GB2408971A - Aircraft using both turbojet and rocket propulsion - Google Patents
Aircraft using both turbojet and rocket propulsion Download PDFInfo
- Publication number
- GB2408971A GB2408971A GB0326397A GB0326397A GB2408971A GB 2408971 A GB2408971 A GB 2408971A GB 0326397 A GB0326397 A GB 0326397A GB 0326397 A GB0326397 A GB 0326397A GB 2408971 A GB2408971 A GB 2408971A
- Authority
- GB
- United Kingdom
- Prior art keywords
- terrestrial
- aircraft
- rocket
- jet
- freight
- 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- Withdrawn
Links
- 230000032258 transport Effects 0.000 claims description 7
- 238000005516 engineering process Methods 0.000 claims description 6
- 230000015556 catabolic process Effects 0.000 claims description 4
- 238000006731 degradation reaction Methods 0.000 claims description 4
- 230000000750 progressive effect Effects 0.000 claims description 2
- 230000009467 reduction Effects 0.000 claims description 2
- 230000006978 adaptation Effects 0.000 claims 1
- 238000002512 chemotherapy Methods 0.000 claims 1
- 239000000446 fuel Substances 0.000 description 12
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 7
- 239000001301 oxygen Substances 0.000 description 7
- 229910052760 oxygen Inorganic materials 0.000 description 7
- 241001254649 Ambidexter Species 0.000 description 6
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical class C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 5
- 235000015842 Hesperis Nutrition 0.000 description 3
- 235000012633 Iberis amara Nutrition 0.000 description 3
- 240000002836 Ipomoea tricolor Species 0.000 description 3
- CBENFWSGALASAD-UHFFFAOYSA-N Ozone Chemical compound [O-][O+]=O CBENFWSGALASAD-UHFFFAOYSA-N 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 230000005484 gravity Effects 0.000 description 3
- JTJMJGYZQZDUJJ-UHFFFAOYSA-N phencyclidine Chemical compound C1CCCCN1C1(C=2C=CC=CC=2)CCCCC1 JTJMJGYZQZDUJJ-UHFFFAOYSA-N 0.000 description 3
- 239000002760 rocket fuel Substances 0.000 description 3
- 239000005437 stratosphere Substances 0.000 description 3
- MYMOFIZGZYHOMD-UHFFFAOYSA-N Dioxygen Chemical compound O=O MYMOFIZGZYHOMD-UHFFFAOYSA-N 0.000 description 2
- 241000196324 Embryophyta Species 0.000 description 2
- 241000243251 Hydra Species 0.000 description 2
- 239000011335 coal coke Substances 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 231100000566 intoxication Toxicity 0.000 description 2
- 230000035987 intoxication Effects 0.000 description 2
- QRXWMOHMRWLFEY-UHFFFAOYSA-N isoniazide Chemical compound NNC(=O)C1=CC=NC=C1 QRXWMOHMRWLFEY-UHFFFAOYSA-N 0.000 description 2
- 239000003350 kerosene Substances 0.000 description 2
- 230000005855 radiation Effects 0.000 description 2
- 230000009466 transformation Effects 0.000 description 2
- 238000000844 transformation Methods 0.000 description 2
- 238000007514 turning Methods 0.000 description 2
- YMHOBZXQZVXHBM-UHFFFAOYSA-N 2,5-dimethoxy-4-bromophenethylamine Chemical compound COC1=CC(CCN)=C(OC)C=C1Br YMHOBZXQZVXHBM-UHFFFAOYSA-N 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 description 1
- 206010012239 Delusion Diseases 0.000 description 1
- CWYNVVGOOAEACU-UHFFFAOYSA-N Fe2+ Chemical compound [Fe+2] CWYNVVGOOAEACU-UHFFFAOYSA-N 0.000 description 1
- 241000238631 Hexapoda Species 0.000 description 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- 235000006679 Mentha X verticillata Nutrition 0.000 description 1
- 235000002899 Mentha suaveolens Nutrition 0.000 description 1
- 235000001636 Mentha x rotundifolia Nutrition 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 241000545067 Venus Species 0.000 description 1
- GMACPFCYCYJHOC-UHFFFAOYSA-N [C].C Chemical compound [C].C GMACPFCYCYJHOC-UHFFFAOYSA-N 0.000 description 1
- OLBVUFHMDRJKTK-UHFFFAOYSA-N [N].[O] Chemical compound [N].[O] OLBVUFHMDRJKTK-UHFFFAOYSA-N 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- 239000008186 active pharmaceutical agent Substances 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 239000004411 aluminium Substances 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 229910002091 carbon monoxide Inorganic materials 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 239000000571 coke Substances 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 231100000868 delusion Toxicity 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 238000003475 lamination Methods 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000005435 mesosphere Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000001459 mortal effect Effects 0.000 description 1
