship (land) it is reliably fixing.
At present, the mooring mast that mooring gear adopts is expansion link, and the head of mooring mast is provided with fork-shaped latch-up structure.Unmanned plane is when warship (land), and mooring mast inserts the locking of mooring grid, produces when avoiding unmanned plane warship and breaks away and topple; Unmanned plane is in the time taking off, and this device ensures that unmanned plane reaches maximum lift, and ensures to discharge unmanned plane under survival wind speed, wind direction condition, to ensure that it is leaving safely warship (land) district.
But, while adopting above-mentioned mooring mode, mainly complete the mooring of unmanned plane by the fork-shaped latch-up structure on operation mooring mast.Therefore, the designing requirement of mooring mast is higher, need to complete " stretch out-lock " and " release-retraction " action supporting corresponding driving and control setup.This technical scheme, has increased the complexity of unmanned plane, has reduced the reliability of unmanned plane.In addition, the volume of mooring mast is relatively large, and action is complicated, and weight is also larger, thereby has reduced the capacity weight of unmanned plane.
Therefore, how to increase the capacity weight of unmanned plane, safety and reliability when raising unmanned plane warship (land), becomes those skilled in the art's technical matters urgently to be resolved hurrily.
Utility model content
In view of this, first object of the present utility model is to provide a kind of mooring grid, to improve the safety and reliability of unmanned plane, increases the capacity weight of unmanned plane; Second object of the present utility model is to provide a kind of airborne mooring mast; The 3rd object of the present utility model is to provide a kind of mooring gear fast.
For realizing above-mentioned first object, the utility model provides following technical scheme:
A kind of mooring grid, described mooring grid comprises upper grid plate, bottom flase floor, support and driven unit.Wherein, described upper grid plate is fixed on described support, and described bottom flase floor is arranged on the below of described upper grid plate; Described upper grid plate is provided with multiple entrance holes, and described entrance hole is cellular layout, and the aperture of described entrance hole is along diminishing gradually near the direction of described bottom flase floor; On the flase floor of described bottom, be provided with multiple hole clippings.When in the first mode of operation, described driven unit drives the flase floor operation of described bottom, forms the passage of the spheroid turnover requirement that meets described airborne mooring mast; When in the second mode of operation, described driven unit drives the flase floor operation of described bottom, and the spheroid of described airborne mooring mast is stuck in described hole clipping.
Preferably, in above-mentioned mooring gear, between described bottom flase floor and described support, be provided with guide rail, described bottom flase floor can move on described guide rail, and the straight-line motion mouth of described driven unit is connected with described bottom flase floor and drives the flase floor translation of described bottom; When in the first mode of operation, described entrance hole and corresponding described hole clipping form and meet the passage that the spheroid turnover of airborne mooring mast requires; When in the second mode of operation, described entrance hole can be stuck in the spheroid of described airborne mooring mast in described hole clipping with corresponding described hole clipping.
Preferably, in above-mentioned mooring gear, described hole clipping is cellular layout, and its aperture is along becoming gradually large away from the direction of described upper grid plate.
Preferably, in above-mentioned mooring gear, described hole clipping is cellular layout, and described hole clipping is straight hole.
Preferably, in above-mentioned mooring gear, when in the first mode of operation, described bottom flase floor is under the driving of described driven unit, and the aperture of described hole clipping is variable large; When in the second mode of operation, described bottom flase floor is under the driving of described driven unit, and the aperture of described hole clipping can diminish.
Preferably, in above-mentioned mooring gear, described driven unit is cylinder, hydraulic actuating cylinder or electric cylinder.
