CN203937864U - Luggage carrier device and aircraft - Google Patents
Luggage carrier device and aircraft Download PDFInfo
- Publication number
- CN203937864U CN203937864U CN201420350901.9U CN201420350901U CN203937864U CN 203937864 U CN203937864 U CN 203937864U CN 201420350901 U CN201420350901 U CN 201420350901U CN 203937864 U CN203937864 U CN 203937864U
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- luggage carrier
- support
- carrier device
- fixing
- holding
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Abstract
The utility model discloses a kind of luggage carrier device, is fixed on fuselage and comprises latch part and luggage carrier.Latch part is arranged at fuselage and comprises resettlement section, a pair of guide groove and clasp groove, the front opening of resettlement section also comprises pair of sidewalls, rear wall, diapire and accepting hole, rear wall connects described sidewall, guide groove is arranged at sidewall, clasp groove is arranged at diapire close opening, luggage carrier comprises fixing-holding rack and fixing arm, fixing arm protrudes from the bottom surface of fixing-holding rack, fixing-holding rack comprises rail portion and the holding part that is convexly set in fixing-holding rack end face, rail portion comprises pair of guide rails, rail portion is contained in accepting hole, and guide rail slips in guide groove, and holding part is contained in clasp groove.The utility model also provides a kind of aircraft.The luggage carrier device that the utility model provides and aircraft, by guide rail being slipped into or departing from chute and holding part, accommodate or depart from clasp groove, just luggage carrier device can be installed on or dismantle in latch part, thereby improve the comfort feature of luggage carrier device Assembly &Disassembly.
Description
Technical field
The utility model relates to a kind of aerial device, particularly a kind of luggage carrier device and aircraft.
Background technology
For large-scale manned aircraft, small aircraft has miniaturization, flexible, low price, and the feature easily of rising and falling, is therefore widely used in model plane, agricultural, fire-fighting and the field of taking photo by plane.But the luggage carrier device of existing small aircraft is fixed on fuselage by the mode of lock screw, all needs to use mounting tools in Assembly &Disassembly process, as screwdriver, make all inconvenience of Assembly &Disassembly of luggage carrier device.
Utility model content
The purpose of this utility model is to solve in prior art because luggage carrier device being fixed on by lock screw to the problem of the Assembly &Disassembly inconvenience that fuselage causes.
For addressing the above problem, the utility model provides following technical scheme.
On the one hand, the utility model provides a kind of luggage carrier device, and it is fixed on the fuselage of aircraft.Described luggage carrier device comprises latch part and luggage carrier, described latch part is arranged at described fuselage and comprises resettlement section, a pair of guide groove and clasp groove, the front opening of described resettlement section also comprises pair of sidewalls, rear wall, diapire and accepting hole, described rear wall connects described sidewall, described guide groove is arranged at described sidewall, described accepting hole is by described sidewall, described rear wall and described diapire surround, described clasp groove is arranged at diapire close described opening, described luggage carrier comprises fixing-holding rack and at least one fixing arm, described fixing arm deviates from described fuselage protrusion from the bottom surface of described fixing-holding rack, described fixing-holding rack comprises rail portion and the holding part that is convexly set in described fixing-holding rack end face, the shape of described rail portion is consistent with the shape of described accepting hole and comprise pair of guide rails, described rail portion is contained in described accepting hole, described guide rail slips in described guide groove, described holding part has certain elasticity and part is contained in described clasp groove, so that described luggage carrier is fixed on to described latch part.
Preferably, the framed structure that described rail portion is cuboid, described guide rail extends in opposite directions from a pair of relative sidewall.
Preferably, described holding part comprises a cross-notching, press section and projection, and described fluting is positioned at the both sides of described press section so that described press section has elasticity, and described projection is protruding to described fuselage and be contained in described clasp groove from described press section.
Preferably, described fixing-holding rack comprises the first support and the second support, and described rail portion and described holding part are convexly set in described the first support, and described fixing arm deviates from described fuselage from described the second support and protrudes.