- 239000002574 poison Substances 0.000 description 1
- 231100000614 poison Toxicity 0.000 description 1
- 238000010248 power generation Methods 0.000 description 1
- 230000003236 psychic effect Effects 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 210000002435 tendon Anatomy 0.000 description 1
- 230000005945 translocation Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
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
- B64G1/401—Liquid propellant rocket engines
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/023—Aircraft characterised by the type or position of power plants of rocket type, e.g. for assisting taking-off or braking
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/16—Aircraft characterised by the type or position of power plants of jet type
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/14—Space shuttles
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Abstract
An aircraft utilises both turbojet and rocket propulsion. A variety of different forms of aircraft are disclosed.
Description
240897 1 1
Specification _
In examining the shortcomings of aero jets to four stroke ignition engines, exhausts tend to cloak easier production simpler less movable parts and greater thrusts. In both the Columbia or US Shuttle and the flying saucer concepts the immediate -profit motives to safe and convincing balanced moments in atmospheric jets then leading to rockets and rocket nozzles, regards effects on ozone at the poles and alterations of the delicate and less dense stratas above the stratosphere.
Terrestrial and marine transports vehicles and ships post World War Two in utilising safer methanes and oxygen re researched fossil plant coal cokes, heavy lead encased grommet nuclear power station electricities, to theoretic trains and airship from submarine extant technologies. Where status quo chemical knowledge and eventual Photo atmospheric total degradations, rather than exces_ oxygen intoxications, would then allow such efforts, by otherwise high passenger traffic ships and airships, via rocket jets., kill factors in looking at aeroplanes and crucial omissive workabilities in the utilizations of one engine inherent imbalance, for light planes, biased to turn with the engine's turning inertia just one way flying as wind fills a sail ships canvas, but that it finds in air generated by its own forward Cyclopian aerially workable propellers or propeller. Where surely, angular velocities
Specification:
öf the Earth and it's satellite, moving at som 29 000 mph (32 000 kmph) at one sixth the Earth's mass is not as frightening, The psychology of aircraft over oceans and seas, if taken as safe, where they fly low enough where ships liners are used, in statistically balanced safety and international accord as to but trade and freight frequencies, a code or humane travel risk statistic could emerge. Weightlessness where the Earth's spin and a but huge cupped hand attractive force by the Sun on it an] its satellite, infers the exacting but thus legalistic liberating feature of humankind's travel and trade futurities.
Russian rocketry and American seem to one to indicate if nothing else nuclear fissional thrust only activated in weightless conditions where exactly and accurately controlled.
The whole basis of perfected flight and the parallel pollutional penalties- of fossil plant and seemingly more so fauna fuels, contrasts such insect bird bat flight unpolluted to such hydra; carbon or pure with impurities coal cokes atmospheric degradations now. Th.e. evolution of double acting steam feasibilities handed naively though else putting off those penalties for but later, showing through human error in aircraft productive workabilities and mortal statistical risk.t That humankind has future progressive Science at its fingertips, or self delusion is up it to it to discover in those terms. at.