In the time that unmanned plane warship (land), this mooring grid is in the first mode of operation, the mooring mast that is provided with spheroid inserts in entrance hole, the spheroid of airborne mooring mast passes through passage, enter in hole clipping, now this mooring gear switches to the second mode of operation, and hole clipping motion is stuck in the spheroid of airborne mooring mast in corresponding hole clipping, completes the mooring of unmanned plane; In the time that unmanned plane takes off, this mooring gear switches to the first mode of operation by the second mode of operation, entrance hole and hole clipping form and meet the passage that spheroid turnover requires, and airborne mooring mast is extracted under the effect of unmanned plane lift from honeycomb hole, thereby realizes letting fly away of unmanned plane.Due to the mooring gear adopting in the utility model, the cooperation of upper grid plate and bottom flase floor can complete the fixing of airborne mooring mast and discharge, therefore, adopt the mooring gear in the utility model lower for the requirement that is arranged on the airborne mooring mast on unmanned plane, the function of mooring mast is relatively single, simple in structure, thus the reliability of unmanned plane improved, increase the capacity weight of unmanned plane.
Second object of the present utility model is to provide a kind of airborne mooring mast, and described airborne mooring mast is used in conjunction with including but not limited to the mooring grid described in above-mentioned arbitrary scheme, and described airborne mooring mast comprises connecting device, elastic rod and spheroid; Wherein, connecting device is for being arranged on elastic rod the pedestal of unmanned plane, and elastic rod connects spheroid and connecting device.
The 3rd object of the present utility model is to provide a kind of mooring gear fast, comprises mooring grid and airborne mooring mast, and described airborne mooring mast comprises connecting device, elastic rod and spheroid; Connecting device is for being arranged on airborne mooring mast the mounting base of unmanned plane; Described mooring grid is the mooring grid described in the above-mentioned arbitrary technical scheme of employing.
Brief description of the drawings
In order to be illustrated more clearly in the utility model embodiment or technical scheme of the prior art, to the accompanying drawing of required use in embodiment or description of the Prior Art be briefly described below, apparently, accompanying drawing in the following describes is only embodiment more of the present utility model, for those of ordinary skill in the art, do not paying under the prerequisite of creative work, can also obtain according to these accompanying drawings other accompanying drawing.
Side-looking structural representation when the first mode of operation of a kind of mooring gear that Fig. 1 provides for the utility model embodiment;
Side-looking structural representation when the second mode of operation of a kind of mooring gear that Fig. 2 provides for the utility model embodiment;
Side-looking structural representation when the first mode of operation of the second mooring gear that Fig. 3 provides for the utility model embodiment;
Side-looking structural representation when the second mode of operation of the second mooring gear that Fig. 4 provides for the utility model embodiment;
Side-looking structural representation when the first mode of operation of the third mooring gear that Fig. 5 provides for the utility model embodiment;
Side-looking structural representation when the second mode of operation of the third mooring gear that Fig. 6 provides for the utility model embodiment;
The plan structure schematic diagram of a kind of upper grid plate that Fig. 7 provides for the utility model embodiment;
The plan structure schematic diagram of the another kind of upper grid plate that Fig. 8 provides for the utility model embodiment.
Wherein: 1 is that unmanned plane, 211 is that support, 212 is that guide rail, 213 is that upper grid plate, 214 is that bottom flase floor, 215 is that entrance hole, 216 is that hole clipping, 217 is that actuating device, 221 is that elastic rod, 222 is that spheroid, 223 is that connecting device, 3 is deck (hardstand).
Detailed description of the invention
For this reason, first core of the utility model is open a kind of mooring grid, taking the safety, reliability and the effective mission payload of increase unmanned plane that improve unmanned plane as object; Second core of the utility model is the airborne mooring mast of open one; The 3rd core of the utility model is the quick mooring gear of open one.Below, with reference to accompanying drawing, embodiment is described.In addition the utility model content that the embodiment shown in, does not record claim plays any restriction effect.The solution of the utility model that in addition,, the full content of the represented formation of embodiment is not limited to record as claim is necessary.
