CN102230456A - Atmosphere breathing type laser engine device - Google Patents

Atmosphere breathing type laser engine device Download PDF

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Publication number
CN102230456A
CN102230456A CN2011101692769A CN201110169276A CN102230456A CN 102230456 A CN102230456 A CN 102230456A CN 2011101692769 A CN2011101692769 A CN 2011101692769A CN 201110169276 A CN201110169276 A CN 201110169276A CN 102230456 A CN102230456 A CN 102230456A
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CN
China
Prior art keywords
piston
laser
lasers
fanjing
dan
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CN2011101692769A
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Chinese (zh)
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CN102230456B (en
Inventor
张永康
戴峰泽
管海兵
钱晓明
姜银方
张朝阳
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Jiangsu University
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Jiangsu University
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Priority to CN2011101692769A priority Critical patent/CN102230456B/en
Publication of CN102230456A publication Critical patent/CN102230456A/en
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Publication of CN102230456B publication Critical patent/CN102230456B/en
Expired - Fee Related legal-status Critical Current
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02GHOT GAS OR COMBUSTION-PRODUCT POSITIVE-DISPLACEMENT ENGINE PLANTS; USE OF WASTE HEAT OF COMBUSTION ENGINES; NOT OTHERWISE PROVIDED FOR
    • F02G1/00Hot gas positive-displacement engine plants
    • F02G1/04Hot gas positive-displacement engine plants of closed-cycle type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02GHOT GAS OR COMBUSTION-PRODUCT POSITIVE-DISPLACEMENT ENGINE PLANTS; USE OF WASTE HEAT OF COMBUSTION ENGINES; NOT OTHERWISE PROVIDED FOR
    • F02G2254/00Heat inputs

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Laser Beam Processing (AREA)
  • Lasers (AREA)

Abstract

The invention relates to an atmosphere breathing type laser engine device which is mainly used for the field needing remote energy source transmission. The atmosphere breathing type laser engine device disclosed by the invention comprises a high-energy laser system, a control system and an engine system, wherein the high-energy laser system outputs a parallel laser beam; after focused through the parabolic reflecting surface of a piston, the parallel laser beam and air mutually act to form a plasma explosion impact wave for pushing the piston to axially move; the control system is used for controlling the normal opening and closing state of a high-energy laser generation device; and all assemblies of the engine system are used for converting the axial movement of the piston into the rotating movement of a crankshaft to output power.