Ambidexter torque in organic fuelled jets and rockets
Description
In industrial skills from malleabilities of metallurgical pLasticities, hard metal with ferrous bases becoming molten rather less rapidly than softer aluminium.
The tate-of-the-art in all inventive laminations, with written or computer stored data tends nowadays, to infer a conflict in that ingenuity and invention, where atmospheric transformations from millennia millions of bears of constant oxygen nitrogen becoming in the 19th and 20th centuries, globally mixed with carbon monoxide, or in purer forms carbons. This has been the tendency, with better casting techniques, machining automations, to present, more economic fuel use yes, faster vehicles debatable. So that as with the 'discovery of fire lighting, a - progre SB ive scientific technology of hydra carbon methane to oxygen burning technology in transport median, to a revolution actually and socially, to coke nuclear electric or oxygen hydrogen type replacement is needed.
Where further initiatives by West Europe in solar planet space and pollutionless future industrial common sense and love of life is absent, these pragmatics are seemingly forgotten in the gains and services of the moment..
By now any thoughts of tackling automotive and oil producing firms first, rests on putting off the day with total nuclear to solar panel type electricities. Where these absolutes are then confirmed by all major producer governments tax and profit print mint targets, ,a mundane position of reduction of vehicular aero and marine craft, to conform with only such power generation clean electric or methane is overdue. Power, that is electrical, that with say underground live cables for computers and mensurate specific absorption rates understood, in regard to et co--r. uters, should leave a static work force and absolute atmospheric purities'..
l'he jet banders to rocket mechanics and chemistry offers
Description
the apparent disparities between stratospheric some 30mls(50k and Mesosphere heights above sea level, the ionispheric from 54mls to 250mls (400kms) , to what seems like 68 miles (85kms,
-
(108.8 km) when zero gravity is experienced introduceo pollutional type uses for both ambiderter psychic perfections and innate balance by roekets.what clearly appears from considerations of ionizations, heights that jet planes can achieve, and ongoing public service transport, rather less commercial else, absolute. priorities of use, to degradations of breathable air globally' is automotive marine pollutionles fuel firstly. Considerations of high altitude Jets, infers that pollution is thinner because air is less dense. Wholesale use of electric cars sud'electro magnetic helmeted and where without radiation threats from grommet like steam to nuclear interfaces for airships, shipping itself and electric train generating power a bealthacr.poition for steel products internationally seems to emerge. Where the use of jet planes that can reach maximum height altitudes with good initially Columbian Shuttle Moon Lander loads, but that can circle the earth, from a jet ambidexter system with racket assistance to boost quick gravityless cond.i).i9 and thence retro rocket fuel amounts to slow re entry. - friction, the objectives could be reached, feasibly..
From assessments there altitude figures give, rocket fuel, for some say with ambidexter jets reaching say 20 miles ( 32 Ems) would be required for journeys, between New York Melbourne some 10 000 miles approx ( 16 000 Ems) as for New York London some 3 000 miles ( 4 BOO kms)..
Coupling of aero jet amble with rocket motors as shown in Figure 1 the obvious control, of wings and ailerons rudders and tails, requires drastic, rocket lozzle directed thrusts, rather as maritime use of water jets' or again variable nozzle controls for navigation..
figure 2 infers activated armature controls could release take off boosters with parachutes, leaving when in orbit such nozzle direction use, momentum like navigation
Description
to provide some perpetual motion power. A orbit then not straight vertically upwards path. Of course fuel, where one circuit of the Earth by artifical satellites takes a hour, short for a tendon Sydney journey today, seems boosted, by only strong initial thrusts'..