As shown in Figures 1 to 8, mooring grid comprises upper grid plate 213, bottom flase floor 214, support 211 and driven unit 217; Wherein, upper grid plate 213 is fixed on support 211, and bottom flase floor 214 is arranged on the below of upper grid plate 213; Upper grid plate 213 is provided with multiple entrance holes 215, and entrance hole 215 is cellular layout; The aperture of entrance hole 215 is along diminishing gradually near the direction of bottom flase floor 214; Bottom flase floor 214 is provided with multiple hole clippings 216.When in the first mode of operation, driven unit drives bottom flase floor 214 to move, and forms and meets the passage that spheroid 222 turnover require; When in the second mode of operation, driven unit drives bottom flase floor 214 to move, and spheroid 222 is stuck in hole clipping 216.
In the time that unmanned plane warship (land), this mooring grid is in the first mode of operation, the mooring mast that is provided with spheroid 222 inserts in any entrance hole 215, the spheroid 222 of airborne mooring mast enters in hole clipping 216 by passage, now this mooring gear switches to the second mode of operation, the spheroid 222 of airborne mooring mast is stuck in corresponding hole clipping 216, completes the mooring of unmanned plane; In the time that unmanned plane takes off, this mooring gear switches to the first mode of operation by the second mode of operation, entrance hole 215 passes in and out with the spheroid 222 that hole clipping 216 formation meet airborne mooring mast the passage requiring, airborne mooring mast is under the effect of unmanned plane lift, the spheroid of airborne mooring mast 222 is extracted from honeycomb hole, thereby realized letting fly away of unmanned plane.Due to the mooring gear adopting in the utility model, bottom flase floor 214 can complete the mooring of mooring mast, therefore, adopt the mooring gear in the utility model lower for the requirement that is arranged on the mooring mast on unmanned plane, the function of mooring mast is relatively single, simple in structure, thus the reliability of unmanned plane improved, increase the capacity weight of unmanned plane.
In an embodiment of the present utility model, bottom flase floor 214 is provided with guide rail 212 with support 211, bottom flase floor 214 is slidably arranged on guide rail 212, and the straight-line motion mouth of driven unit is connected with bottom flase floor 214 and drives flase floor 214 translations of described bottom; When in the first mode of operation, entrance hole 215 passes in and out with the spheroid 222 that corresponding hole clipping 216 formation meet airborne mooring mast the passage requiring; When in the second mode of operation, hole clipping 216 is moved the spheroid of airborne mooring mast 222 is stuck in hole clipping 216.
In the utility model embodiment, the arrangement of entrance hole 215 on upper grid plate 213 has multiple, for example, be matrix form layout, cellular layout.As shown in Figure 7, entrance hole 215 is cellular at the arrangement form of upper grid plate 213.Wherein, the projection of shape of entrance hole 215 is equilateral polygon or circle, and the aperture of entrance hole 215 is along becoming gradually greatly (can be understood as the aperture of entrance hole 215 to diminishing gradually near the direction of bottom flase floor 214) away from the direction of bottom flase floor 214, so setting can ensure in any entrance hole of spheroid 222 radom insertion on mooring mast.As shown in Figure 8, entrance hole 215 is matrix structure and arranges, and the aperture of entrance hole 215 is along diminishing gradually (aperture that can be understood as entrance hole 215 becomes large gradually along the direction away from bottom flase floor 214) near the direction of bottom flase floor 214, and so setting can ensure in any entrance hole of spheroid 222 radom insertion on mooring mast.
The arrangement of the hole clipping 216 of bottom flase floor 214 is identical with the arrangement of the entrance hole 215 of upper grid plate 213; In the time that the entrance hole 215 of upper grid plate 213 is arranged for matrix structure, the hole clipping 216 homography shape structural arrangement of bottom flase floor 214.In the time that the entrance hole 215 of upper grid plate 213 is arranged for cellular structure, the corresponding cellular structure layout of the hole clipping 216 of bottom flase floor 214, the cross sectional shape of hole clipping 216 is circular.So be arranged so that the probability that spheroid 222 inserts mooring grid increases greatly.
