CN104309564A - Vehicular turbine jet engine protecting system - Google Patents

Vehicular turbine jet engine protecting system Download PDF

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Publication number
CN104309564A
CN104309564A CN201410574735.5A CN201410574735A CN104309564A CN 104309564 A CN104309564 A CN 104309564A CN 201410574735 A CN201410574735 A CN 201410574735A CN 104309564 A CN104309564 A CN 104309564A
Authority
CN
China
Prior art keywords
turbine
turbojet
control system
automobile
jet pipe
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
Application number
CN201410574735.5A
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Chinese (zh)
Inventor
陈恒兰
黄立丽
蒋科化
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to CN201410574735.5A priority Critical patent/CN104309564A/en
Publication of CN104309564A publication Critical patent/CN104309564A/en
Pending legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60RVEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR
    • B60R21/00Arrangements or fittings on vehicles for protecting or preventing injuries to occupants or pedestrians in case of accidents or other traffic risks
    • B60R21/01Electrical circuits for triggering passive safety arrangements, e.g. airbags, safety belt tighteners, in case of vehicle accidents or impending vehicle accidents
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60RVEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR
    • B60R21/00Arrangements or fittings on vehicles for protecting or preventing injuries to occupants or pedestrians in case of accidents or other traffic risks
    • B60R2021/0002Type of accident

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

The invention provides a vehicular turbine jet engine protecting system with a protecting function. The vehicular turbine jet engine protecting system comprises an air incoming way 1, an air compressor 2, a control system 3, a combustion chamber 4, a turbine 5 and a tail jet pipe 6. The vehicular turbine jet engine protecting system is characterized in that the air incoming way 1 is connected with the air compressor 2 which is connected with the combustion chamber 4, the control system 3 is connected with a vehicle cab control system and connected with the air incoming way 2 through a lead, the combustion chamber 4 is connected with the turbine 5 which is connected with the tail jet pipe 6, and a nozzle of the tail jet pipe 6 is perpendicular to the ground. The vehicular turbine jet engine protecting system has the protecting function, can prevent a current vehicle from being impacted by vehicles ahead or behind at the same time and is high in safety coefficient and high in thrust.

Description

Automobile-used turbojet protective system
Technical field
The present invention relates to a kind of turbojet security protection system with safeguard function for vehicle.
Background technology
In recent years relating in patent documentation for protecting in security technology that vehicle is knocked, not applying turbojet protective system and being knocked to avoid vehicle.The application number announced as Chinese patent information center is the utility model patent of 201020274946.4---four kinds of vehicle retrorockets and newtype brake system, the patent provides a kind of four kinds of vehicle retrorockets and newtype brake system, relate to Rail car manufacture and jet propulsion technology, provide single constituent element and double elements two kinds of liquid rockets, solid-rocket, Gu-liquid hybrid rocket, and the brake system that this four kinds of rockets form respectively, when needs emergency braking, retrorocket is started immediately, and within the time of per centum second, make rapid reaction, the high temperature and high pressure gas that rocket propellant fast burn produces, from jet pipe ejection at a high speed, breaks into powerful thrust, balances out car body acquired force of inertia in advancing, shorten " tyre skid ", cut down traffic accidents, improve vehicle safety performance, be applicable to various visitor, lorry, is especially applicable to the various vehicles needing long-distance running and travel on hill path, as transcontinental coach, truck, cross-country car, rolling cart, motor bike, battery-driven car, hybrid electric vehicle, special vehicle, various car, pick up, racing car, agricultural tricycle, agricultural four-wheel etc.But this application mainly applies to full size vehicle, be only limited to drag function.
Summary of the invention
For the deficiencies in the prior art, the invention provides a kind of automobile-used turbojet protective system, may be used for protecting the Vehicular impact that this vehicle is avoided by the vehicle in front or rear, or avoid this vehicle to be clashed into by the vehicle of front and back two side simultaneously.
Its technical scheme is: a kind of automobile-used turbojet protective system with safeguard function, comprise inlet channel 1, air compressor 2, control system 3, combustion chamber 4, turbine 5, jet pipe 6, it is characterized in that: described inlet channel 1 connects air compressor 2, described air compressor 2 connects combustion chamber 4, described control system 3 connects vehicle cab control system and has wire to connect inlet channel 1, described combustion chamber 4 connects turbine 5, described turbine 5 connects jet pipe 6, and described jet pipe 6 spout becomes vertical direction with ground.
As optimization, a kind of automobile-used turbojet protective system with safeguard function of the present invention, is characterized in that: described automobile-used turbojet protective system is arranged on vehicle bottom.
As optimization, a kind of automobile-used turbojet protective system with safeguard function of the present invention, is characterized in that: described jet pipe 6 has 4.
As optimization, a kind of automobile-used turbojet protective system with safeguard function of the present invention, it is characterized in that: also installing parachute 7 additional at roof has a wire connection control system 3, parachute has makes vehicle in the buffer action fallen by safety and stability after having sprayed.
As optimization, a kind of automobile-used turbojet protective system with safeguard function of the present invention, is characterized in that: described parachute 7 is arranged on roof.
Principle of work of the present invention: 1, when finding in traveling way that there is this vehicle of vehicle strike at front or rear, chaufeur starts control system 3 of the present invention in time, air is entered by inlet channel 1, pressurizeed by air compressor 2, heated by combustion chamber 4, accelerated by turbine 5, discharged by jet pipe 6 and produce thrust, this vehicle is raised more than 2-3 rice by the ground reaction force produced, and avoids by the Vehicular impact at front or rear and causes safety misadventure; 2, after this vehicle raises by ground reaction force, chaufeur releases a parachute 7 by control system, allows the gently stable landing of this vehicle.
Advantage of the present invention: 1, have safeguard function, can avoid this vehicle by the Vehicular impact at vehicle front or rear, solves prior art and lacks the safety problem that this vehicle of protection knocked into the back by Vehicular impact and vehicle pileup below; 2, safety factor is higher, and this vehicle can be avoided to be clashed into simultaneously by the vehicle at vehicle front and rear; 3, thrust ratio is more powerful.Turbojet application jet propulsion avoids rocket and the intrinsic weakness of athodyd.Because have employed turbo-driven air compressor, so driving engine also has enough pressure to produce powerful thrust when low speed.
Accompanying drawing explanation
Fig. 1 is structural representation of the present invention.
In figure: inlet channel 1, air compressor 2, control system 3, combustion chamber 4, turbine 5, jet pipe 6, parachute 7.
Detailed description of the invention
Below embodiments of the invention are described in detail by reference to the accompanying drawings.
embodiment 1:as shown in Figure 1, a kind of automobile-used turbojet protective system with safeguard function, comprise inlet channel 1, air compressor 2, control system 3, combustion chamber 4, turbine 5, jet pipe 6, it is characterized in that: described inlet channel 1 connects air compressor 2, described air compressor 2 connects combustion chamber 4, described control system 3 connects vehicle cab control system and has wire to connect inlet channel 1, described combustion chamber 4 connects turbine 5, described turbine 5 connects jet pipe 6, described jet pipe 6 spout becomes vertical direction with ground, described automobile-used turbojet protective system is arranged on vehicle bottom.
embodiment 2:a kind of automobile-used turbojet protective system with safeguard function, comprise inlet channel 1, air compressor 2, control system 3, combustion chamber 4, turbine 5, jet pipe 6, parachute 7, it is characterized in that: described inlet channel 1 connects air compressor 2, described air compressor 2 connects combustion chamber 4, described control system 3 connects vehicle cab control system and has wire to connect inlet channel 1, described combustion chamber 4 connects turbine 5, described turbine 5 connects jet pipe 6, described jet pipe 6 spout becomes vertical direction with ground, and described parachute 7 is arranged on roof and has wire connection control system 3.

Claims (5)

1. one kind has the automobile-used turbojet protective system of safeguard function, comprise inlet channel (1), air compressor (2), control system (3), combustion chamber (4), turbine (5), jet pipe (6), it is characterized in that: described inlet channel (1) connects air compressor (2), described air compressor (2) connects combustion chamber (4), described control system (3) connects vehicle cab control system and has wire to connect inlet channel (1), described combustion chamber (4) connects turbine (5), described turbine (5) connects jet pipe (6), described jet pipe (6) spout becomes vertical direction with ground.
2. there is the automobile-used turbojet protective system of safeguard function according to claim 1, it is characterized in that: described automobile-used turbojet protective system is arranged on vehicle bottom.
3. there is the automobile-used turbojet protective system of safeguard function according to claim 1, it is characterized in that: described jet pipe (6) has 4.
4. there is the automobile-used turbojet protective system of safeguard function according to claim 1, it is characterized in that: also install parachute (7) additional and have wire connection control system (3).
5. there is the automobile-used turbojet protective system of safeguard function according to claim 4, it is characterized in that: described parachute (7) is arranged on roof.
CN201410574735.5A 2014-10-25 2014-10-25 Vehicular turbine jet engine protecting system Pending CN104309564A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410574735.5A CN104309564A (en) 2014-10-25 2014-10-25 Vehicular turbine jet engine protecting system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410574735.5A CN104309564A (en) 2014-10-25 2014-10-25 Vehicular turbine jet engine protecting system

Publications (1)

Publication Number Publication Date
CN104309564A true CN104309564A (en) 2015-01-28

Family

ID=52364934

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410574735.5A Pending CN104309564A (en) 2014-10-25 2014-10-25 Vehicular turbine jet engine protecting system

Country Status (1)

Country Link
CN (1) CN104309564A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115285083A (en) * 2022-09-26 2022-11-04 苏州亚太精睿传动科技股份有限公司 Vehicle braking system and vehicle braking method

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2685174Y (en) * 2004-02-24 2005-03-16 龚小刚 Vehicle emergency braking and anticollision apparatus
CN102616096A (en) * 2012-04-24 2012-08-01 赵辉 Solar flying automobile with folding wings
CN103407573A (en) * 2013-06-09 2013-11-27 丁飞 Vertical take-off and landing jet-propelled disc-shaped aircraft

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2685174Y (en) * 2004-02-24 2005-03-16 龚小刚 Vehicle emergency braking and anticollision apparatus
CN102616096A (en) * 2012-04-24 2012-08-01 赵辉 Solar flying automobile with folding wings
CN103407573A (en) * 2013-06-09 2013-11-27 丁飞 Vertical take-off and landing jet-propelled disc-shaped aircraft

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115285083A (en) * 2022-09-26 2022-11-04 苏州亚太精睿传动科技股份有限公司 Vehicle braking system and vehicle braking method

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PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C02 Deemed withdrawal of patent application after publication (patent law 2001)
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20150128