Figure 3 infers that yes lower ambi jet fuel needs will leave capacity for greater atmospheric vacuum and gravity zero conditions, to utilise rocket liquid oxygen fuels more economically. Being aero ambideter turning moments in taking off, reaching maximum stratospheric air
altitude, is a ancillary job to overall, prior art
notoriously inefficient with rocket fuel per mile (kilometres) travelled, Here the fuselage is considered for fuel, wings for , i^ passenger space and crew in the " nosed Vertical take off cruciform aircraft rocket shapes or the saucer shape for slow jet nozzles downwards aspects for a 1000m height over rsea. Conventional aero jet take offs) of course require, differing modes of seating and belt securities, most terrestrial journies hardly providing hammock bunk provisions. The perpetual notional hour global encirclements of satellites, unfixed as at a terrestrial pole would seem to succomb to powered fuel storage equations..
Figure 4, shows rough atmospheric layers.
_, _ r j The Ozone layer is subject to solar radiation.
Radar and altitude detecting instruments or gaseous analyst Of these layers shows the obvious straight paths to zero gravity and thence r avel from A'' to , and re-entry.
Description
Figure 5 shows the flying saucer concept. Ailerons rudders as per fixed winged aircraft, vertical take off provision and then rapid ascent in a angled manner.
Figure 6 infers a return to conventional take off and land aircraft, but with rocket provision, payload capacity and wing to - fuselage ratios adequate now to take in both DS shuttle technologies and flying saucer lift'..
The facts and figures and actual physical phenomena associated with these miraculous modes of transport housed in the wonder of electronics electro magnetic forces and quantum theory, the speed of sound,light and air turbulence, should be to cause and effects, experimentally model wise open for all to see. Were these craft made into models, tested by remote control, distant control and with correct scaling up laws of physics, safely and rather to full recovery of the same aircraft to rockets over sea, even futuristically or actually with float wheel provision, ambidexter instrumentation and guage, pollution priorities are but the one absolute against
Description
a possible jet ambldexter route from off isolated parts of Long Island Connecticut, to near Shannon Bay. The only oxygen kerosene balancing, journey, the capitalist socio agricultural economic free world needs to make over otherwise ship airship connected land, Both Earth circling satellites without liquid oxygen needs by moving not stationary, vertical jet to Mesospherei stratosphere economies and pollution levels, require 6B mls (109kms)) vertically to reach weightlessness. Robotic tests made off Los Angeles, Qr models, bouncing up and down from weightlessness to gravitational effects, suffer dangerous though invisible atmospherics. In deciding fuel oxygen or kerosene fuels, or non momentum between:landings and take offs are crucial, where given landing co ordinates the Columbia shuttle can come down without power, when no flying boat floats are needed! As the communicational accord worldwide reaches UN ED US CIS et Koyto like uninanimities on atmospherics with; considered organic gaseous poisons or innocuous saturations of carbons, gradual transformations to and from petrol methane electric to electric car lorry work leisure habits, seemingly impossible to change, even with computer voltage cables delimiting travel between towns and countries, jet ambidexter rocket priorities, to ozone levels outside or inside the atmosphere should emerge, Figure 4 represents the layers of the Earth, varying mainly in air densities, where satellite technology is cluttered to aerodynamic spin off to weightlessness safeties that seem relatively secure in lax ing. The wine; observed orbits of other planets from Holmes Chapel or Puerto R'co rather provide with Mars or Venus manned/womanned objectives Savings on jet ambidexter biases ofAD1917 four strokes in terrestrial atmosphere, to not dropped smaller model baby sized aircraft rocket planes, seems a absolute for terrestrial handed jets to rocket, orbiting
Description
To where oxygen under that stratosphere, and some possible intoxications, is considered in popular chemistry to be the least likely, per fifteen acres of ploughed land battery tractor collected vehicular exhaust polluter. Reduced fuel for balanced jet turbines, seemingly to add some logistics, to overall, satellite perpetual motion translocations and the amounts of fuel then needed for GPS global positioning satellite A to destinations can or could be achieved'.. at,
Claims (2)
- Claims 1. Introduction from state of the art chemo technology andaeronautics a feasible aero jet with rocket power separately used and in conjunction, that would be a rapid means if accurately produced of terrestrial transport for freight and passengers avoiding itself atmospheric degradation'.