Description

Atmosphere respiration type laser engine device
Technical field
The present invention relates to motor and remote-wireless energy transmission field, refer in particular to the photic puncture that superlaser and air interaction after utilize focusing on cause, the plasma explosive blast of formation as thrust keep engine running the laser engine device.
Background technique
Conventional engines uses fuel owing to necessary, so its use is subjected to the restriction of fuel.For example aircraft or rocket, the consumption of its fuel is very huge, greatly reduces the load of these launch vehicles.And conventional engines is under lowpressure or oxygen-free environment, can't proper functioning.And the burning of fuel can give off a large amount of harmful gases, is unfavorable for environmental protection.A Kantrowitz [A.Kantrowitz.Propulsion to orbit by ground-based lasers[J] .Astronautics and Aeronautics in 1974,1972,10 (5): 74-76 has proposed to utilize the laser Push Technology to launch the notion of grapefruit satellite, its principle is that propulsion system is installed on grapefruit satellite, the core work parts of this propulsion system are one or one group of parabolic, parabolic is used for focusing on the laser beam from ground, make near the air generation plasma blast of focus, thereby reflective surface is formed a deboost.Done a large amount of fundamental researchs about a lot of researchers afterwards, utilized various types of lasers as the energy about laser propelling aspect.When adopting pulse laser as the energy, the effect of laser beam and working medium can produce very big instantaneous acceleration, its running is not steady, and very difficult controlling party to, and such propulsion system can only produce along the axial reaction thrust of parabolic, so its application can be very limited.Domestic Zhou Xinlong has declared a kind of laser power motor patent, the patent No.: 99206057 in 1999.The principle of this utility model patent is that the air that utilizes laser to light in the firing chamber forms negative pressure, does manual work thereby promote piston by atmospheric pressure.Can at first, form vacuum behind the laser combustion air and yet there are no report both at home and abroad, secondly, the thrust of utilizing barometric pressure to produce be big inadequately concerning motor.People such as Hua Yinqun have declared a kind of no fuel laser engine patent in 2004, the patent No.: 200410014435, its principle is to utilize the high energy pulse laser exposure at working medium, makes the working medium plasma, and the plasma blast forms shock wave and promotes the piston acting.
In existing technology, the technology drawback of its existence is:
(1) adopt collimated laser beam, because laser beam does not focus on, produce the plasma detonation wave, its specific power must be enough big;
(2) working medium is sealed in the firing chamber, working medium can be recycled, because the plasma temperature that the laser emission working medium produces is high to the material requirement of its firing chamber up to 20000k;
(3) pulse laser work can only be adopted, continuous laser work can not be adopted;
(4) adopt the contact-type electronic push-button switch to control laser, to guarantee the proper functioning of motor, control the working state of laser owing to adopt the lead mode, therefore, can't realize remote or high-altitude transmission laser energy, not bring into play the advantage of laser as a kind of outstanding remote transmission energy.
Summary of the invention
The purpose of this invention is to provide a kind of motor that utilizes plasma explosive blast that superlaser after the focusing and air interact and form as thrust.
This motor is by the superlaser generator, and sensing system and connecting rod etc. partly constitute.High energy laser beam is after piston end surface focuses on, interact with air, form the plasma explosive blast, generation is to the deboost of piston end surface, pass through connecting rod, the rotation that the axial motion of piston is converted into bent axle makes piston produce axial rotation, thus output torque, and sensing system is used for guaranteeing the lasting high-efficient operation of motor.
In order to realize that piston end surface is designed to parabolic with high energy collimated laser beam reflect focalization.
The collimated laser beam that the high energy laser generator sends is focused on by the parabolic of piston, makes near the air breakdown of focus, produces the plasma explosive blast, thereby reacts on piston face, and piston is formed deboost.The laser that the high energy pulse laser generator sends can be Long Pulse LASER, also can be short-pulse laser.
Nozzle is arranged at a side of cylinder wall, and the effect of nozzle is to make to maintain air in certain amount in the cylinder, and is used for cooling off cylinder.
To start function to continue high-efficient operation in order making, must to guarantee piston when working stroke, the high energy laser generator is in opening state; And when piston returned, laser was in closed condition.The sensing system of being made up of He-Ne Lasers sensor and reflector group is controlled the working state of superlaser generator.The reflector group is installed on the bent axle, is made up of two anti-mirrors and Dan Fanjing, and reflective surface of two anti-mirrors and the reflective surface of Dan Fanjing are in same plane.The He-Ne Lasers sensor can be launched two bundle He-Ne Lasers, and its distance is greater than the width of two anti-mirrors and Dan Fanjing, causes to guarantee two bundle He-Ne Lasers can not be radiated at simultaneously on the same reflector and sends the erroneous trigger signal.When piston was in top dead center, the reflection direction of reflective surface of two anti-mirrors and the reflective surface of Dan Fanjing all pointed to the He-Ne Lasers sensor, and this moment, sensing system received two bundle reflected light, opened the high energy pulse generating device of laser; When lower dead center is arrived in piston motion, the reflection direction of another reflective surface of two anti-mirrors points to the He-Ne Lasers sensor, and the non-reflecting surface of Dan Fanjing reflector laser not, at this moment, sensing system sends pulse signal for the high energy laser generating means, and the high energy laser generating means stops to launch laser.So circulation, thus make motor can continue high-efficient operation.
Advantage of the present invention is:
1) no need of any fuel as long as air is arranged in environment, can run well under anoxic or environment under low pressure equally, and environment is not had any pollution;
2) end thrust can be converted to the thrust of any direction by this motor, and can make the running of motor steady;
3) engine device separates with laser beam emitting device, and its separating distance can reach tens kilometers even hundreds of kilometer, can at a distance laser energy be converted into engine power.;
4) engine device is simple in structure, greatly simplified manufacturing technique.
Description of drawings
Fig. 1 is the structural representation that the present invention is based on the two stroke engine of laser blast wave.
Among the figure, 1: high energy laser generator, 2: high energy laser beam, 3: nozzle, 4: piston, 5: cylinder, 6: connecting rod, 7: bent axle, 8: two anti-mirrors, 9: Dan Fanjing, 10: helium neon laser beam, 11: the He-Ne Lasers sensor.
Embodiment
The embodiment that proposes below in conjunction with description of drawings the present invention, but be not used for limiting the present invention.
Its working procedure is as follows: at first, nozzle 3 blows air in cylinder 5, sensing system is in running order, bent axle 7 is rotated, drive piston 4 and do axial motion, when piston 4 moves to top dead center, the normal direction of reflective surface of two anti-mirrors 8 and the reflective surface of Dan Fanjing 9 is all pointed to the He-Ne Lasers sensor, this moments two, bundle He-Ne Lasers 10 were radiated at respectively on the reflective surface of reflective surface of two anti-mirrors 8 and Dan Fanjing 9, sensing system is received two bundle reflected light, send a trigger signal and give high energy laser generator 1 this moment, open high energy laser generator 1, high energy laser generator 1 is launched high energy laser beam 2, after the parabolic type reflect focalization face of piston 4 focuses on, with near the air breakdown its focus, form the plasma explosive blast, promoting piston 4 moves vertically, by piston 4, cylinder 5, the connecting rod that connecting rod 6 and bent axle 7 are formed, the axial motion of piston 4 is converted to the rotation of bent axle 7, output torque, when piston 4 moved to lower dead center, two anti-mirrors 8 and Dan Fanjing 9 just turned over 180 degree, another reflective surface reflection He-Ne Lasers 10 of two anti-mirrors 8, and He-Ne Lasers is not reflected at the back side of Dan Fanjing 9, this moment, sensing system was received a branch of reflected light, and send a pulse signal and close high energy laser generator 1 this moment, and this stage relies on rotator inertia, when piston 4 arrives top dead center again, continue next shuttling movement, so repeat, realize the lasting high-efficient operation of motor.