Preferably, described fixing-holding rack also comprises a plurality of feets, described feet be individually fixed in described the first support with described the second support to be fixedly connected with described the first support and described the second support.
Preferably, described the first support is provided with a plurality of the first stent foots, and described the second support is provided with a plurality of the second stent foots, and described in each, feet is individually fixed in described in each the first stent foot and the second stent foot described in each.
Preferably, described in each, the first stent foot is provided with the first holding hole, and described in each, the second stent foot is provided with the second holding hole, and described in each, feet is individually fixed in described in each the first holding hole and described in each in the second holding hole.
Preferably, described luggage carrier device comprises a pair of fixing arm, and described fixing arm all deviates from described fuselage protrusion from the bottom surface of described the second support.
Preferably, described fixing-holding rack comprises the limiting section that is convexly set in described the first support, and described limiting section support is by described rear wall.
On the other hand, the utility model also provides a kind of aircraft, the above-mentioned luggage carrier device that it comprises fuselage and is installed on fuselage.
The utility model provide with luggage carrier device and aircraft, cause is by being contained in described rail portion in described accepting hole, described guide rail slips in described guide groove, described holding part is partly contained in described clasp groove just can be fixed on latch part by luggage carrier, be about to luggage carrier and be fixed on fuselage, only need make described holding part depart from described clasp groove, and make described guide rail skid off described guide groove, just luggage carrier slave can be removed with it, make the Assembly &Disassembly of luggage carrier device convenient quick again, greatly improved the comfort feature that luggage carrier device is used.
Accompanying drawing explanation
In order to be illustrated more clearly in the technical solution of the utility model, to the accompanying drawing of required use in embodiment be briefly described below, apparently, accompanying drawing in the following describes is only embodiments more of the present utility model, for those of ordinary skills, do not paying under the prerequisite of creative work, can also obtain from these accompanying drawings other accompanying drawing.
Figure l is the assembling schematic diagram of the aircraft that provides of the utility model.
Fig. 2 is the schematic diagram of the latch part in Fig. 1.
Fig. 3 is the enlarged diagram of the oval III in Fig. 2.
Fig. 4 is the schematic diagram of the luggage carrier in Fig. 1.
Fig. 5 is the schematic diagram of another angle of Fig. 4.
Fig. 6 is the enlarged diagram of circle VI in Fig. 5.
The specific embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the utility model embodiment is clearly and completely described.
Please refer to Fig. 1, the aircraft 100 that the utility model provides comprises fuselage 10 and is installed on the luggage carrier device 20 of fuselage 10.
Please refer to Fig. 1 to Fig. 4, described luggage carrier device 20 comprises latch part 30 and luggage carrier 40, described latch part 30 is arranged at described fuselage 10 and comprises resettlement section 32, a pair of guide groove 34 and clasp groove 36, the front opening of described resettlement section 32 also comprises pair of sidewalls 320, rear wall 322, diapire 324 and accepting hole 326, described rear wall 322 connects described sidewall 320, described guide groove 34 is arranged at described sidewall 320, described accepting hole 324 is by sidewall 320, rear wall 322 and diapire 324 surround, described clasp groove 36 is arranged at diapire 324 close described opening, described luggage carrier 40 comprises fixing-holding rack 42 and at least one fixing arm 44, described fixing arm 44 deviates from described fuselage 10 protrusions from the bottom surface of described fixing-holding rack 42, described fixing-holding rack 42 comprises rail portion 420 and the holding part 422 that is convexly set in described fixing-holding rack 42 end faces, the shape of the shape of described rail portion 420 and described accepting hole 326 is consistent and comprise pair of guide rails 4202, described rail portion 420 is contained in described accepting hole 326, described guide rail 4202 slips in described guide groove 34, described holding part 422 has certain elasticity and part is contained in described clasp groove 36, so that described luggage carrier 40 is fixed on to described latch part 30.
Cause is by being contained in described rail portion 420 in described accepting hole 326, described guide rail 4202 slips in described guide groove 34, described holding part 422 parts are contained in described clasp groove 36 and just luggage carrier 40 can be fixed on to latch part 30, are about to luggage carrier 40 and are fixed on fuselage 10; Only need make described holding part 422 depart from described clasp groove 36, and make described guide rail 4202 skid off described guide groove 34, just luggage carrier 40 can be removed from fuselage 10, make the Assembly &Disassembly of luggage carrier 40 convenient quick again, greatly improved the comfort feature that luggage carrier device 20 is used, solved prior art because all need to use mounting tools in Assembly &Disassembly process, as screwdriver, and the problem of the Assembly &Disassembly inconvenience causing.
Particularly, during installation, as fuselage 10 as described in luggage carrier 40 need being fixed on, only need described rail portion 420 be contained in described accepting hole 326 and described guide rail 4202 is slipped in described guide groove 34, described holding part 422 parts are contained in described clasp groove 36, just luggage carrier 40 can be fixed on to latch part 30, be about to luggage carrier 40 and be fixed on fuselage 10.During dismounting, press described holding part 422 and make holding part 422 depart from clasp grooves 36, and make the described guide rail 4202 described guide groove 34 that slips away, just can, by luggage carrier 40 from described latch part 30 dismountings, be about to luggage carrier 40 from described fuselage 10 dismountings.In other words, described luggage carrier device 20 of the present utility model is in Assembly &Disassembly process, all do not need to use mounting tools, just described luggage carrier device 20 can be installed on to fuselage 10 or dismantle from fuselage 10, greatly improve the comfort feature of described luggage carrier device 20 Assembly &Disassembly, thereby improved the comfort feature using.
In the present embodiment, described diapire 324 is inclined-plane and tilts towards described opening from described rear wall 322, and described guide rail 4202 is easily slipped in described guide groove 34.
In a kind of optional embodiment, the framed structure that described rail portion 420 is cuboid, described guide rail 4202 extends in opposite directions from a pair of relative sidewall 320.
Particularly, described guide rail 4202 is positioned at the top of sidewall 320, and described guide groove 34 is arranged at the intersection of described sidewall 320 and described diapire 324, so that described rail portion 420 can be contained in described accepting hole 326.
Please refer to Fig. 2 to Fig. 6, in a kind of optional embodiment, described holding part 422 comprises a cross-notching 4220, press section 4222 and projection 4224, described fluting 4220 is positioned at the both sides of described press section 4222 so that described press section 4222 has elasticity, and described projection 4224 is protruding to described fuselage 10 and be contained in described clasp groove 36 from described press section 4222.
In the present embodiment, press section 4222 is roughly L shaped and forms endways a press surface, is beneficial to press.
Because of 4220 both sides that are positioned at press section 4222 of slotting, thereby press section 4222 has certain elasticity.In the time luggage carrier 40 need being installed on to fuselage 10, pressing described press section 4222 so that described holding part 422 can slide on diapire 324, thereby described guide rail 4202 is slipped in described guide groove 34, to reach the object that luggage carrier 40 is fixed on to fuselage 10; When needs by luggage carrier 40 when fuselage 10 is dismantled, press described press section 4222 so that described projection 4224 departs from described clasp groove 36, thereby described guide rail 4202 can be skidded off to described guide groove 34, to reach the object from fuselage 10 dismountings by luggage carrier 40.
In a kind of optional embodiment, described fixing-holding rack 42 also comprises the first support 425 and the second support 427, described rail portion 420 and described holding part 422 are convexly set in described the first support 425, and described fixing arm 44 deviates from described fuselage 10 from described the second support 427 and protrudes.
In a kind of optional embodiment, described fixing-holding rack 42 also comprises a plurality of feets 429, described feet 429 be individually fixed in described the first support 425 with described the second support 427 to be fixedly connected with described the first support 425 and described the second support 427.
Please refer to Fig. 3 to Fig. 6, in a kind of optional embodiment, described the first support 425 is provided with a plurality of the first stent foots 4250, described the second support 427 is provided with a plurality of the second stent foots 4270, and described in each, feet 429 is individually fixed in described in each the first stent foot 4250 and the second stent foot 4270 described in each.
Particularly, described the first stent foot 4250 extends to four corners from the body of the first support 425 respectively, thereby has alleviated the weight of the first support 425; Described the second stent foot 4270 extends to four corners from the body of the second support 427 respectively, thereby alleviated the weight of the second support 427, alleviate the weight of described fixing-holding rack 42, and then alleviated the weight of positive aircraft, be conducive to aircraft towards the trend of light and handy future development.
In a kind of optional embodiment, described in each, the first stent foot 4250 is provided with the first holding hole (not label), described in each, the second stent foot 4270 is provided with the second holding hole (not label), and described in each, feet 429 is individually fixed in described in each the first holding hole and described in each in the second holding hole.
In the present embodiment, described feet 429 is made by damping material, as quality of rubber materials, for reducing vibrations, transmits, and for reducing the vibration of fuselage 10 generations, passes to by loading 200.
Further, because described fixing-holding rack 42 of the present utility model comprises the first support 425 and the second support 427, and the described feet 429 with cushioning effect is set between the first support 425 and the second support 427, thereby the vibration that fuselage 10 produces, as the vibration that driving engine produces, be difficult for passing to by loading 200 by fixing-holding rack 42.
Particularly, for the described rail portion 420 of luggage carrier 40 fixed main body 10 and described holding part 422 are convexly set in to described the first support 425, installation is protruded from the second support 427 by the described fixing arm 44 of loading 200, and between the first support 425 and the second support 427, be provided with a plurality of described feets 429 with cushioning effect, thereby the vibration that fuselage 10 produces, as the vibration that driving engine produces, be difficult for passing to by loading 200 by fixing-holding rack 42, reduced by the vibration hazard of loading 200.
In a kind of optional embodiment, described luggage carrier device 20 comprises a pair of fixing arm 44, and described fixing arm 44 all deviates from described fuselage 10 protrusions from the bottom surface of described the second support 427.During installation, by loading 200, be installed between two fixing arms 44.
In other embodiments, also can only have a fixing arm 44, but fixing arm 44 is provided with a pair of retaining claw.During installation, by loading 200, be installed between two retaining claws.
In the present embodiment, by loading 200, be photographic equipment.
In a kind of optional embodiment, described fixing-holding rack 42 comprises the limiting section 424 that is convexly set in described the first support 425, and described limiting section 424 is against described rear wall 322.Because the utlity model has limiting section 424, when described rail portion 420 is contained in to described accepting hole 326, the excessive slip of described guide rail 4202 in guide groove 34 be can prevent, thereby the projection 4224 of described holding part 422 and the location between described clasp groove 36 guaranteed.
In other embodiments, can there is no limiting section 424 yet.
Please refer to Fig. 1 to Fig. 6, during installation, described rail portion 420 is contained in described accepting hole 326 and described guide rail 4202 is slipped in described guide groove 34, and the projection 4224 that makes described holding part 422 snaps in described clasp groove 36, thereby luggage carrier device 20 is fixed on to latch part 30, is about to luggage carrier 40 and is fixed on fuselage 10; During dismounting, press described press section 4222 and make projection 4224 depart from clasp grooves 36, and make the described guide rail 4202 described guide groove 34 that slips away, just can, by luggage carrier 40 from described latch part 30 dismountings, be about to luggage carrier 40 from described fuselage 10 dismountings; Be luggage carrier device 20 of the present utility model in the process of Assembly &Disassembly, all do not need use instrument, greatly improve the comfort feature of Assembly &Disassembly, thereby improved the comfort feature using.
The above is preferred implementation of the present utility model; it should be pointed out that for those skilled in the art, do not departing under the prerequisite of the utility model principle; can also make some improvements and modifications, these improvements and modifications are also considered as protection domain of the present utility model.
