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CN106184822A - Utilize the propulsion mode of Ampere force - Google Patents

Utilize the propulsion mode of Ampere force Download PDF

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Publication number
CN106184822A
CN106184822A CN201610268757.8A CN201610268757A CN106184822A CN 106184822 A CN106184822 A CN 106184822A CN 201610268757 A CN201610268757 A CN 201610268757A CN 106184822 A CN106184822 A CN 106184822A
Authority
CN
China
Prior art keywords
ampere force
propulsion mode
magnetic field
propulsion
utilize
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
CN201610268757.8A
Other languages
Chinese (zh)
Inventor
刘德智
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 CN201610268757.8A priority Critical patent/CN106184822A/en
Publication of CN106184822A publication Critical patent/CN106184822A/en
Pending legal-status Critical Current

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/402—Propellant tanks; Feeding propellants
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/407—Solar sailing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/408—Nuclear spacecraft propulsion
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/409—Unconventional spacecraft propulsion systems

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • High Energy & Nuclear Physics (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Shielding Devices Or Components To Electric Or Magnetic Fields (AREA)

Abstract

The present invention is to utilize the propulsion mode of Ampere force, is a kind of new propulsion mode.Jet-propulsion Technology Energy conversion efficiency of today is the lowest.This propulsion mode converts electrical energy into kinetic energy by Ampere force.Compared to jet-propulsion technology, the energy conversion efficiency of this device can reach 50% and more than.This propulsion mode can be used for rocket from now on, aircraft and spacecraft.

Description

Utilize the propulsion mode of Ampere force
Applicant: Liu Dezhi
Technical field
The invention belongs to Push Technology field, specially utilize the propulsion mode that Ampere force is power.
Background technology
Aircraft uses jet-propulsion technology mostly at present.Jet propulsive efficiency ratio is relatively low, so I proposes a kind of new The propulsion mode utilizing Ampere force.
Summary of the invention
In obturator, there is a N circle rectangle lead loop connecing power supply.Have on rectangular coil top a direction to Left magnetic field, in wire, electric current is as shown in the figure.Now wire is by Ampere force F=NBIL upwards.Ampere force makes wire upwards Motion, can head on obturator and make obturator also move upward when wire moves upward.Magnetic Field Source is fixed on obturator top The right and left in portion, when obturator moves upward, Magnetic Field Source also moves upward, so the relative position of Magnetic Field Source and wire is not Becoming, therefore magnetic field is the most to the left through wire, and Ampere force is constant.So obturator constantly can add under the effect of Ampere force Speed.
Accompanying drawing explanation
1. accompanying drawing 1: the rectangle ring in figure is N circle rectangular coil, represents with ring in the drawings, f is suffered by single-turn circular coil Ampere force.Rectangular coil is vertically fixed on obturator medial surface.Magnetic Field Source is permanent magnet.R is anti-short-circuit resistance.Power supply For DC source.Electric current is I.Obturator is magnetic shielding device.
Accompanying drawing 1 is principle of the invention figure.
2. accompanying drawing 2: magnetic field is just through the situation of a part for rectangle ring, i.e. this programme.In this case, rectangle ring is only By Ampere force F upwards.And this programme is by fixed magnetic field source and rectangular coil, make both relative invariant positions, thus This state can be kept, so Ampere force is constant, it is achieved accelerate.
Accompanying drawing 2 is magnetic field of the present invention and relationship ofloops figure.
3. accompanying drawing 3: accompanying drawing 3 is the UI and the Fv graph of a relation about time t.
4. accompanying drawing 4: whole rectangle ring is all in uniform magnetic field B.In this case, the power suffered by four limits of ring offsets mutually Disappear.Being equivalently employed without power, the most this situation is inadvisable.
Detailed description of the invention
The most on earth, Ampere force is more than gravity, can realize upwards flying.
The equation of motion on earth is as follows: (F-mg) s=1/2mv2
(NBIL-mg) s=1/2mv2
Taking B=1T, I=1A, L=0.2m, m=1kg, g=10, v=1m/s, N=100 can obtain s=1/20 rice.I.e. accelerate to one Metre per second (m/s) needs the distance of 1/20 meter.
2. it is not influenced by gravitation in space, predominantly Ampere force.It is easier to realize accelerating.Electric energy is supplied:
Solar panels can be used to power, and nuclear fission is powered and laser powered sensor.
Energy is changed
In space, electric energy is converted into kinetic energy and heat energy: UI=Fv+Q ' (t)
Limit velocity
Owing to output can not be higher than input power, Fv ＜=UI can be obtained
During speed maximum, FV=UI
Limit velocity V=U/BL
Energy conversion efficiency
Not considering anti-short-circuit resistance, ideally, in space, the time, energy turned from 0 to when accelerating to limit velocity Changing efficiency is 50%.
Because Fv is the linear function about t, available power and the graph of a relation of time, see accompanying drawing 3.
So comparing both areas, can obtain energy conversion efficiency is 50%.
If whole device has initial velocity, energy conversion efficiency is more than 50%.
Short circuit problem
Because being wire, it may appear that short circuit problem, so having connect a small resistor to prevent power supply short circuit.