Claims (2)

1. atmosphere respiration type laser engine device, it is characterized in that, comprise high energy pulse laser generator (1), nozzle (3), piston (4), cylinder (5), connecting rod (6), bent axle (7), two anti-mirror (8), Dan Fanjing (9) and He-Ne Lasers sensor (11); The end face of described piston (4) is a parabolic, and the parabolic type that the collimated laser beam that described high energy pulse generating device of laser (1) sends is aimed at piston (4) focuses on curved surface; Described nozzle (3) is arranged at the interior spray of a side direction cylinder (5) air of cylinder (5) wall; Described piston (4), cylinder (5), connecting rod (6) and bent axle (7) are formed connecting rod, and the end face that piston (4) points to laser one side is the parabolic type focal surface; Described two anti-mirror (8) and Dan Fanjing (9) are installed on the bent axle, described two anti-mirror (8) is a double mirror, Dan Fanjing (9) is the single face reflector, reflective surface of described two anti-mirrors (8) and the reflective surface of Dan Fanjing (9) are in same plane, when piston is positioned at top dead center, the reflection direction of the reflective surface of (8) reflective surface of two anti-mirrors and Dan Fanjing (9) points to He-Ne Lasers sensor (11), the two bundle He-Ne Lasers that He-Ne Lasers sensor (11) sends point to two anti-mirrors (8) and Dan Fanjing (9) respectively, when piston was positioned at lower dead center, the reflection direction of another reflective surface of two anti-mirrors (8) pointed to He-Ne Lasers sensor (11); The two bundle He-Ne Lasers distances that He-Ne Lasers sensor (11) sends are greater than the width of two anti-mirrors, and He-Ne Lasers sensor (11) is connected by datawire with high energy pulse laser generator (1).
2. atmosphere respiration type laser engine device according to claim 1 is characterized in that the laser that described high energy pulse laser generator (1) sends is Long Pulse LASER or short-pulse laser.
CN2011101692769A 2011-06-22 2011-06-22 Atmosphere breathing type laser engine device Expired - Fee Related CN102230456B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2011101692769A CN102230456B (en) 2011-06-22 2011-06-22 Atmosphere breathing type laser engine device

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Application Number Priority Date Filing Date Title
CN2011101692769A CN102230456B (en) 2011-06-22 2011-06-22 Atmosphere breathing type laser engine device

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CN102230456B CN102230456B (en) 2013-05-08

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102767497A (en) * 2012-05-22 2012-11-07 北京卫星环境工程研究所 Fuel-free spacecraft propelling system based on spatial atomic oxygen and propelling method
CN102797656A (en) * 2012-08-03 2012-11-28 北京卫星环境工程研究所 Air breathing type helicon wave electric propulsion device
CN113062838A (en) * 2021-04-30 2021-07-02 中国科学院力学研究所 Laser preionization enhanced air suction device and method for air suction electric propulsion technology
US11767828B2 (en) 2023-03-27 2023-09-26 Daniel L. Amend Light turbine, turbine, and turbine housing for vane evaluation

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5420437A (en) * 1994-01-11 1995-05-30 Siess; Harold E. Method and apparatus for generation and implantation of ions
CN2400591Y (en) * 1999-03-21 2000-10-11 周新龙 Laser power engine
DE10061673A1 (en) * 2000-12-12 2002-06-13 Volkswagen Ag Engine spark plug element for coupling energy into volume filled with defined medium has electrode with end region with elongated, mutually separated electrode sections, each coupled to electrode connection
CN1563712A (en) * 2004-03-25 2005-01-12 江苏大学 Fuelless laser engine
CN102022299A (en) * 2010-12-07 2011-04-20 中国人民解放军国防科学技术大学 Laser microthruster

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5420437A (en) * 1994-01-11 1995-05-30 Siess; Harold E. Method and apparatus for generation and implantation of ions
CN2400591Y (en) * 1999-03-21 2000-10-11 周新龙 Laser power engine
DE10061673A1 (en) * 2000-12-12 2002-06-13 Volkswagen Ag Engine spark plug element for coupling energy into volume filled with defined medium has electrode with end region with elongated, mutually separated electrode sections, each coupled to electrode connection
CN1563712A (en) * 2004-03-25 2005-01-12 江苏大学 Fuelless laser engine
CN102022299A (en) * 2010-12-07 2011-04-20 中国人民解放军国防科学技术大学 Laser microthruster

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102767497A (en) * 2012-05-22 2012-11-07 北京卫星环境工程研究所 Fuel-free spacecraft propelling system based on spatial atomic oxygen and propelling method
CN102767497B (en) * 2012-05-22 2014-06-18 北京卫星环境工程研究所 Fuel-free spacecraft propelling system based on spatial atomic oxygen and propelling method
CN102797656A (en) * 2012-08-03 2012-11-28 北京卫星环境工程研究所 Air breathing type helicon wave electric propulsion device
CN102797656B (en) * 2012-08-03 2014-08-13 北京卫星环境工程研究所 Air breathing type helicon wave electric propulsion device
CN113062838A (en) * 2021-04-30 2021-07-02 中国科学院力学研究所 Laser preionization enhanced air suction device and method for air suction electric propulsion technology
CN113062838B (en) * 2021-04-30 2024-05-03 中国科学院力学研究所 Laser preionization enhanced air suction device and method for air suction electric pushing technology
US11767828B2 (en) 2023-03-27 2023-09-26 Daniel L. Amend Light turbine, turbine, and turbine housing for vane evaluation

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Inventor after: Dai Fengze

Inventor after: Zhang Yongkang

Inventor after: Guan Haibing

Inventor after: Qian Xiaoming

Inventor after: Jiang Yinfang

Inventor after: Zhang Chaoyang

Inventor before: Zhang Yongkang

Inventor before: Dai Fengze

Inventor before: Guan Haibing

Inventor before: Qian Xiaoming

Inventor before: Jiang Yinfang

Inventor before: Zhang Chaoyang

COR Change of bibliographic data

Free format text: CORRECT: INVENTOR; FROM: ZHANG YONGKANG DAI FENGZE GUAN HAIBING QIAN XIAOMING JIANG YINFANG ZHANG ZHAOYANG TO: DAI FENGZE ZHANG YONGKANG GUAN HAIBING QIAN XIAOMING JIANG YINFANG ZHANG ZHAOYANG

CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20130508

Termination date: 20150622

EXPY Termination of patent right or utility model