The aperture of the hole clipping 216 of the utility model middle and lower part flase floor 214 is along becoming gradually greatly away from the direction of upper grid plate 213, as depicted in figs. 1 and 2.That is to say, the entrance hole 215 of upper grid plate 213 is taper hole (or approximate taper hole), and the hole clipping 216 of bottom flase floor 214 is reverse taper hole (or approximate reverse taper hole).When in the first mode of operation, when spheroid 222 enters to hole clipping 216 by entrance hole 215, because the aperture of hole clipping 216 becomes greatly gradually along the direction away from upper grid plate 213, therefore, the power less (or without application force) that the hole wall of hole clipping 216 acts on spheroid 222; When in the second mode of operation, spheroid 222 is positioned at hole clipping 216, and hole clipping 216 forms wedge structure with spheroid 222, and therefore spheroid 222 has the trend moving downward, thereby further strains unmanned plane.
Or the aperture of the hole clipping 216 of the utility model middle and lower part flase floor 214 is constant, for straight hole as shown in Figure 3 to Figure 4.
In the another embodiment of the utility model, bottom flase floor 214 is for having independently, the clip-bore device of variable-diameter, as shown in Figure 5 and Figure 6, wherein, the axial alignment of the axis of hole clipping 216 and entrance hole 215, each hole clipping 216 forms an incomplete taper hole by multiple clamps that are obliquely installed, and multiple clamp is under the drive of driven unit, to mutually near or mutually away from direction move, the close movement mutually of multiple clamps, diminishes the aperture of hole clipping 216 gradually; Mutually away from direction move, the aperture of hole clipping 216 is become greatly gradually, block the screens of spheroid 222 and the passage that spheroid passes in and out thereby hole clipping 216 is formed under the cooperation of entrance hole 215.
Driven unit is the actuating unit that can export desired movement, for example, be cylinder, hydraulic actuating cylinder, electric cylinder, linear electric motors etc., and the utility model embodiment is not limited only to above-mentioned form.
Act on the resistance on unmanned plane in order to reduce unmanned plane this mooring gear when the takeoff condition, when in the first mode of operation, entrance hole 215 and hole clipping 216 are on both face of joints, and the diameter of hole clipping 216 should equal entrance hole 215 diameters; When in the second mode of operation, entrance hole 215 and hole clipping 216 are on both face of joints, and the diameter of hole clipping 216 should be less than the maximum gauge of spheroid 222.
The invention also discloses a kind of airborne mooring mast, this mooring mast is used in conjunction with including but not limited to the mooring grid described in above-mentioned arbitrary technical scheme, and this airborne mooring mast comprises connecting device 223, elastic rod 221 and spheroid 222; Wherein, connecting device 223 is for being arranged on elastic rod the mounting base of unmanned plane, and elastic rod 221 connects spheroid 222 and connecting device 223.Adopt the airborne mooring mast of the utility model structure can reduce significantly the weight of unmanned plane, therefore, capacity weight that can corresponding raising unmanned plane.
The invention also discloses a kind of mooring gear fast, comprise mooring grid and airborne mooring mast, wherein, mooring grid is arranged on the place that unmanned plane can take-off and landing, for example, can be deck 3, high building, automobile, train etc.Wherein, mooring grid is the mooring grid described in above-mentioned arbitrary technical scheme, and described airborne mooring mast is the airborne mooring mast described in above-mentioned arbitrary technical scheme.Because above-mentioned mooring grid and airborne mooring mast have above-mentioned effect, the quick mooring gear in the utility model embodiment also has corresponding effect, repeats no more herein.
To the above-mentioned explanation of the disclosed embodiments, make professional and technical personnel in the field can realize or use the utility model.To be apparent for those skilled in the art to the multiple amendment of these embodiment, General Principle as defined herein can, in the situation that not departing from spirit or scope of the present utility model, realize in other embodiments.Therefore, the utility model will can not be restricted to these embodiment shown in this article, but will meet the widest scope consistent with principle disclosed herein and features of novelty.
Claims (9)
1. a mooring grid, is characterized in that, described mooring grid comprises upper grid plate, bottom flase floor, support and driven unit; Wherein, described upper grid plate is fixed on described support, and described bottom flase floor is arranged on the below of described upper grid plate; Described upper grid plate is provided with multiple entrance holes, and described entrance hole is cellular layout, and the aperture of described entrance hole is diminishing gradually near the direction of described bottom flase floor; Described bottom flase floor is provided with multiple hole clippings, and when in the first mode of operation, described driven unit drives the flase floor operation of described bottom, forms the passage of the spheroid turnover requirement that meets airborne mooring mast; When in the second mode of operation, described driven unit drives the flase floor operation of described bottom, and the spheroid of described airborne mooring mast is stuck in described hole clipping.
2. mooring grid as claimed in claim 1, it is characterized in that, between described bottom flase floor and described support, be provided with guide rail, described bottom flase floor can move on described guide rail, and described driven unit is connected with described bottom flase floor and drives the flase floor translation of described bottom; When in the first mode of operation, described entrance hole and corresponding described hole clipping form and meet the passage that the spheroid turnover of airborne mooring mast requires; When in the second mode of operation, described entrance hole is stuck in the spheroid of described airborne mooring mast in described hole clipping with corresponding described hole clipping.
3. mooring grid as claimed in claim 2, is characterized in that, described hole clipping is cellular layout, and its aperture is along becoming gradually large away from the direction of described upper grid plate.
4. mooring grid as claimed in claim 2, is characterized in that, described hole clipping is cellular layout, and described hole clipping is straight hole.
5. mooring grid as claimed in claim 4, is characterized in that, described hole clipping and described entrance hole are in the equal diameters of contact surface.
6. mooring grid as claimed in claim 5, is characterized in that, described driven unit adopts cylinder or hydraulic actuating cylinder or electric cylinder to realize relative motion.
7. mooring grid as claimed in claim 1, it is characterized in that, when in the first mode of operation, described bottom flase floor is under the driving of described driven unit, it is large that the aperture of described hole clipping becomes, when in the second mode of operation, described bottom flase floor is under the driving of described driven unit, and the aperture of described hole clipping diminishes.
8. an airborne mooring mast, is characterized in that, the mooring grid in this airborne mooring mast and claim 1-7 described in any one is used in conjunction with, and described airborne mooring mast comprises connecting device, elastic rod and spheroid; Wherein, connecting device is for being arranged on elastic rod the pedestal of unmanned plane, and elastic rod connects spheroid and connecting device.
9. a quick mooring gear, comprises mooring grid and airborne mooring mast, it is characterized in that, described mooring grid is the mooring grid described in any one in claim 1 to 7, and described airborne mooring mast is airborne mooring mast described in claim 8.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420410387.3U CN203996922U (en) | 2014-07-24 | 2014-07-24 | A kind of mooring grid, airborne mooring mast and quick mooring gear |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420410387.3U CN203996922U (en) | 2014-07-24 | 2014-07-24 | A kind of mooring grid, airborne mooring mast and quick mooring gear |
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| Publication Number | Publication Date |
|---|---|
| CN203996922U true CN203996922U (en) | 2014-12-10 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420410387.3U Expired - Fee Related CN203996922U (en) | 2014-07-24 | 2014-07-24 | A kind of mooring grid, airborne mooring mast and quick mooring gear |
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| CN (1) | CN203996922U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104097787A (en) * | 2014-07-24 | 2014-10-15 | 郑州德莱孚科技有限公司 | Mooring grille, onboard mooring mast and quick mooring device |
| CN109229383A (en) * | 2018-10-17 | 2019-01-18 | 中国特种飞行器研究所 | One kind is novel to be tethered at unmanned plane |
-
2014
- 2014-07-24 CN CN201420410387.3U patent/CN203996922U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104097787A (en) * | 2014-07-24 | 2014-10-15 | 郑州德莱孚科技有限公司 | Mooring grille, onboard mooring mast and quick mooring device |
| CN109229383A (en) * | 2018-10-17 | 2019-01-18 | 中国特种飞行器研究所 | One kind is novel to be tethered at unmanned plane |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20141210 Termination date: 20160724 |
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| CF01 | Termination of patent right due to non-payment of annual fee |