Claims (1)

1. the propulsion mode utilizing Ampere force, it is characterised in that Magnetic Field Source and hot-wire coil are fixed in obturator, Make the relative invariant position of Magnetic Field Source and hot-wire coil, make around coil, there is a stationary magnetic field, obtain constant Ampere force, Device is made to accelerate.
CN201610268757.8A 2016-04-18 2016-04-18 Utilize the propulsion mode of Ampere force Pending CN106184822A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610268757.8A CN106184822A (en) 2016-04-18 2016-04-18 Utilize the propulsion mode of Ampere force

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610268757.8A CN106184822A (en) 2016-04-18 2016-04-18 Utilize the propulsion mode of Ampere force

Publications (1)

Publication Number Publication Date
CN106184822A true CN106184822A (en) 2016-12-07

Family

ID=57453010

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610268757.8A Pending CN106184822A (en) 2016-04-18 2016-04-18 Utilize the propulsion mode of Ampere force

Country Status (1)

Country Link
CN (1) CN106184822A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107010212A (en) * 2017-04-13 2017-08-04 上海微小卫星工程中心 Semi-autonomous sustainable aerial transport system based on combined type aircraft
CN111252267A (en) * 2020-04-30 2020-06-09 蓝箭航天空间科技股份有限公司 Space verification aircraft
CN111645879A (en) * 2020-04-30 2020-09-11 蓝箭航天空间科技股份有限公司 Ampere force driven flight method and aircraft

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2071186C1 (en) * 1993-07-07 1996-12-27 Анатолий Петрович Сысоев Electroacoustic converter
CN101823562A (en) * 2009-10-29 2010-09-08 杨伦华 Electromagnetic aircraft launch system for small scientific satellite spacecrafts on moon
CN102005980A (en) * 2009-08-30 2011-04-06 徐跃 Electromagnetic power device
CN102030113A (en) * 2009-10-01 2011-04-27 徐跃 Strong electromagnetic propulsion device
WO2012001459A1 (en) * 2010-06-30 2012-01-05 L Ferreira Moacir Jr Electrodynamic space thruster method and apparatus
US20150251561A1 (en) * 2013-08-20 2015-09-10 Airbus Ds Gmbh Air Vehicle and Levitation System for Air Vehicle

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2071186C1 (en) * 1993-07-07 1996-12-27 Анатолий Петрович Сысоев Electroacoustic converter
CN102005980A (en) * 2009-08-30 2011-04-06 徐跃 Electromagnetic power device
CN102030113A (en) * 2009-10-01 2011-04-27 徐跃 Strong electromagnetic propulsion device
CN101823562A (en) * 2009-10-29 2010-09-08 杨伦华 Electromagnetic aircraft launch system for small scientific satellite spacecrafts on moon
WO2012001459A1 (en) * 2010-06-30 2012-01-05 L Ferreira Moacir Jr Electrodynamic space thruster method and apparatus
US20150251561A1 (en) * 2013-08-20 2015-09-10 Airbus Ds Gmbh Air Vehicle and Levitation System for Air Vehicle

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107010212A (en) * 2017-04-13 2017-08-04 上海微小卫星工程中心 Semi-autonomous sustainable aerial transport system based on combined type aircraft
CN111252267A (en) * 2020-04-30 2020-06-09 蓝箭航天空间科技股份有限公司 Space verification aircraft
CN111645879A (en) * 2020-04-30 2020-09-11 蓝箭航天空间科技股份有限公司 Ampere force driven flight method and aircraft
CN111907732A (en) * 2020-04-30 2020-11-10 蓝箭航天空间科技股份有限公司 Space verification aircraft

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Application publication date: 20161207

WD01 Invention patent application deemed withdrawn after publication