- 2. Prioritied adaptations of aerial transports for astronomy conjunctions progressive science that assist do not deter terrestrial oceanic modes of freight passenger transport seen to be aiming for fossi' fauna pollution reductions in reviewing fossil flora or nuclear, to terrestrial lead container grommet delimited precautions now..Peter A Fulmes 17th7,',ay2001
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0326397A GB2408971A (en) | 2003-11-05 | 2003-11-05 | Aircraft using both turbojet and rocket propulsion |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0326397A GB2408971A (en) | 2003-11-05 | 2003-11-05 | Aircraft using both turbojet and rocket propulsion |
Publications (2)
Publication Number | Publication Date |
---|---|
GB0326397D0 GB0326397D0 (en) | 2003-12-17 |
GB2408971A true GB2408971A (en) | 2005-06-15 |
Family
ID=29726420
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB0326397A Withdrawn GB2408971A (en) | 2003-11-05 | 2003-11-05 | Aircraft using both turbojet and rocket propulsion |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2408971A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CZ300681B6 (en) * | 2008-08-20 | 2009-07-15 | Vycítal@Jirí | Aircraft hybrid drive |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB758403A (en) * | 1953-01-11 | 1956-10-03 | Joseph Smurik | Improvements relating to aircraft |
GB830520A (en) * | 1956-09-10 | 1960-03-16 | William Low Eddie | Improvements in or relating to aircraft |
GB1111845A (en) * | 1967-04-14 | 1968-05-01 | Arthur Paul Pedrick | Improvements in hypersonic vtol aircraft |
GB2190964A (en) * | 1986-05-28 | 1987-12-02 | Messerschmitt Boelkow Blohm | Combined turbojet, ramjet, rocket propulsion unit |
US4817892A (en) * | 1986-04-28 | 1989-04-04 | Janeke Charl E | Aerospace plane and engine therefor |
US6119985A (en) * | 1997-03-07 | 2000-09-19 | Pioneer Rocketplane Corporation | Reusable rocket-propelled high altitude airplane and method and apparatus for mid-air oxidizer transfer to said airplane |
US6227486B1 (en) * | 1999-05-28 | 2001-05-08 | Mse Technology Applications, Inc. | Propulsion system for earth to orbit vehicle |
-
2003
- 2003-11-05 GB GB0326397A patent/GB2408971A/en not_active Withdrawn
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB758403A (en) * | 1953-01-11 | 1956-10-03 | Joseph Smurik | Improvements relating to aircraft |
GB830520A (en) * | 1956-09-10 | 1960-03-16 | William Low Eddie | Improvements in or relating to aircraft |
GB1111845A (en) * | 1967-04-14 | 1968-05-01 | Arthur Paul Pedrick | Improvements in hypersonic vtol aircraft |
US4817892A (en) * | 1986-04-28 | 1989-04-04 | Janeke Charl E | Aerospace plane and engine therefor |
GB2190964A (en) * | 1986-05-28 | 1987-12-02 | Messerschmitt Boelkow Blohm | Combined turbojet, ramjet, rocket propulsion unit |
US6119985A (en) * | 1997-03-07 | 2000-09-19 | Pioneer Rocketplane Corporation | Reusable rocket-propelled high altitude airplane and method and apparatus for mid-air oxidizer transfer to said airplane |
US6227486B1 (en) * | 1999-05-28 | 2001-05-08 | Mse Technology Applications, Inc. | Propulsion system for earth to orbit vehicle |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CZ300681B6 (en) * | 2008-08-20 | 2009-07-15 | Vycítal@Jirí | Aircraft hybrid drive |
Also Published As
Publication number | Publication date |
---|---|
GB0326397D0 (en) | 2003-12-17 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |