CN108482042A - It is a kind of be used for three dwell airplane mode switching mechanism - Google Patents
It is a kind of be used for three dwell airplane mode switching mechanism Download PDFInfo
- Publication number
- CN108482042A CN108482042A CN201810435092.4A CN201810435092A CN108482042A CN 108482042 A CN108482042 A CN 108482042A CN 201810435092 A CN201810435092 A CN 201810435092A CN 108482042 A CN108482042 A CN 108482042A
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- gear
- fixed
- hinged
- knucle
- motor
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- 230000007246 mechanism Effects 0.000 title claims abstract description 19
- 230000005611 electricity Effects 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 11
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 4
- 230000000694 effects Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60F—VEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
- B60F5/00—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media
- B60F5/02—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media convertible into aircraft
Abstract
The invention discloses it is a kind of be used for three dwell airplane mode switching mechanism, stepper motor is provided in fuselage body, stepper motor is connected with leading screw, and slide plate is provided on leading screw, connecting plate one is hinged on slide plate, connecting plate one is hinged with connecting plate two, connecting plate two is hinged with connecting plate three, and connecting plate three is fixed with upper connecting rod, and one end of upper connecting rod is hinged on fuselage body, the other end is hinged in connecting rod fixed mount, and connecting rod fixed mount is fixed on bearing；Lower link is also hinged on fuselage body, the other end of lower link is hinged on by fixing axle in connecting rod fixed mount, and fixing axle is fixed on lower link, and one end of fixing axle is provided with bevel gear one, bevel gear one is engaged with bevel gear two, and bevel gear two is connected with Knucle-gear one by two connecting shaft of bevel gear；Knucle-gear one is engaged with Knucle-gear two, and Knucle-gear two connects axis connection motor rack by Knucle-gear two.The invention has the advantages that simple in structure, three switchings for dwelling aircraft Three models may be implemented.
Description
Technical field
It dwells vehicle technology field the present invention relates to three, more specifically, being related to a kind of cutting for three airplane modes of dwelling
The mechanism changed.
Background technology
Three aircraft of dwelling can not only fly in the air, but also can on the way walk, and can also move about in water, be a kind of new
The three of type are dwelt flight equipment.It is existing be used for three dwell airplane mode switching mechanism it is complex, both increase aircraft
Weight, and improve production cost.
Therefore, in view of the above, invention is a kind of simple in structure, using effect is good to be used for three airplane modes of dwelling and cuts
The mechanism changed is those skilled in the art's problem to be solved.
Invention content
In order to overcome the technical drawbacks described above, the present invention provide it is a kind of be used for three dwell airplane mode switching mechanism.
To achieve the above object, the present invention uses following technical scheme：
A kind of to be used for three mechanisms for dwelling airplane mode switching, including fuselage body is provided with step in the fuselage body
Stepper motor is connected with leading screw on the output shaft of stepper motor, slide plate is provided on leading screw, connecting plate one is hinged on slide plate, even
Fishplate bar one is hinged with connecting plate two, and connecting plate two is hinged with connecting plate three, and connecting plate three is fixed with upper connecting rod, one end of upper connecting rod
It is hinged on fuselage body, the other end is hinged in connecting rod fixed mount, and connecting rod fixed mount is fixed on bearing；The fuselage body
On be also hinged with lower link, the other end of lower link is hinged on by fixing axle in connecting rod fixed mount, and fixing axle is fixed on lower company
On bar, one end of fixing axle is provided with bevel gear one, and bevel gear one is engaged with bevel gear two, and bevel gear two is connected by bevel gear two
Spindle is connected with Knucle-gear one, and wherein two connecting shaft of bevel gear passes through bearing, bevel gear two to be arranged in the outside of bearing, Knucle-gear
One is arranged in the inside of bearing；The Knucle-gear one is engaged with Knucle-gear two, and Knucle-gear two connects axis connection by Knucle-gear two
Motor rack, two one end of the connecting shaft of Knucle-gear are fixed on bearing, and the other end is fixed on motor rack；The both ends of the motor rack are solid
Surely there is fixed column, fixing sleeve is set in fixed column, motor rack is connected with baffle, two fixing sleeves and gear by baffle link block
Plate cooperation is fixed with wheel, and the inner ring of wheel is provided with ring gear, wherein the fixed outside for being set on wheel, baffle plate setting exist
The inside of wheel；It is further fixed on flight motor, land motor and gear set fixing axle on the motor rack, wherein flight motor
It is provided with blade on output shaft, gear set is wherein provided in gear set fixing axle, is arranged on the output shaft of land motor with teeth
Wheel, gear are engaged by gear set with ring gear.
Further, 4 groups of connecting plates one are hinged with simultaneously on the slide plate.
Further, the bearing and motor rack are coaxially connected by two connecting shaft of Knucle-gear.
Further, gear set protection board is provided on the outside of the gear set, gear set protection board is fixed on gear set
In fixing axle.
Further, opened up on the baffle link block it is fluted, ring gear be arranged in groove.
The beneficial effects of the invention are as follows：Simple in structure, using effect is good, it may be convenient to realize that three dwell three kinds of aircraft
The switching of pattern.
Description of the drawings
Fig. 1 be it is of the present invention it is a kind of be used for three dwell airplane mode switching mechanism structural schematic diagram；
Fig. 2 is the partial enlarged view at Figure 1A；
Fig. 3 be it is of the present invention it is a kind of be used for three dwell airplane mode switching mechanism partial structural diagram one；
Fig. 4 be it is of the present invention it is a kind of be used for three dwell airplane mode switching mechanism partial structural diagram two；
Fig. 5 is the partial enlarged view at Fig. 4 B；
Fig. 6 be it is of the present invention it is a kind of be used for three dwell airplane mode switching mechanism partial structural diagram three；
Fig. 7 is the partial enlarged view at Fig. 6 C；
Fig. 8 is the connection diagram of fuselage body and bearing；
Fig. 9 is the structural schematic diagram of motor rack of the present invention；
Figure 10 is the connection diagram of motor rack and wheel；
Figure 11 is the partial enlarged view at Figure 10 D；
Figure 12 be it is of the present invention it is a kind of be used for three dwell airplane mode switching mechanism partial structural diagram four；
Figure 13 is the schematic diagram of present apparatus offline mode；
Figure 14 is the schematic diagram of present apparatus land pattern；
Figure 15 is the schematic diagram of present apparatus marine mode；
In figure, 1, fuselage body；2, stepper motor；3, leading screw；4, slide plate；5, connecting plate one；6, connecting plate two；7, it connects
Plate three；8, upper connecting rod；9, lower link；10, fixing axle；11, connecting rod fixed mount；12, bearing；13, bevel gear one；14, bevel gear
Two；15, two connecting shaft of bevel gear；16, Knucle-gear one；17, Knucle-gear two；18, two connecting shaft of Knucle-gear；19, motor rack；20、
Fixed column；21, baffle；22, flight motor；23, land motor；24, blade；25, gear set fixing axle；26, gear set；27、
Wheel；28, ring gear；29, gear set protection board；30, baffle link block；31, fixing sleeve.
Specific implementation mode
The present invention is specifically described below in conjunction with the accompanying drawings, it is a kind of to dwell aircraft mould for three according to shown in Fig. 1-15
The mechanism of formula switching, including fuselage body 1, stepper motor 2 is provided in fuselage body 1, is connected on the output shaft of stepper motor 2
It is connected to leading screw 3, slide plate 4 is provided on leading screw 3, connecting plate 1 is hinged on slide plate 4, connecting plate 1 is hinged with connecting plate 26,
Connecting plate 26 is hinged with connecting plate 37, and connecting plate 37 is fixed with upper connecting rod 8, and one end of upper connecting rod 8 is hinged on fuselage body 1
On, the other end is hinged in connecting rod fixed mount 11, and connecting rod fixed mount 11 is fixed on bearing 12；It is also hinged on fuselage body 1
There are lower link 9, the other end of lower link 9 to be hinged in connecting rod fixed mount 11 by fixing axle 10, fixing axle 10 is fixed on lower company
On bar 9, one end of fixing axle 10 is provided with bevel gear 1, and bevel gear 1 is engaged with bevel gear 2 14, and bevel gear 2 14 is logical
It crosses two connecting shaft 15 of bevel gear and is connected with Knucle-gear 1, wherein two connecting shaft 15 of bevel gear passes through bearing 12, bevel gear 2 14
It is arranged in the outside of bearing 12, Knucle-gear 1 is arranged in the inside of bearing 12；Knucle-gear 1 is engaged with Knucle-gear 2 17, circle
Gear 2 17 connects motor rack 19 by two connecting shaft 18 of Knucle-gear, and two connecting shaft of Knucle-gear, 18 one end is fixed on bearing 12,
The other end is fixed on motor rack 19；It is fixed with fixed column 20 at the both ends of motor rack 19, fixing sleeve is set in fixed column 20
31, motor rack 19 is connected with baffle 21 by baffle link block 30, and two fixing sleeves 31 and the cooperation of baffle 21 are fixed with wheel 27,
The inner ring of wheel 27 is provided with ring gear 28, and wherein fixing sleeve 31 is arranged in the outside of wheel 27, and baffle 21 is arranged in wheel 27
Inside；Flight motor 22, land motor 23 and gear set fixing axle 25, wherein flight motor are further fixed on motor rack 19
It is provided with blade 24 on 22 output shaft, gear set 26, the output of land motor 23 are wherein provided in gear set fixing axle 25
Gear is provided on axis, gear is engaged by gear set 26 with ring gear 28；
It is hinged with 4 groups of connecting plates 1 simultaneously on its middle slide plate 4；
Wherein bearing 12 and motor rack 19 are coaxially connected by two connecting shaft 18 of Knucle-gear；
The outside of wherein gear set 26 is provided with gear set protection board 29, and gear set protection board 29 is fixed on gear set and fixes
On axis 25；
Wherein opened up on baffle link block 30 it is fluted, ring gear 28 be arranged in groove.
In the present embodiment, stepper motor 2 drives leading screw 3 to rotate, and leading screw 3 drives slide plate 4 to slide up and down, and slide plate 4 is logical
Crossing connecting plate 1, connecting plate 26 and connecting plate 37 drives upper connecting rod 8 and lower link 9 to move, and lower link 9 can be around bearing 12
Movement, lower link 9 can be rotated by fixing axle 10 with dynamic bevel gear 1, and bevel gear 1 can pass through bevel gear 2 14, cone tooth
It takes turns two connecting shafts 15 and Knucle-gear 1 drives Knucle-gear 2 17 to rotate, Knucle-gear 2 17 can pass through two connecting shaft of Knucle-gear, 18 band
Dynamic motor rack 19 moves, and so that motor rack 19 is switched to different three with motor car wheel 27 and dwells pattern.
When in land pattern, land motor 23 rotates, after land motor 23 is slowed down by gear set 26, with wheel 27
Ring gear 28 be meshed, and then with motor car wheel 27 rotate.
When in offline mode, the rotation of flight motor 22 drives blade 24 to rotate, and completes flight.
When in marine mode, fuselage body 1 is suspended in the water surface, and flight motor 22 is higher than the water surface, 22 band of flight motor
Dynamic blade 24 rotates rearward air draft, and driving aircraft moves on the water surface.
Above-mentioned technical proposal only embodies the optimal technical scheme of technical solution of the present invention, those skilled in the art
The principle of the present invention is embodied to some variations that some of which part may be made, belongs to the scope of protection of the present invention it
It is interior.
Claims (5)
1. a kind of being used for three mechanisms for dwelling airplane mode switching, including fuselage body (1), it is characterised in that：The fuselage sheet
It is provided with stepper motor (2) in body (1), leading screw (3) is connected on the output shaft of stepper motor (2), leading screw is provided with cunning on (3)
Plate (4) is hinged with connecting plate one (5) on slide plate (4), and connecting plate one (5) is hinged with connecting plate two (6), and connecting plate two (6) is hinged
There are connecting plate three (7), connecting plate three (7) to be fixed with upper connecting rod (8), one end of upper connecting rod (8) is hinged on fuselage body (1),
The other end is hinged in connecting rod fixed mount (11), and connecting rod fixed mount (11) is fixed on bearing (12)；On the fuselage body (1)
It is also hinged with lower link (9), the other end of lower link (9) is hinged on by fixing axle (10) in connecting rod fixed mount (11), fixed
Axis (10) is fixed on lower link (9), and one end of fixing axle (10) is provided with bevel gear one (13), and bevel gear one (13) is engaged with
Bevel gear two (14), bevel gear two (14) are connected with Knucle-gear one (16), wherein bevel gear by two connecting shaft of bevel gear (15)
Two connecting shafts (15) pass through bearing (12), bevel gear two (14) setting to exist in the outside of bearing (12), Knucle-gear one (16) setting
The inside of bearing (12)；The Knucle-gear one (16) is engaged with Knucle-gear two (17), and Knucle-gear two (17) is connected by Knucle-gear two
Spindle (18) connects motor rack (19), and two connecting shaft of Knucle-gear (18) one end is fixed on bearing (12), and the other end is fixed on electricity
In rack (19)；The both ends of the motor rack (19) are fixed with fixed column (20), and fixing sleeve (31) is set in fixed column (20),
Motor rack (19) is connected with baffle (21) by baffle link block (30), and two fixing sleeves (31) and baffle (21) cooperation are fixed with
The inner ring of wheel (27), wheel (27) is provided with ring gear (28), and wherein fixing sleeve (31) setting is in the outside of wheel (27), gear
Plate (21) is arranged in the inside of wheel (27)；Flight motor (22), land motor (23) are further fixed on the motor rack (19)
With gear set fixing axle (25), wherein blade (24), wherein gear set fixing axle are provided on the output shaft of flight motor (22)
(25) be provided with gear set (26) on, be provided with gear on the output shaft of land motor (23), gear by gear set (26) with
Ring gear (28) engages.
2. it is according to claim 1 it is a kind of be used for three dwell airplane mode switching mechanism, it is characterised in that：The slide plate
(4) 4 groups of connecting plates one (5) are hinged with simultaneously on.
3. it is according to claim 1 it is a kind of be used for three dwell airplane mode switching mechanism, it is characterised in that：The bearing
(12) and motor rack (19) is coaxially connected by two connecting shaft of Knucle-gear (18).
4. it is according to claim 1 it is a kind of be used for three dwell airplane mode switching mechanism, it is characterised in that：The gear
Gear set protection board (29) is provided on the outside of group (26), gear set protection board (29) is fixed in gear set fixing axle (25).
5. it is according to claim 1 it is a kind of be used for three dwell airplane mode switching mechanism, it is characterised in that：The baffle
Opened up on link block (30) it is fluted, ring gear (28) be arranged in groove.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810435092.4A CN108482042A (en) | 2018-04-28 | 2018-04-28 | It is a kind of be used for three dwell airplane mode switching mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810435092.4A CN108482042A (en) | 2018-04-28 | 2018-04-28 | It is a kind of be used for three dwell airplane mode switching mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108482042A true CN108482042A (en) | 2018-09-04 |
Family
ID=63354258
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810435092.4A Pending CN108482042A (en) | 2018-04-28 | 2018-04-28 | It is a kind of be used for three dwell airplane mode switching mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108482042A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111070985A (en) * | 2019-12-30 | 2020-04-28 | 万勇 | Deformable unmanned aerial vehicle |
| US11772440B2 (en) * | 2018-06-04 | 2023-10-03 | Ali Salem | Multi-purpose wheels for use in multi-purpose vehicles |
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| CN101104376A (en) * | 2006-07-12 | 2008-01-16 | 许俊峰 | A flyable and roadable vehicle and its using method |
| CN103600631A (en) * | 2013-11-19 | 2014-02-26 | 浙江理工大学 | Amphibious wheel mechanism based on eccentric paddle mechanism |
| WO2014112894A1 (en) * | 2013-01-15 | 2014-07-24 | Kharitonov Dmitry Nikolaevich | Propulsion system for a hybrid (convertible) vehicle |
| CN208452724U (en) * | 2018-04-28 | 2019-02-01 | 河北工程大学 | It is a kind of for three dwell airplane mode switching mechanism |
-
2018
- 2018-04-28 CN CN201810435092.4A patent/CN108482042A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101104376A (en) * | 2006-07-12 | 2008-01-16 | 许俊峰 | A flyable and roadable vehicle and its using method |
| WO2014112894A1 (en) * | 2013-01-15 | 2014-07-24 | Kharitonov Dmitry Nikolaevich | Propulsion system for a hybrid (convertible) vehicle |
| CN103600631A (en) * | 2013-11-19 | 2014-02-26 | 浙江理工大学 | Amphibious wheel mechanism based on eccentric paddle mechanism |
| CN208452724U (en) * | 2018-04-28 | 2019-02-01 | 河北工程大学 | It is a kind of for three dwell airplane mode switching mechanism |
Non-Patent Citations (1)
| Title |
|---|
| 姜忠昱;: "一种海陆空三栖的多功能搜救器的设计", 中国战略新兴产业, no. 04, 28 January 2017 (2017-01-28), pages 67 - 70 * |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US11772440B2 (en) * | 2018-06-04 | 2023-10-03 | Ali Salem | Multi-purpose wheels for use in multi-purpose vehicles |
| CN111070985A (en) * | 2019-12-30 | 2020-04-28 | 万勇 | Deformable unmanned aerial vehicle |
| CN111070985B (en) * | 2019-12-30 | 2021-04-30 | 深圳康桥信息科技有限责任公司 | Deformable unmanned aerial vehicle |
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