[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

GB2517409A - An engine comprising a travelling wave magnetic field generator - Google Patents

An engine comprising a travelling wave magnetic field generator Download PDF

Info

Publication number
GB2517409A
GB2517409A GB1312183.5A GB201312183A GB2517409A GB 2517409 A GB2517409 A GB 2517409A GB 201312183 A GB201312183 A GB 201312183A GB 2517409 A GB2517409 A GB 2517409A
Authority
GB
United Kingdom
Prior art keywords
fluid
magnetic field
conducting
hollow body
engine
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.)
Withdrawn
Application number
GB1312183.5A
Other versions
GB201312183D0 (en
Inventor
Richard Prosser
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
Publication of GB201312183D0 publication Critical patent/GB201312183D0/en
Publication of GB2517409A publication Critical patent/GB2517409A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03HPRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03H1/00Using plasma to produce a reactive propulsive thrust
    • F03H1/0081Electromagnetic plasma thrusters
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/08Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/26Burning control

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Electromagnetism (AREA)
  • Plasma & Fusion (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)

Abstract

A petroleum derived fuel, e.g. natural gas/paraffin, is ignited in air within a hollow tubular body 2 and a resulting expanding conductive fluid ignition product is expelled from an outlet 8 of the hollow body 2 to produce thrust. The jet engine 1 uses a travelling wave magnetic field produced by a linear motor 11 to control the expansion of the fluid ignition product, accelerating the fluid ignition product, through acceleration zone 7, to produce thrust. The linear motor 11 comprises several magnetic field coils 12 axially spaced along the acceleration zone 7. The engine1 may include a second set of coils 13 downstream of the acceleration zone 7, which induce a current as the accelerated ignition product passes, the current being used to recharge the capacitor/battery 12A.

Description

An Engine Comnrising a Travelling Wave Magnetic Field Generator The present invention relates to a method in which a conducting fluid is controlled by a travelling wave magnetic field and ill particular an engine based on such a method.
Acceleration of a Conducting Fluid by a Traveling Magnetic Field' by Willis H. Braun describes the use of travelling magnetic wave accelerator which accelerates a conductiye fluid for the propulsion of interplanetary yehicles.
The accelerator works on a principle analogous to a linear motor. The accelerator comprises a tube surrounded by a series of coils through which an alternating current is fed. By controlling the current flow through the coils, a travelling magnetic wave can bc induced within thc tube. The magnctic wave acts upon a conducting fluid fcd into the tube, accelerating the fluid towards the other end of the tube.
In Experimental Investigation of A Constant-Velocity Travelillg Magnetic Wave Plasma Engine' by Robert E. Jones and other, the propellant is formed by firing electrons from an electron emitter into xenon gas in order to partially ionise it.
The Traveling-Wave Pump' by Eugene E. Covert aild other describes the use of such as system for power generation or wind tunnel propulsion. The plasma is generated in a manner similar to the aforementioned reference with the difference that helium is used as the propellant.
The following invention was conceived following discovery by the inventor that a flame is caused to be extinguished when placed near an electromagnet through which a current is passing.
According to a first aspect of the invention there is provided a method in which a fliel is ignited and the expanding fluid resulting from the ignition expelled to produce thrust, wherein a travelling wave magnetic field is used to control the expansion of the resulting expanding fluid.
Although not wishing to be bound to any particular theory, the inventor speculates the products of the ignition are or comprise an ionised or partially ionised gas which is affectable by a magnetic field. The invention provides a simpler method of forming the electrically conductive fluid over those previously known. It also enables an engine without moving parts.
In a preferred embodiment of the method gas comprising oxygen, favourably air, enters a hollow body, the flammable friel is ignited in the gas within the hollow body to form the conducting fluid and the travelling wave magnetic field controls the expansion of the conducting fluid towards an outlet of the hollow body. In order that the method is used to provide useful thrust, the gas may enter at or towards a first end of the body and the exhaust be accelerated towards a second end of the body.
The travelling wave magnetic field may be produced using a linear motor comprising one or more coils arranged such that when an alternating current is passed there-through, a corresponding magnetic wave is produced within the body which travels in a longitudinal direction with respect to the body.
Although a solid fuel may be used, in most practical applications a gas or liquid flammable fuel is preferred. Natural gas or petroleum derived fuels are thought particularly suitable.
The electrically conducting fluid may be directed past a circuit, e.g. through a further coil or coils, to induce, through electromagnetic induction, an electric current in the circuit. The induced current may be used to power the linear motor.
According to a second aspect of the invention there is provided an engine comprising a hollow body having an inlet through which a fluid can pass into the body, means to ignite a flammable fuel in the fluid to form an electrically conductive fluid and means to generate a travelling wave magnetic field to control the expansion of the electrically conductive fluid away from the inlet towards an outlet of the body.
The invention will now be described by way of example with reference to the Figure which is a schematic of an engine in which thrust is generated by igniting a fuel in air and accelerating the resulting conductive fluid using a travelling magnetic wave.
A jet engine 1 comprises a tubular body 2 having an outer casing 3 and a non-electrically conducting inner casing 4. The inner casing 4, which may be made from a ceramic material, is hollow and open at both ends to define a fluid pathway having an inlet 5 for air, a combustion zone 6, a zone in which the combustion products are accelerated 7 and an outlet 8.
Air that has passed through the intake 5 is mixed in the combustion zone 6 with a liquid petroleum derived fuel, e.g. paraflin, supplied via a fuel injector (shown schematically as 9) and the fuel/air mix ignited by an ignition system which may include a sparking means, e.g. a sparking plug 10.
The combustion product, being affectable by a magnetic field, is accelerated towards the outlet 8 by a linear motor 11 that comprises several magnetic field coils 12 each of which surround a portion the pathway such that combustion product must pass through the centre of the coils 12. The coils 12 are spaced axially along the acceleration zone 7.
The coils 12 arc connected to a multi-phase ale power supply 12A, which may be provided via a battery/capacitor and associated circuitry in order to create a travelling magnetic wave along the acceleration zone 7 in a manner which is well known to persons skilled in the art of linear motors.
In operation, the combustion product from the ignition in thc combustion zone is preferentially accelerated away towards the outlet 8, this causes more air to be drawn through the inlet 5 in which further fuel can be burnt.
The inner casing 3 and outer casing 4 are radially spaced apart to tbrm an annular bypasspassagel4thatextendsfromtheinlet5tothebackofthebody2. Whenthe engine is operating, air is drawn through the bypass passage 14 in order to provide cooling to the inner casing 3, coils 12, 13.
A second set of coils 13 are located towards the back of the engine, downstream of the accelerator zone 7. As with coils 12, they surround the pathway. As the accelerated ignition product passes along the pathway, through coils 13 they induce a current in the coils 13 and associated circuit 13A to recharge the capacitor/battery I 2A.
The engine may comprises a further coil 15 positioned upstream of coils for lbrming a steady magnetic field through which the accelerated ignition product passes before reaching coils 13. The steady magnetic field acts to separate the ions and electrons within the ignition product so that a net ion current results. The heavier ions are forced towards the centre of the stream of ignition product whereas the electrons are drawn radially outwards towards the inner wall of inner casing 4. Because the flow rate towards the centre of the stream is faster than at the edges of the stream a net ion current is produced which when passing through coils 13 induces a current therein.
The engine may comprises further coils (not shown) arranged to produce a steady magnetic field which extends from the combustion zone 6 to the outlet 8, to minimise the contact of the combustion products against the inner casing 4 to reduce energy loss caused by transfer of energy to the inner casing 4 as heat In a variation to the above, electrons can be introduced at the fuel injector so as to form electrostatiSly-charged droplets; these will improve the effectiveness of the magnetic fields. A high-voltage field will be rcquiitd and the positive electrode of the electrostatic circuit could be placed outsidc of the combustion chamber, with a collector plate inside. This arrangement will result in a further drag' fbrce on the electmns closest to the outer wall, increasing the net ion current and hence the efficiency of the generator.
The engine as a whole will tend to have a resonant frequency, which should result in the minimum energy loss possible. The engine may be fhrthcr provided with an anti-noise' circuit centred around that frequency will help to reduce the overall volume of the sound produced at the expense of optimum performance.

Claims (17)

  1. Claims 1. A method in which a fuel is ignited and the expanding fluid resulting from the ignition expelled to produce thrust, wherein a travelling wave magnetic field is used to control the expansion of the resulting expanding fluid.
  2. 2. A method according to claim I in which the travelling wave magnetic field is used to control the direction of expansion of the resulting expanded fluid.
  3. 3. A method according to claim 1 or 2 wherein the flammable fuel is mixed in a gas comprising oxygen
  4. 4. A method according to claim 3 wherein the flammable fuel is mixed in air.
  5. 5. A method according to any previous claim wherein the flammable fuel is a hydrocarbon fuel.
  6. 6. A method according to any previous claim wherein a linear motor causes acceleration of the expanded fluid.
  7. 7. A method according to any previous claim wherein a gas enters a first end of a hollow body, the flammable fuel is mixed and ignited in the gas within the hollow body to form an electrically conducting expanding fluid and the travelling magnetic field controls the expansion of the resulting electrically conducting expanding fluid towards an outlet at a second end of the hollow body.
  8. 8. A method according to claim 7 wherein the electrically conducting expanded fluid is directed past a circuit to induce, through electromagnetic induction, an electric current in the circuit.
  9. 9. A method according to claim 8 wherein the clectrically conducting fluid passes through a steady magnetic and/or electrostatic field in order to separate ions and electrons within the conducting expanding fluid before the conducting expanded fluid passes the circuit.
  10. 10. A method according to claim 8 or 9 wherein the current induced in the circuit is used to power the linear motor.
  11. 11. Anengineusingthemethodofanyclaim 1-10.
  12. 12. An engine comprising a hollow body having an inlet through which a fluid can pass into the body, means to ignite a flammable fuel in the fluid to form a electrically conductive fluid and means to generate a travelling wave magnetic field to control the expansion of the electrically conductive fluid away from the inlet towards an outlet of the body.
  13. 13. An engine according to claim 12 comprising means to cause a current to pass through one or more coils which surround the body so as to induce alongitudinally travelling magnetic wave field.
  14. 14. An engine according to claim 12 or 13 comprising an outer casing which is radially spaced from the hollow body to form a bypass channel through which fluid can flow to cool the hollow body
  15. 15. An engine according to any claim 12-14 wherein the electrically conductive fluidisarntngedtopassacircuitsoastoinduccacurrentwithinsaidcfrcuit
  16. 16. An engine according to claim 15 comprising means to generate a steady magnetic and/or electrostatic field through which the electrically conductive fluid is directed before passing the circuit.
  17. 17. A method in which a conducting fluid is accclcrated with a travelling magnetic field to generate thrust, wherein a flammable fuel is ignited in a gas comprising oxygen to create the conducting fluid.
GB1312183.5A 2013-06-14 2013-07-08 An engine comprising a travelling wave magnetic field generator Withdrawn GB2517409A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB1310632.3A GB201310632D0 (en) 2013-06-14 2013-06-14 An engine comprising a travelling wave magnetic field generator

Publications (2)

Publication Number Publication Date
GB201312183D0 GB201312183D0 (en) 2013-08-21
GB2517409A true GB2517409A (en) 2015-02-25

Family

ID=48914574

Family Applications (2)

Application Number Title Priority Date Filing Date
GBGB1310632.3A Ceased GB201310632D0 (en) 2013-06-14 2013-06-14 An engine comprising a travelling wave magnetic field generator
GB1312183.5A Withdrawn GB2517409A (en) 2013-06-14 2013-07-08 An engine comprising a travelling wave magnetic field generator

Family Applications Before (1)

Application Number Title Priority Date Filing Date
GBGB1310632.3A Ceased GB201310632D0 (en) 2013-06-14 2013-06-14 An engine comprising a travelling wave magnetic field generator

Country Status (1)

Country Link
GB (2) GB201310632D0 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108317061A (en) * 2017-12-22 2018-07-24 兰州空间技术物理研究所 A kind of ion Hall mixing thruster of common magnet
CN111140447A (en) * 2019-12-23 2020-05-12 北京航空航天大学 Vector magnetic nozzle for electric propulsion comprising a bypass electromagnetic coil

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5170623A (en) * 1991-01-28 1992-12-15 Trw Inc. Hybrid chemical/electromagnetic propulsion system
WO2010096087A1 (en) * 2008-08-19 2010-08-26 Sonic Blue Aerospace, Inc. Magnetic advanced generation jet electric turbine
US20130047578A1 (en) * 2011-08-31 2013-02-28 Space Systems/Loral, Inc. Unified chemical electric propulsion system

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5170623A (en) * 1991-01-28 1992-12-15 Trw Inc. Hybrid chemical/electromagnetic propulsion system
WO2010096087A1 (en) * 2008-08-19 2010-08-26 Sonic Blue Aerospace, Inc. Magnetic advanced generation jet electric turbine
US20130047578A1 (en) * 2011-08-31 2013-02-28 Space Systems/Loral, Inc. Unified chemical electric propulsion system

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108317061A (en) * 2017-12-22 2018-07-24 兰州空间技术物理研究所 A kind of ion Hall mixing thruster of common magnet
CN111140447A (en) * 2019-12-23 2020-05-12 北京航空航天大学 Vector magnetic nozzle for electric propulsion comprising a bypass electromagnetic coil

Also Published As

Publication number Publication date
GB201310632D0 (en) 2013-07-31
GB201312183D0 (en) 2013-08-21

Similar Documents

Publication Publication Date Title
US6484492B2 (en) Magnetohydrodynamic flow control for pulse detonation engines
Wang et al. Transient plasma ignition of quiescent and flowing air/fuel mixtures
US8082725B2 (en) Electro-dynamic swirler, combustion apparatus and methods using the same
US3110294A (en) Methods and apparatus for mixing fluids
US20100186414A1 (en) Magnetic ion plasma annular injection combustor
AU725458B2 (en) Traveling spark ignition system and ignitor therefor
CN1761816B (en) Spacecraft thruster
US6321733B1 (en) Traveling spark ignition system and ignitor therefor
US20110174277A1 (en) Universal hydrogen plasma carburetor
US8146371B2 (en) Direct induction combustor/generator
US20060076872A1 (en) Hall effect thruster with anode having magnetic field barrier
EP3438437B1 (en) Scramjets and associated aircraft and methods
Zheng et al. Acceleration of DDT by non-thermal plasma in a single-trial detonation tube
GB2517409A (en) An engine comprising a travelling wave magnetic field generator
US3388291A (en) Annular magnetic hall current accelerator
US3660700A (en) Magnetohydrodynamic generator
CN104314692A (en) Microwave surface wave ignition combustion supporting device
CN110793060B (en) Controllable plasma igniter in atmospheric pressure environment
CA1180743A (en) Disc-shaped m.h.d. generator
Beal et al. Development of the linear gridless ion thruster
Alekseev et al. The influence of an external magnetic field on the burning of a high-speed air-carbon mixture
US3162781A (en) Magnetohydrodynamic generator
RU2290736C1 (en) Method for generating electrical energy on board hypersonic flying vehicle and mhd generator used for the purpose
US3371490A (en) Magnetodynamic plasma accelerator device
RU2225533C2 (en) Rocket electric motor

Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)