CN108891217A - Automobile aerocraft - Google Patents
Automobile aerocraft Download PDFInfo
- Publication number
- CN108891217A CN108891217A CN201810733429.XA CN201810733429A CN108891217A CN 108891217 A CN108891217 A CN 108891217A CN 201810733429 A CN201810733429 A CN 201810733429A CN 108891217 A CN108891217 A CN 108891217A
- Authority
- CN
- China
- Prior art keywords
- parachute
- vehicle body
- elastic component
- automobile
- automobile aerocraft
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 230000000712 assembly Effects 0.000 claims abstract description 9
- 238000000429 assembly Methods 0.000 claims abstract description 9
- 238000010586 diagram Methods 0.000 description 6
- 206010057071 Rectal tenesmus Diseases 0.000 description 3
- 208000012271 tenesmus Diseases 0.000 description 3
- 238000000034 method Methods 0.000 description 2
- 239000007858 starting material Substances 0.000 description 2
- 239000002775 capsule Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D17/00—Parachutes
- B64D17/80—Parachutes in association with aircraft, e.g. for braking thereof
Abstract
The present invention provides a kind of automobile aerocrafts, are 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.When automobile aerocraft runs out of steam in the sky, vehicle body can rapidly drop, and at this moment user starts parachute assembly, and due to air drag principle, the parachute relative atmospheric movement of parachute assembly 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 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 present invention 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.
Summary of the invention
The purpose of the present invention is to provide a kind of automobile aerocrafts, existing in the prior art when hovercar exists to improve
When running out of steam in the air, lapse rate is too fast, and hovercar is easy to cause to crash, and the technology of the life security of driver is threatened to ask
Topic.
Automobile aerocraft provided by the invention, including vehicle body and two parachute assemblies；Two parachute assemblies distinguish phase
To the two sides that vehicle body is arranged in.
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 invention, when automobile aerocraft runs out of steam in the sky, vehicle body can rapidly drop, this
When user parachute assembly is started, due to air drag principle, the parachute relative atmospheric of parachute assembly moves inflation
Expansion, slows 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 to specific in order to illustrate more clearly of the specific embodiment of the invention or technical solution in the prior art
Embodiment or attached drawing needed to be used in the description of the prior art be briefly described, it should be apparent that, it is described below
Attached drawing is some embodiments of the present invention, for those of ordinary skill in the art, before not making the creative labor
It puts, 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 in an embodiment of the present invention；
Top view when Fig. 2 is the parachute assembly starting of automobile aerocraft provided in an embodiment of the present invention；
Fig. 3 is the structural schematic diagram when parachute assembly of automobile aerocraft provided in an embodiment of the present invention is inactive；
Fig. 4 is the top view when parachute assembly of automobile aerocraft provided in an embodiment of the present invention is inactive；
Fig. 5 is the structural schematic diagram of ejection mechanism provided in an embodiment of the present invention.
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
Technical solution of the present invention is clearly and completely described below in conjunction with attached drawing, it is clear that described implementation
Example is a part of the embodiment of the present invention, instead of all the embodiments.Based on the embodiments of the present invention, ordinary skill
Personnel's every other embodiment obtained without making creative work, shall fall within the protection scope of the present invention.
In the description of the present invention, it should be noted that such as occur term " center ", "upper", "lower", "left", "right",
"vertical", "horizontal", "inner", "outside" etc., indicated by orientation or positional relationship be orientation based on the figure or position
Relationship is merely for convenience of description of the present invention and simplification of the description, rather than the device or element of indication or suggestion meaning must have
There is specific orientation, be constructed and operated in a specific orientation, therefore is not considered as limiting the invention.In addition, as occurred
Term " first ", " second ", " third " are used for descriptive purposes only and cannot be understood as indicating or suggesting relative importance.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " installation ", " phase
Even ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or be integrally connected；It can
To be mechanical connection, it is also possible to be electrically connected；It can be directly connected, can also can be indirectly connected through an intermediary
Connection inside two elements.For the ordinary skill in the art, above-mentioned term can be understood at this with concrete condition
Concrete meaning in invention.
Structural schematic diagram when Fig. 1 is the parachute assembly starting of automobile aerocraft provided in an embodiment of the present invention；Fig. 2 is
Top view when the parachute assembly starting of automobile aerocraft provided in an embodiment of the present invention；Fig. 3 provides for the embodiment of the present invention
Automobile aerocraft parachute assembly it is inactive when structural schematic diagram；Fig. 4 is automobile provided in an embodiment of the present invention flight
The top view when parachute assembly of device is inactive；As shown in Figure 1, Figure 2, shown in Fig. 3 and Fig. 4, automobile provided in this embodiment flies
Row device, including vehicle body 1 and two parachute assemblies 2；Two parachute assemblies 2 are oppositely arranged on the two sides of vehicle body 1 respectively.
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 in an embodiment of the present invention；As shown in Figure 1, Figure 2, Fig. 3, Fig. 4 and Fig. 5
Shown, on the basis of the above embodiments, further, parachute assembly 2 includes ejection mechanism 4, trigger mechanism and landing
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 lid
Plate 6, cover board 6 is for covering or exposing opening；Ejection mechanism 4 is connect with parachute 3 and trigger mechanism respectively；Trigger mechanism is used
It is mobile to expose opening in control 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 embodiments are only used to illustrate the technical solution of the present invention., rather than its limitations；To the greatest extent
Present invention has been described in detail with reference to the aforementioned embodiments for pipe, those skilled in the art should understand that：Its according to
So be possible to modify the technical solutions described in the foregoing embodiments, or to some or all of the technical features into
Row equivalent replacement；And these are modified or replaceed, various embodiments of the present invention technology that it does not separate the essence of the corresponding technical solution
The range of scheme.
Claims (10)
1. a kind of automobile aerocraft, which is characterized in that including：Vehicle body and two parachute assemblies；
Two parachute assemblies are oppositely arranged on the two sides of the vehicle body respectively.
2. automobile aerocraft according to claim 1, which is characterized in that the parachute assembly includes ejection mechanism, touching
Send out 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.
3. automobile aerocraft according to claim 2, 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.
4. automobile aerocraft according to claim 3, 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.
5. automobile aerocraft according to claim 4, 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.
6. automobile aerocraft according to claim 5, 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.
7. automobile aerocraft according to claim 2, which is characterized in that the trigger mechanism includes triggering handle.
8. automobile aerocraft according to claim 1-7, which is characterized in that the front-end and back-end of the vehicle body point
It is not provided with the parachute assembly.
9. 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.
10. automobile aerocraft according to claim 9, which is characterized in that the air bag setting of the floatage air bag mechanism exists
The lower end of the vehicle body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810733429.XA CN108891217A (en) | 2018-07-04 | 2018-07-04 | Automobile aerocraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810733429.XA CN108891217A (en) | 2018-07-04 | 2018-07-04 | Automobile aerocraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108891217A true CN108891217A (en) | 2018-11-27 |
Family
ID=64347880
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810733429.XA Pending CN108891217A (en) | 2018-07-04 | 2018-07-04 | Automobile aerocraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108891217A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109823531A (en) * | 2019-03-13 | 2019-05-31 | 深圳市百川融创科技有限公司 | A kind of ejection recyclable device based on ram air parachute rope |
| CN111516629A (en) * | 2020-04-30 | 2020-08-11 | 江苏理工学院 | Automobile high-altitude falling emergency system and emergency method thereof |
| CN113200150A (en) * | 2021-06-18 | 2021-08-03 | 徐州质普智能设备有限公司 | High-ejection-take-off intelligent unmanned aerial vehicle |
| WO2024087315A1 (en) * | 2022-10-28 | 2024-05-02 | 广东汇天航空航天科技有限公司 | Flying automobile |
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| US5673873A (en) * | 1994-06-09 | 1997-10-07 | Stemme Gmbh & Co. Kg | Rescue system for aircraft |
| TW420622B (en) * | 1999-08-23 | 2001-02-01 | Fuji Ya Entpr Co Ltd | Lose-control safety device for remote controlled model flight vehicle |
| CN108177491A (en) * | 2018-01-08 | 2018-06-19 | 杨中震 | One kind can vertical take-off and landing flying car |
| CN209063829U (en) * | 2018-07-04 | 2019-07-05 | 天津超算科技有限公司 | Automobile aerocraft |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| US5673873A (en) * | 1994-06-09 | 1997-10-07 | Stemme Gmbh & Co. Kg | Rescue system for aircraft |
| CN1137982A (en) * | 1995-06-09 | 1996-12-18 | 王夜辉 | Flyable car |
| TW420622B (en) * | 1999-08-23 | 2001-02-01 | Fuji Ya Entpr Co Ltd | Lose-control safety device for remote controlled model flight vehicle |
| CN108177491A (en) * | 2018-01-08 | 2018-06-19 | 杨中震 | One kind can vertical take-off and landing flying car |
| CN209063829U (en) * | 2018-07-04 | 2019-07-05 | 天津超算科技有限公司 | Automobile aerocraft |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109823531A (en) * | 2019-03-13 | 2019-05-31 | 深圳市百川融创科技有限公司 | A kind of ejection recyclable device based on ram air parachute rope |
| CN109823531B (en) * | 2019-03-13 | 2023-12-29 | 深圳市百川融创科技有限公司 | Ejection recovery device based on punching parafoil rope |
| CN111516629A (en) * | 2020-04-30 | 2020-08-11 | 江苏理工学院 | Automobile high-altitude falling emergency system and emergency method thereof |
| CN113200150A (en) * | 2021-06-18 | 2021-08-03 | 徐州质普智能设备有限公司 | High-ejection-take-off intelligent unmanned aerial vehicle |
| WO2024087315A1 (en) * | 2022-10-28 | 2024-05-02 | 广东汇天航空航天科技有限公司 | Flying automobile |
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