Claims (10)
1. a luggage carrier device, be installed on the fuselage of aircraft, it is characterized in that, described luggage carrier device comprises latch part and luggage carrier, described latch part is arranged at described fuselage and comprises resettlement section, a pair of guide groove and clasp groove, the front opening of described resettlement section also comprises pair of sidewalls, rear wall, diapire and accepting hole, described rear wall connects described sidewall, described guide groove is arranged at described sidewall, described accepting hole is by described sidewall, described rear wall and described diapire surround, described clasp groove is arranged at diapire close described opening, described luggage carrier comprises fixing-holding rack and at least one fixing arm, described fixing arm deviates from described fuselage protrusion from the bottom surface of described fixing-holding rack, described fixing-holding rack comprises rail portion and the holding part that is convexly set in described fixing-holding rack end face, the shape of described rail portion is consistent with the shape of described accepting hole and comprise pair of guide rails, described rail portion is contained in described accepting hole, described guide rail slips in described guide groove, described holding part has certain elasticity and part is contained in described clasp groove, so that described luggage carrier is fixed on to described latch part.
2. luggage carrier device as claimed in claim 1, is characterized in that, the framed structure that described rail portion is cuboid, and described guide rail extends in opposite directions from a pair of relative sidewall.
3. luggage carrier device as claimed in claim 1, it is characterized in that, described holding part comprises a cross-notching, press section and projection, described fluting is positioned at the both sides of described press section so that described press section has elasticity, and described projection is protruding to described fuselage and be contained in described clasp groove from described press section.
4. luggage carrier device as claimed in claim 1, is characterized in that, described fixing-holding rack comprises the first support and the second support, and described rail portion and described holding part are convexly set in described the first support, and described fixing arm deviates from described fuselage from described the second support and protrudes.
5. luggage carrier device as claimed in claim 4, is characterized in that, described fixing-holding rack also comprises a plurality of feets, described feet be individually fixed in described the first support with described the second support to be fixedly connected with described the first support and described the second support.
6. luggage carrier device as claimed in claim 5, it is characterized in that, described the first support is provided with a plurality of the first stent foots, and described the second support is provided with a plurality of the second stent foots, and described in each, feet is individually fixed in described in each the first stent foot and the second stent foot described in each.
7. luggage carrier device as claimed in claim 6, it is characterized in that, described in each, the first stent foot is provided with the first holding hole, described in each, the second stent foot is provided with the second holding hole, and described in each, feet is individually fixed in described in each the first holding hole and described in each in the second holding hole.
8. luggage carrier device as claimed in claim 4, is characterized in that, described luggage carrier device comprises a pair of fixing arm, and described fixing arm all deviates from described fuselage protrusion from the bottom surface of described the second support.
9. luggage carrier device as claimed in claim 4, is characterized in that, described fixing-holding rack comprises the limiting section that is convexly set in described the first support, and described limiting section support is by described rear wall.
10. an aircraft, comprises fuselage, it is characterized in that, described aircraft also comprises the luggage carrier device as described in claim 1-9 any one that is installed on described fuselage.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420350901.9U CN203937864U (en) | 2014-06-26 | 2014-06-26 | Luggage carrier device and aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420350901.9U CN203937864U (en) | 2014-06-26 | 2014-06-26 | Luggage carrier device and aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203937864U true CN203937864U (en) | 2014-11-12 |
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ID=51857203
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420350901.9U Active CN203937864U (en) | 2014-06-26 | 2014-06-26 | Luggage carrier device and aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203937864U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107355455A (en) * | 2017-07-27 | 2017-11-17 | 顺丰科技有限公司 | One kind carrying lock and locking, unlocking method |
-
2014
- 2014-06-26 CN CN201420350901.9U patent/CN203937864U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107355455A (en) * | 2017-07-27 | 2017-11-17 | 顺丰科技有限公司 | One kind carrying lock and locking, unlocking method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |