CN209063829U - Automobile aerocraft - Google Patents
Automobile aerocraft Download PDFInfo
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- CN209063829U CN209063829U CN201821063016.7U CN201821063016U CN209063829U CN 209063829 U CN209063829 U CN 209063829U CN 201821063016 U CN201821063016 U CN 201821063016U CN 209063829 U CN209063829 U CN 209063829U
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- parachute
- vehicle body
- elastic component
- automobile aerocraft
- automobile
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Abstract
The utility model provides a kind of automobile aerocraft, is related to the technical field of the vehicles, and automobile aerocraft includes vehicle body and two parachute assemblies；Two parachute assemblies are oppositely arranged on the two sides of vehicle body respectively；The parachute assembly includes ejection mechanism, trigger mechanism and parachute；The receiving storehouse for accommodating the parachute and the ejection mechanism is provided on the vehicle body；The opening for accommodating storehouse is provided with cover board, and the cover board is for covering or exposing the opening；The ejection mechanism is connect with the parachute and the trigger mechanism respectively；The trigger mechanism is mobile to expose opening for controlling the cover board, and controls the ejection mechanism and the parachute is removed the receiving storehouse.The setting of the parachute assembly of the automobile aerocraft can provide time progress emergent management and be saved oneself for user, and can cut down impact force when vehicle body collides on ground, to improve the safety of automobile aerocraft.
Description
Technical field
The utility model relates to technical field of transportation means, more particularly, to a kind of automobile aerocraft.
Background technique
Traffic and means of transport of the automobile as a kind of modern society, there is irreplaceable work in present society
With.However, our road also becomes increasingly congestion can't bear as the development of society, automobile increase.It therefore, is understanding
The certainly above problem, more and more producers begin to focus on hovercar.
In the prior art, hovercar is mainly fixed-wing takeoff hovercar.In use, fixed-wing
Takeoff flight vapour is along going to give it the gun, and when driving to certain speed, the lower section air pressure of fixed-wing is greater than the gas of top
Pressure, provides lift by the upper and lower air pressure difference.
But when hovercar runs out of steam in the sky, lapse rate is too fast, and hovercar is easy to cause to crash, prestige
Coerce the life security of driver.
Utility model content
The purpose of this utility model is to provide a kind of automobile aerocrafts, existing in the prior art when flight vapour to improve
When vehicle runs out of steam in the sky, lapse rate is too fast, and hovercar is easy to cause to crash, and threatens the skill of the life security of driver
Art problem.
Automobile aerocraft provided by the utility model, including vehicle body and two parachute assemblies；Two parachute assemblies point
It is not oppositely arranged on the two sides of vehicle body.
Further, parachute assembly includes ejection mechanism, trigger mechanism and parachute；It is provided on vehicle body for holding
Receive the receiving storehouse of parachute and ejection mechanism；The opening for accommodating storehouse is provided with cover board, and cover board is for covering or exposing opening；
Ejection mechanism is connect with parachute and trigger mechanism respectively；Trigger mechanism is mobile to expose opening for controlling cover board, and controls
Parachute is removed and accommodates storehouse by ejection mechanism.
Further, parachute includes extractor parachute, main chute and connecting rope；Connecting rope connects with extractor parachute and main chute respectively
It connects, main chute is connect with vehicle body；Ejection mechanism, which is used to remove extractor parachute, accommodates storehouse.
Further, ejection mechanism includes guiding piece, guide part, elastic component, traction rope and fixing piece；Traction rope difference
It is connect with guiding piece and extractor parachute；One end of elastic component is abutted with vehicle body, and fixing piece is for enabling elastic component be in compressive state；Touching
Hair mechanism is for removing fixing piece, to enable extending direction pop-up of the elastic component by guiding piece along guide part accommodate storehouse.
Further, guide part is guide cylinder；Elastic component and guiding piece are arranged at the inside of guide cylinder, and elastic component edge is led
It is arranged to the extending direction of cylinder.
Further, fixing piece is fixed pin；The through-hole for wearing fixed pin is provided on guide cylinder；Fixed pin and elastic component
It abuts, and the one end of elastic component far from vehicle body is arranged in fixed pin.
Further, trigger mechanism includes triggering handle.
Further, the front-end and back-end of vehicle body are respectively arranged with parachute assembly.
Further, floatage air bag mechanism and control handle are provided on vehicle body；It controls handle and floatage air bag mechanism connects
It connects, control handle is for controlling the starting of floatage air bag mechanism.
Further, the lower end of vehicle body is arranged in the air bag of floatage air bag mechanism.
Automobile aerocraft provided by the utility model, when automobile aerocraft runs out of steam in the sky, vehicle body can rapidly under
Pendant, at this moment user starts parachute assembly, and due to air drag principle, the parachute relative atmospheric of parachute assembly is moved
It is inflating expanded, slow down vehicle body lapse rate.
The setting of the parachute assembly of the automobile aerocraft can provide time progress emergent management and oneself for user
It rescues, and impact force when vehicle body collides on ground can be cut down, to improve the safety of automobile aerocraft.
Detailed description of the invention
It, below will be right in order to illustrate more clearly of specific embodiment of the present invention or technical solution in the prior art
Specific embodiment or attached drawing needed to be used in the description of the prior art are briefly described, it should be apparent that, it is described below
In attached drawing be that some embodiments of the utility model are not paying creativeness for those of ordinary skill in the art
Under the premise of labour, it is also possible to obtain other drawings based on these drawings.
Structural schematic diagram when Fig. 1 is the parachute assembly starting of automobile aerocraft provided by the embodiment of the utility model；
Top view when Fig. 2 is the parachute assembly starting of automobile aerocraft provided by the embodiment of the utility model；
Fig. 3 is the structural representation when parachute assembly of automobile aerocraft provided by the embodiment of the utility model is inactive
Figure；
Fig. 4 is the top view when parachute assembly of automobile aerocraft provided by the embodiment of the utility model is inactive；
Fig. 5 is the structural schematic diagram of ejection mechanism provided by the embodiment of the utility model.
Icon: 1- vehicle body；2- parachute assembly；3- parachute；4- ejection mechanism；5- accommodates storehouse；6- cover board；7- wing；
301- main chute；302- extractor parachute；303- connecting rope；401- guiding piece；402- guide part；403- elastic component；404- traction rope；
405- fixing piece.
Specific embodiment
The technical solution of the utility model is clearly and completely described below in conjunction with attached drawing, it is clear that described
Embodiment is the utility model a part of the embodiment, instead of all the embodiments.Based on the embodiments of the present invention, originally
Field those of ordinary skill every other embodiment obtained without making creative work belongs to practical
Novel protected range.
In the description of the present invention, it should be noted that such as occur term " center ", "upper", "lower", " left side ",
" right side ", "vertical", "horizontal", "inner", "outside" etc., indicated by orientation or positional relationship be orientation based on the figure or
Positional relationship is merely for convenience of describing the present invention and simplifying the description, rather than the device or member of indication or suggestion meaning
Part must have a particular orientation, be constructed and operated in a specific orientation, therefore should not be understood as limiting the present invention.
In addition, such as there is term " first ", " second ", " third " are used for description purposes only, be not understood to indicate or imply opposite
Importance.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " is pacified
Dress ", " connected ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or integrally
Connection；It can be mechanical connection, be also possible to be electrically connected；Can be directly connected, can also indirectly connected through an intermediary,
It can be the connection inside two elements.For the ordinary skill in the art, above-mentioned art can be understood with concrete condition
The concrete meaning of language in the present invention.
Structural schematic diagram when Fig. 1 is the parachute assembly starting of automobile aerocraft provided by the embodiment of the utility model；
Top view when Fig. 2 is the parachute assembly starting of automobile aerocraft provided by the embodiment of the utility model；Fig. 3 is that this is practical new
The structural schematic diagram when parachute assembly for the automobile aerocraft that type embodiment provides is inactive；Fig. 4 is the utility model implementation
The top view when parachute assembly for the automobile aerocraft that example provides is inactive；As shown in Figure 1, Figure 2, shown in Fig. 3 and Fig. 4, this reality
The automobile aerocraft of example offer, including vehicle body 1 and two parachute assemblies 2 are provided；Two parachute assemblies 2 are oppositely arranged on respectively
The two sides of vehicle body 1.
Automobile aerocraft provided in this embodiment, when automobile aerocraft runs out of steam in the sky, under the meeting rapidly of vehicle body 1
Pendant, at this moment user starts parachute assembly 2, due to air drag principle, 3 relative atmospheric of parachute of parachute assembly 2
It moves inflating expanded, slows down 1 lapse rate of vehicle body.
The setting of the parachute assembly 2 of the automobile aerocraft can provide time progress emergent management and oneself for user
It rescues, and impact force when vehicle body 1 collides on ground can be cut down, to improve the safety of automobile aerocraft.
Fig. 5 is the structural schematic diagram of ejection mechanism provided by the embodiment of the utility model；As shown in Figure 1, Figure 2, Fig. 3, Fig. 4 and
Shown in Fig. 5, on the basis of the above embodiments, further, parachute assembly 2 includes ejection mechanism 4, trigger mechanism and drop
Fall umbrella 3；The receiving storehouse 5 for accommodating parachute 3 and ejection mechanism 4 is provided on vehicle body 1；The opening for accommodating storehouse 5 is provided with
Cover board 6, cover board 6 is for covering or exposing opening；Ejection mechanism 4 is connect with parachute 3 and trigger mechanism respectively；Trigger mechanism
It is mobile to expose opening for controlling cover board 6, and control ejection mechanism 4 and parachute 3 is removed into receiving storehouse 5.
Wherein, the middle part of 1 side of vehicle body should be arranged in opening, in this way when two parachutes 3 pop up, can enable vehicle body 1
It is more stable.
The two sides of vehicle body 1 are also relatively set with wing 7, and opening should be arranged in the top of wing 7, work as parachute assembly in this way
When 2 starting, parachute 3 will not generate interference, the damage for preventing wing 7 and parachute 3 from being impacted by the two with wing 7.
Ejection mechanism 4 may include cylinder and push rod, and push rod is arranged between cylinder and parachute 3, trigger mechanism and gas
Cylinder connection.In use, user controls cover board 6 by trigger mechanism and opens to expose opening, then controls cylinder band
Dynamic push rod, which releases parachute 3, accommodates storehouse 5, and the movement of 3 relative atmospheric of parachute is inflating expanded, to slow down 1 lapse rate of vehicle body.
Trigger mechanism may include trigger button, and trigger button can be to be electrically connected with ejection mechanism 4.
Cover board 6 and vehicle body 1 are rotatablely connected by rotating bar, and one end of rotating bar and the power output shaft of driving motor connect
It connects, trigger mechanism is connect with driving motor.In use, trigger mechanism control driving motor starting, driving motor move
Power output shaft is rotated to drive rotating bar to rotate, to drive the rotation of cover board 6 to expose opening.
In the present embodiment, in use, in automobile aerocraft normally travel or flight, parachute 3 is located at
It accommodates in storehouse 5；When automobile aerocraft is fallen at high speeds, user controls the movement of cover board 6 by operation trigger mechanism to expose
Opening, then trigger mechanism control ejection mechanism 4, which removes parachute 3, accommodates storehouse 5, and 3 relative atmospheric of parachute moves inflation exhibition
It opens, to slow down 1 lapse rate of vehicle body, and then improves the safety of automobile aerocraft.The setting for accommodating storehouse 5 and cover board 6 can
Play the role of protect parachute 3, and can also prevent parachute 3 without using when error starting, hinder automobile aerocraft
Normal use.
As depicted in figs. 1 and 2, on the basis of the above embodiments, further, parachute 3 includes extractor parachute 302, master
Umbrella 301 and connecting rope 303；Connecting rope 303 is connect with extractor parachute 302 and main chute 301 respectively, and main chute 301 is connect with vehicle body 1；
Ejection mechanism 4, which is used to remove extractor parachute 302, accommodates storehouse 5.
Wherein, connecting rope 303 can be wirerope.
Main chute 301 can be connect with vehicle body 1 by wirerope.
In the present embodiment, in use, when automobile aerocraft runs out of steam in the sky, user passes through operation touching
Hair mechanism controls cover board 6 is mobile to expose opening, and then trigger mechanism control ejection mechanism 4, which removes extractor parachute 302, accommodates storehouse
5, the movement of 302 relative atmospheric of extractor parachute is inflating expanded, thus taken main chute 301 out of from receiving storehouse 5 by connecting rope 303, it is main
The movement of 301 relative atmospheric of umbrella is inflating expanded, to slow down 1 lapse rate of vehicle body, and then improves the safety of automobile aerocraft.By
It is larger in the volume and weight of main chute 301, main chute 301 is removed into receiving storehouse 5 and needs biggish external force, the setting of extractor parachute 302
The active force to parachute 3 of ejection mechanism 4 can be reduced, extractor parachute 302 need to only be removed and accommodate storehouse 5 by ejection mechanism 4, then
It pulls main chute 301 to remove to the active force of extractor parachute 302 by air to accommodate storehouse 5, can reduce setting for ejection mechanism 4 in this way
It is set to this, and the stability used is higher.
As shown in figure 5, on the basis of the above embodiments, further, ejection mechanism 4 includes guiding piece 401, guide part
402, elastic component 403, traction rope 404 and fixing piece 405；Traction rope 404 is connect with guiding piece 401 and extractor parachute 302 respectively；
One end of elastic component 403 is abutted with vehicle body 1, and fixing piece 405 is for enabling elastic component 403 be in compressive state；Trigger mechanism is used for
Fixing piece 405 is removed, to enable extending direction pop-up of the elastic component 403 by guiding piece 401 along guide part 402 accommodate storehouse 5.
Wherein, guide part 402 can be guide rod, be provided with guiding groove, elastic component 403, fixing piece 405 on guide rod
And guiding piece 401 is arranged in guiding groove, extending direction setting of the elastic component 403 along guiding groove.In use process
In, after removing fixing piece 405, elastic component 403 is resetted from compressive state, and elastic component 403 generates and guiding groove extending direction
Guiding piece 401 is moved to along the extending direction of guiding groove and accommodates outside storehouse 5 by identical elastic force, the elastic force.
Elastic component 403 can be spring or elastic rubber etc..
Traction rope 404 can be wirerope.
Fixing piece 405 can be plate, when elastic component 403 is when in a compressed state, one end of elastic component 403 and vehicle body 1
It abuts, the other end is abutted with plate.
The elastic force that the weight and elastic component 403 of guiding piece 401 reset should accommodate storehouse 5 can guarantee that extractor parachute 302 removes
Subject to.
Elastic component 403 can be to be bolted, be clamped or Nian Jie etc. with vehicle body 1.
In the present embodiment, in use, when automobile aerocraft is fallen at high speeds, user passes through operation triggering machine
Structure control cover board 6 is mobile to expose opening, and then trigger mechanism control removes fixing piece 405, after fixing piece 405 removes, bullet
Property part 403 from compressive state reset, elastic component 403 generate elastic force by guiding piece 401 along guide part 402 extending direction pop up
Storehouse 5 is accommodated, guiding piece 401 drives extractor parachute 302 to remove and accommodates storehouse 5 by traction rope 404.The setting of guide part 402 can limit
Determine the pop-up path of guiding piece 401, it is ensured that guiding piece 401 can pop up accommodate storehouse 5, and the setting of above-mentioned elastic mechanism at
This lower, high stability.
As shown in figure 5, on the basis of the above embodiments, further, guide part 402 is guide cylinder；403 He of elastic component
Guiding piece 401 is arranged at the inside of guide cylinder, and elastic component 403 is arranged along the extending direction of guide cylinder.
Preferably, guiding piece 401 is spherical in shape, its frictional force between guide cylinder can be reduced in this way, its language is enabled to go out to lead
To cylinder speed faster.
In the present embodiment, in use, the setting of guide cylinder can enable reset path and the guiding piece of elastic component 403
401 movement routine is more accurate, to improve the Stability and veracity of operation.
As shown in figure 5, on the basis of the above embodiments, further, fixing piece 405 is fixed pin；It is set on guide cylinder
It is equipped with the through-hole for wearing fixed pin；Fixed pin is abutted with elastic component 403, and elastic component 403 is arranged in far from vehicle body 1 in fixed pin
One end.Trigger mechanism includes triggering handle.
Wherein, automobile aerocraft may include hydraulic cylinder, and one end of hydraulic cylinder and one end of fixed pin connect.Trigger mechanism
It can extend or shorten by electric-controlled hydraulic cylinder, so that fixed pin be driven to extract out from through-hole.
The cockpit of vehicle body 1 should be arranged in triggering handle, with convenient for users in case of emergency capable of quickly touching
Encounter.
It, in use, can be with elastic component 403 far from vehicle body 1 when fixed pin is inserted into through-hole in the present embodiment
One end abuts, so that elastic component 403 be enabled to be in compressive state, removes through-hole when user controls fixed pin by triggering handle
When, fixed pin is separated with elastic component 403, and the setup cost of fixed pin is lower, and occupied space is smaller, and operate stability compared with
It is high.
As shown in Figure 1, Figure 2, shown in Fig. 3 and Fig. 4, on the basis of the above embodiments, further, the front end of vehicle body 1 and
Rear end is respectively arranged with parachute assembly 2.
Wherein, starter is provided on vehicle body 1, starter can control multiple parachute assemblies 2 while start, to guarantee
The stationarity of automobile aerocraft tenesmus；User can also control according to the actual situation starts one or more parachute assembly
2。
The parachute 3 of 1 front and back of vehicle body should open simultaneously or the parachute 3 of 1 two sides of vehicle body should be opened simultaneously, such energy
Enough guarantee the stationarity of automobile aerocraft tenesmus.
In the present embodiment, in use, user can start the landing of 1 front-end and back-end of vehicle body according to the actual situation
Umbrella device 2, to slow down lapse rate.
On the basis of the above embodiments, further, floatage air bag mechanism and control handle are provided on vehicle body 1；Control
Handle processed is connect with floatage air bag mechanism, and control handle is for controlling the starting of floatage air bag mechanism.
Wherein, floatage air bag mechanism may include multiple air bags, and multiple air bags can be oppositely arranged on 1 two sides of vehicle body.
In the present embodiment, in use, user controls the starting of floatage air bag mechanism, buoyancy gas by control handle
Capsule mechanism can provide buoyancy for vehicle body 1, slow down the lapse rate of automobile aerocraft, to further increase automobile aerocraft
Safety.
On the basis of the above embodiments, further, the lower end of vehicle body 1 is arranged in the air bag of floatage air bag mechanism.
In the present embodiment, the lower end of vehicle body 1 is arranged in air bag, and during the tenesmus of automobile aerocraft, air bag can be risen
To the effect for slowing down lapse rate；When automobile aerocraft falls to ground, air bag can prevent car body directly and ground generation
It hits, plays explosion-proof；In addition, air bag can also play buoyancy when automobile aerocraft falls on the water surface, vehicle is enabled
Body 1 floats on the surface.
Finally, it should be noted that the above various embodiments is only to illustrate the technical solution of the utility model, rather than it is limited
System；Although the present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art should
Understand: it is still possible to modify the technical solutions described in the foregoing embodiments, or to some or all of
Technical characteristic is equivalently replaced；And these are modified or replaceed, it does not separate the essence of the corresponding technical solution, and this is practical new
The range of each embodiment technical solution of type.
Claims (9)
1. a kind of automobile aerocraft characterized by comprising vehicle body and two parachute assemblies；
Two parachute assemblies are oppositely arranged on the two sides of the vehicle body respectively；
The parachute assembly includes ejection mechanism, trigger mechanism and parachute；
The receiving storehouse for accommodating the parachute and the ejection mechanism is provided on the vehicle body；The opening for accommodating storehouse
Place is provided with cover board, and the cover board is for covering or exposing the opening；
The ejection mechanism is connect with the parachute and the trigger mechanism respectively；The trigger mechanism is for controlling the lid
Plate is mobile to expose opening, and controls the ejection mechanism and the parachute is removed the receiving storehouse.
2. automobile aerocraft according to claim 1, which is characterized in that the parachute include extractor parachute, main chute and
Connecting rope；
The connecting rope is connect with the extractor parachute and the main chute respectively, and the main chute is connect with the vehicle body；The ejection
Mechanism is used to the extractor parachute removing the receiving storehouse.
3. automobile aerocraft according to claim 2, which is characterized in that the ejection mechanism include guiding piece, guide part,
Elastic component, traction rope and fixing piece；
The traction rope is connect with the guiding piece and the extractor parachute respectively；One end of the elastic component is supported with the vehicle body
It connects, the fixing piece is for enabling the elastic component be in compressive state；The trigger mechanism is for removing fixing piece, described in enabling
Extending direction of the elastic component by the guiding piece along the guide part pops up the receiving storehouse.
4. automobile aerocraft according to claim 3, which is characterized in that the guide part is guide cylinder；
The elastic component and the guiding piece are arranged at the inside of the guide cylinder, and the elastic component prolongs along the guide cylinder
Stretch direction setting.
5. automobile aerocraft according to claim 4, which is characterized in that the fixing piece is fixed pin；
The through-hole for wearing the fixed pin is provided on the guide cylinder；The fixed pin is abutted with the elastic component, and described
The one end of the elastic component far from the vehicle body is arranged in fixed pin.
6. automobile aerocraft according to claim 1, which is characterized in that the trigger mechanism includes triggering handle.
7. automobile aerocraft according to claim 1-6, which is characterized in that the front-end and back-end of the vehicle body point
It is not provided with the parachute assembly.
8. automobile aerocraft according to claim 1, which is characterized in that be provided on the vehicle body floatage air bag mechanism and
Control handle；
The control handle is connect with the floatage air bag mechanism, and the control handle is opened for controlling the floatage air bag mechanism
It is dynamic.
9. automobile aerocraft according to claim 8, which is characterized in that the air bag of the floatage air bag mechanism is arranged in institute
State the lower end of vehicle body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821063016.7U CN209063829U (en) | 2018-07-04 | 2018-07-04 | Automobile aerocraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821063016.7U CN209063829U (en) | 2018-07-04 | 2018-07-04 | Automobile aerocraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209063829U true CN209063829U (en) | 2019-07-05 |
Family
ID=67089273
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821063016.7U Active CN209063829U (en) | 2018-07-04 | 2018-07-04 | Automobile aerocraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209063829U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108891217A (en) * | 2018-07-04 | 2018-11-27 | 天津超算科技有限公司 | Automobile aerocraft |
| CN112109925A (en) * | 2020-05-12 | 2020-12-22 | 北京凌空天行科技有限责任公司 | Parachute connection mechanism of aerospace vehicle |
| CN113492687A (en) * | 2020-04-07 | 2021-10-12 | 中国航天科工飞航技术研究院（中国航天海鹰机电技术研究院） | Magnetic suspension sledge ejection device |
-
2018
- 2018-07-04 CN CN201821063016.7U patent/CN209063829U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108891217A (en) * | 2018-07-04 | 2018-11-27 | 天津超算科技有限公司 | Automobile aerocraft |
| CN113492687A (en) * | 2020-04-07 | 2021-10-12 | 中国航天科工飞航技术研究院（中国航天海鹰机电技术研究院） | Magnetic suspension sledge ejection device |
| CN112109925A (en) * | 2020-05-12 | 2020-12-22 | 北京凌空天行科技有限责任公司 | Parachute connection mechanism of aerospace vehicle |
| CN112109925B (en) * | 2020-05-12 | 2021-12-07 | 北京凌空天行科技有限责任公司 | Parachute connection mechanism of aerospace vehicle |
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