EP3619402A1 - Procede de construction de propulseurs ou de moteurs contenus dans un carter cylindrique et propulseur ou moteur associé - Google Patents
Procede de construction de propulseurs ou de moteurs contenus dans un carter cylindrique et propulseur ou moteur associéInfo
- Publication number
- EP3619402A1 EP3619402A1 EP18722475.3A EP18722475A EP3619402A1 EP 3619402 A1 EP3619402 A1 EP 3619402A1 EP 18722475 A EP18722475 A EP 18722475A EP 3619402 A1 EP3619402 A1 EP 3619402A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- wheel
- chamber
- fixed
- carpyz
- shaft
- 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- Withdrawn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
- 238000000034 method Methods 0.000 title claims description 19
- 239000012530 fluid Substances 0.000 claims abstract description 44
- 101000837626 Homo sapiens Thyroid hormone receptor alpha Proteins 0.000 claims abstract description 26
- 102100028702 Thyroid hormone receptor alpha Human genes 0.000 claims abstract description 26
- 230000005611 electricity Effects 0.000 claims description 25
- 230000002093 peripheral effect Effects 0.000 claims description 12
- 238000010276 construction Methods 0.000 claims description 6
- 239000000446 fuel Substances 0.000 claims description 5
- 239000003380 propellant Substances 0.000 claims description 5
- 230000003247 decreasing effect Effects 0.000 claims description 3
- 239000007788 liquid Substances 0.000 claims description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Chemical compound O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 3
- 238000006243 chemical reaction Methods 0.000 claims description 2
- 238000002485 combustion reaction Methods 0.000 claims description 2
- 238000010304 firing Methods 0.000 claims description 2
- 239000007787 solid Substances 0.000 claims description 2
- 244000241796 Christia obcordata Species 0.000 abstract 1
- 238000007664 blowing Methods 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
- F01D1/02—Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines
- F01D1/023—Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines the working-fluid being divided into several separate flows ; several separate fluid flows being united in a single flow; the machine or engine having provision for two or more different possible fluid flow paths
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
- F01D1/02—Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines
- F01D1/026—Impact turbines with buckets, i.e. impulse turbines, e.g. Pelton turbines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D15/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
- F01D15/10—Adaptations for driving, or combinations with, electric generators
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
- F02K3/068—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type being characterised by a short axial length relative to the diameter
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
- F02K3/077—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type the plant being of the multiple flow type, i.e. having three or more flows
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L50/00—Electric propulsion with power supplied within the vehicle
- B60L50/10—Electric propulsion with power supplied within the vehicle using propulsion power supplied by engine-driven generators, e.g. generators driven by combustion engines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/04—Blade-carrying members, e.g. rotors for radial-flow machines or engines
- F01D5/043—Blade-carrying members, e.g. rotors for radial-flow machines or engines of the axial inlet- radial outlet, or vice versa, type
- F01D5/048—Form or construction
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/70—Application in combination with
- F05D2220/76—Application in combination with an electrical generator
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K7/00—Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
- H02K7/18—Structural association of electric generators with mechanical driving motors, e.g. with turbines
Definitions
- the present invention relates to a method of construction of thrusters or engines contained in a cylindrical housing, and thrusters or engines of this type. STATE OF THE ART
- the invention presents a method for constructing thrusters or motors contained in a cylindrical casing (CA1) characterized by the fact that they use a wheel of the CARPYZ THRA Turbine Helix Reactor Powered 1 type according to the publication by Patent WO20161 10364 coupled to an SME + RME electric motor and, or at least one wheel type CARPYZ TaG Turbine Buckets 3 according to the patent publication WO2014067823 is at least one wheel Spoons type CARPYZ TaC according to the application LU100749 of March 28 2918, which is coupled to an electricity generator SGE + EGR, which alone is associated with it, and that they use the forces supplied to them by electrical energy or energy fluids which are introduced from the outside by orifices in the 16-19 housing through the peripheral chambers D and E or in the center of the THRA.
- CA1 CARPYZ THRA Turbine Helix Reactor Powered 1 type according to the publication by Patent WO20161 10364 coupled to an SME + RME electric
- CARPYZ Propellants combine the mechanical and electrical energies, supplied from the outside, and by energy fluids, and in very innovative ways propose to provide very strong axial thrusts adaptable to the needs demanded every moment by all kinds of gear so that in particular they take off vertically. This is possible by using CARPYZ Turbo Helicopter Reactor THRA powered wheels associated with TaG Bucket Turbines or TaC Spoons upwardly oriented even with their small diameter. These thrusters first use the large thrust provided simultaneously by the propellers driven by electric motors, but then especially that provided by the turboprops using simultaneously a very energetic liquid or gaseous fuel, for example a hydrogenated gas or water vapor. at high pressure, which generates momentarily on demand a very great force necessary for vertical takeoff.
- a very energetic liquid or gaseous fuel for example a hydrogenated gas or water vapor.
- the thrusters due to their small diameter tilt gradually to the horizontal. They then use only the energy demanded by the electric motors integrated in the thrusters that rotate the two internal propellers which are in series, and which are much less energy-efficient than the reactors. This goes in the direction of the aircraft if possible all electric after takeoff or fully ecological and also hope for an overall improvement in weight.
- the invention also has a thruster or motor contained in a cylindrical casing (CA1) constructed by this method of construction, in which the thruster or motor comprises a wheel type CARPYZ THRA Turbine Propeller Reactor Powered 1 coupled to an electric motor SME + RME and at least one wheel type CARPYZ TaG Turbine Bucket 3 or type CARPYZ TaC Turbine Spoon which is coupled to an electricity generator SGE + EGR, either a bucket wheel type CARPYZ TaG or a spoon wheel of CARPYZ type TaC only where associated, and that it uses the forces provided by electrical energy or energy fluids which are introduced from the outside through orifices made in the casing 16-19 through the peripheral chambers D and E or in the center of the THRA wheel.
- CA1 cylindrical casing
- FIG. 1 and 2 show a half-propeller cut at its axis constructed according to one possible embodiment by the method of the invention
- FIG. 3 shows the method of the invention with the arrangement used for the godet wheel to rotate the shaft in a bearing whose fixed ring is connected and fixed within the fixed chamber;
- FIG. 4 represents the method of the invention with the arrangement used for the godet wheel to rotate the motor shaft secured to the EGR rotor of an electricity generator whose SGE stator is connected and fixed to the outside the fixed chamber;
- FIG. 5 represents a front view of a THRA wheel with turbo inlet + propeller + peripheral chamber
- FIG. 6 represents a rear view of a THRA wheel with a peripheral circular slot and for example a tube which starts from the center, passes into a blade and ends up on the slot;
- FIG. 7 shows a partial view of a wheel and the inlet of the inner duct of a blade
- FIG. 8 shows a partial view of a circular slot wheel with slot and blade entries
- FIG. 9 shows a partial view of the output of the fixed wheel with the fluid that rotates according to the invention.
- the invention is a method for constructing thrusters or engines which are contained in a cylindrical casing (CA1) and they use a wheel type CARPYZ THRA Turbine Propeller Reactor Powered 1 according to Patent Publication WO20161 10364 1 coupled to an electric motor (SME + RME) and at least one wheel type CARPYZ TaG Turbine Buckets 3 according to the patent publication WO2014067823 or at least one wheel type CARPYZ TaC Turbine spoons according to the application LU100749 of March 28, 2918 which is coupled to a SGE + EGE electricity generator, either with a CARPYZ TaG-type bucket wheel or with CARPYZ TaC-type spoons only where associated, and that they use the forces supplied to them by electrical energy or energetic fluids which are introduced from the outside through orifices made in the housing 16-19 through the peripheral chambers D and E or in the center of the THRA.
- thrusters are contained in a crankcase and first use a wheel type CARPYZ THRA Turbine Propeller Reactor Powered.
- the ambient fluid between 12 first in the center of the wheel A, whose direction of rotation right or left is predetermined by the designer, and continues its way in the inner channels B of the hollow blades of the propeller located in the middle of the wheel 1 which blows backwards and whose blades go to their largest diameter to a peripheral circular chamber C provided with at least one circular slot open towards the rear of the wheel.
- This wheel is rotated at the rear in the center by the shaft X1 of the rotor of an electric motor SME + RME which is preferably pierced by a hole of small diameter 13 in its center from side to side.
- the jets of fluid projected by the slots of the chamber of the wheel C are received by circular slots placed in concordance opposite in the bore of the inlet of the cylindrical fixed hollow chamber glued to the casing D, and the channels formed by the slots which are provided with profiled blades placed inside between the cylindrical walls and confirm the direction of rotation of the fluid supplied by the chamber C.
- a set of hollow radial profiled fixed blades 2 pass through the chamber fixed to the casing D, and will then become firmly attached to the stators of the electric motor EMS and the electricity generator SGE which are placed in the center of the wheel.
- the hollow interior of these profiled fixed blades allows the passage of the electric wire plies 15-17 for the stators, the SME electric motor and the electricity generator SGE.
- the fluid received from the slots of the chamber C is continued by turning in the fixed circular chamber E which receives the energy or fuels introduced by orifices 16 from outside the housing propellant, and are immediately distributed in the rooms.
- the chambers are provided with electric firing devices 18.
- the first two chambers are continued by another fixed cylindrical fixed chamber F fixed to the casing which is provided inside concentric tubes to the axis of the wheel placed one inside the other and spirally wound radial blades placed internally between the cylindrical walls of this chamber which form intersecting channels that each individually directs the flow of fluid energy by rotating towards the rear of the wheel.
- the chamber F sends the jets of the energy fluids through its channels by turning on the channels of the buckets of a wheel Turbine bucket or spoons of a wheel Turbine G Spoons which are placed in circular concordance with the output of the channels of the F.
- the cups or spoons when rotating fit globally on virtual cylindrical crowns. The center of these crowns is often occupied by a rear-blowing propeller 3 and enhances the flow provided by the THRA wheel 1.
- this propeller is fixed on the shaft X2 of the rotor of the electricity generator
- the stator of the electricity generator SGE is secured to the stator of the electric motor EMS of the wheel type CARPYZ THRA and they are connected to the chamber fixed to the casing D by hollow profiled fixed radial blades which allow to pass and straighten at best the central flow 2 of the propeller of the CARPYZ THRA type wheel. These profiled hollow blades allow in their interior the passage of electric sheets for the engine and for the generator 15-17.
- a wheel V provided with independent profiled radial blades is optionally interposed and mounted on pivots between the chamber D and the stator of the engine SME and its blades are adjustable by a rod 14 coming from the outside of the housing through D.
- the shaft X1 of the rotor of the electric motor RME is decreased in diameter towards the rear at its output from the engine and enters the inside of the tube of the shaft X2 of the rotor of the generator of electricity RGE provided with bearings L in order to maintain together in concentricity the trees in one another.
- the rotor shaft of the electric motor which is decreased in diameter X1 is continued through the cased shaft of the electricity generator X2 which receives at its output from the electricity generator a rotating disk plate D2.
- the shaft of the electric motor also receives, as soon as after, another disk disk D1 which when they are clamped together by remotely controlled electrically remote devices 22 which make it possible to join the rotation of the two shafts on demand.
- An electrical variant makes it possible to regulate, by means of the frequency converter used to control the speed of the electric motor, as a function of the speed of the electricity generator possibly controlled by the encoder and / or by the electric power which it emits in order to synchronize together at the same time. better the rotation speeds of X1 X2 trees.
- the fixed casing of the thruster is extended towards the rear and covers the rotary wheel with buckets or spoons and is then secured to a fixed chamber H which is placed in concordance with the flow outlet of the wheel TaG bucket or the wheel TaC spoons and is provided with concentric tubes placed one inside the other in
- the casing of the thruster in this case is not constantly cylindrical rectilinear, but has its diameter which goes flowing CA2 or narrowing backwards, to change the useful surface of energy exchange buckets of the TaG wheel or spoons of the TaC wheel with the energy fluids it receives.
- the supply of energy fluid chambers is made starting from the outside of the casing of the thruster 19 by at least one pipe which pass through the fixed chamber bonded to the casing D and continues in the fixed profiled hollow blades 2 which go up to the shaft of the rotor of the electric motor X2 to which they connect by a small chamber placed between two circular joints.
- the shaft is drilled radially there and communicated with at least one hole parallel to the axis of the shaft which radially communicate with tubes that enter the THRA wheel.
- a direct supply can be made to this place 21. They go to the sprayers placed in the peripheral chamber of the wheel (C) which send either the jets or the fog of the energy fluids rotating in the channels of the fixed chamber D whose orientation of the blades confirm the direction of rotation of the fluids.
- the energy products introduced from outside the casing of the propellant 16 into the chamber E are gaseous or liquid or partially solid, and by combustion or chemical reactions or by their temperature (such as high-pressure water vapor) , can locally generate large fluid pressures that will migrate to the chamber F and go to the outputs of the channels by turning on to activate the buckets of the TaG bucket wheel or the spoons of the Tc spoon wheel.
- FIGS. 5 to 10 show THRA wheels and turbines with TaG cups of CARPYZ type or with spoons of CARPYZ TaC type.
- Figure 5 shows a front view of a turbo inlet + impeller + peripheral chamber impeller.
- Figure 6 shows a rear view of a wheel with a peripheral circular slot and for example a tube that starts from the center, passes into a blade and ended on the slot.
- Figure 7 shows a partial view of a wheel and the inlet of the inner duct of a blade.
- Figure 8 shows a partial view of a circular slot wheel with slot and blade entries.
- Figure 9 shows a partial view of the output of the fixed wheel with the rotating fluid.
- Figure 10 shows a partial view of a bucket turbine which receives the fluid which rotates it.
- FIG. 1 shows a half-thruster cut at its axis constructed according to the present application or is represented by 3 large hollow arrows the direction of the central fluid flow generated in the center by the propeller 1 which then passes between the profiled radial blades of the wheel fixed 2 which solidarises the fixed chamber (D) to the stators of the electric motor SME and the electricity generator SGE. Then the force of the flow is increased by the central helix of the bucket wheel or spoon 3.
- Figures 1 and 2 show the THRA wheel which takes the ambient fluid 12 in the center front (A), which is then led p1 in the hollow blades of the propeller B and ends in the circular chamber C which projects it into the fixed chamber D which rotates it by introducing it into the chamber E with the energy fluid coming from outside the casing 16 and which is then pushed back into the chamber F which makes it turn and sends it into the buckets of the bucket wheel or the spoons of the spinner wheel G which rotates and the fluid continues in the fixed chamber H which rectifies it before its exit from the thruster towards the rear 20.
- Figures 1 and 2 show in the center the motor shaft X1 integral with the rotor of the engine RME which is extended after the motor with a diameter adapted to receive a bearing bushing L which is contained in the tube of the hollow shaft X2 of the rotor of the electricity generator which is prolonged after the generator and then receives a disk D2.
- the extended shaft of the engine then also receives a disk D1 which when desired is clamped 22 with that of the generator allows to join the rotation of the two shafts on demand.
- FIG. 2 shows that the supply of the fuel sprayed into the chamber D comes from the circular chamber C P2 which receives it by tubes which pass into the inside of the hollow blades B of the propeller of the wheel THRA which are fed with the shaft 21 of the engine pierced for, which receives it by tubes which are integrated in the radial blades 2 and are fed 19 through the fixed chamber D and the housing.
- the thruster casing is flared CA2 or narrowed rearwardly in order to adapt the usable surface required by the buckets or spoons G.
- FIG. 4 shows the arrangement used for the spoon or spoon wheel G to rotate the motor shaft X3 integral with the EGR rotor of an electricity generator whose SGE stator is connected and fixed to the outside of the generator. the fixed room E.
- Figure 3 shows the arrangement used for the spinner wheel G spins X3 shaft in a bearing L whose fixed ring is connected 11 and fixed inside the fixed chamber E.
- FIG. 1 also shows a wheel V provided with independent profiled radial blades interposed, mounted on pivots between the chamber D and the stator of the engine SME whose blades are adjustable by a rod 14.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
- Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Description
Claims
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| LU100192A LU100192B1 (fr) | 2017-05-04 | 2017-05-04 | Procédé de construction de propulseurs ou de moteurs contenus dans un carter cylindrique |
| PCT/EP2018/061255 WO2018202738A1 (fr) | 2017-05-04 | 2018-05-03 | Procede de construction de propulseurs ou de moteurs contenus dans un carter cylindrique et propulseur ou moteur associé |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| EP3619402A1 true EP3619402A1 (fr) | 2020-03-11 |
Family
ID=59014696
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP18722475.3A Withdrawn EP3619402A1 (fr) | 2017-05-04 | 2018-05-03 | Procede de construction de propulseurs ou de moteurs contenus dans un carter cylindrique et propulseur ou moteur associé |
Country Status (11)
| Country | Link |
|---|---|
| US (1) | US20200325779A1 (fr) |
| EP (1) | EP3619402A1 (fr) |
| JP (1) | JP2020520429A (fr) |
| CN (1) | CN110770414A (fr) |
| AU (1) | AU2018262592A1 (fr) |
| BR (1) | BR112019023155A2 (fr) |
| CA (1) | CA3062227A1 (fr) |
| LU (1) | LU100192B1 (fr) |
| RU (1) | RU2019139105A (fr) |
| WO (1) | WO2018202738A1 (fr) |
| ZA (1) | ZA201907677B (fr) |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2629142A1 (fr) * | 1988-03-24 | 1989-09-29 | Carrouset Pierre | Machine rotative a deplacement non positif utilisable comme pompe, compresseur, propulseur ou turbine motrice |
| US20030192303A1 (en) * | 2002-04-15 | 2003-10-16 | Paul Marius A. | Integrated bypass turbojet engines for aircraft and other vehicles |
| US20060086078A1 (en) * | 2004-10-21 | 2006-04-27 | Paul Marius A | Universal Carnot propulsion systems for turbo rocketry |
| DE102008017844A1 (de) * | 2008-04-08 | 2009-10-15 | Rolls-Royce Deutschland Ltd & Co Kg | Strömungsmaschine mit Fluid-Injektorbaugruppe |
| FR2935429B1 (fr) * | 2008-08-26 | 2011-11-25 | Snecma | Aubage fixe de turbomachine a masse reduite et turbomachine comportant au moins un tel aubage fixe |
| CN102434218B (zh) * | 2011-11-27 | 2014-04-23 | 王政玉 | 一种流体涡轮发动机 |
| FR2997460B1 (fr) | 2012-10-29 | 2014-11-28 | Carpyz | Turbine comportant au moins 2 roues 3d creuse emboitees l'une dans l'autre |
| FR3031551A1 (fr) | 2015-01-09 | 2016-07-15 | Carpyz Ingenierie | Methode de conception et construction de roues turbos, helicos, reacteurs, alimentees |
-
2017
- 2017-05-04 LU LU100192A patent/LU100192B1/fr active IP Right Grant
-
2018
- 2018-05-03 US US16/610,455 patent/US20200325779A1/en not_active Abandoned
- 2018-05-03 BR BR112019023155-2A patent/BR112019023155A2/pt not_active Application Discontinuation
- 2018-05-03 EP EP18722475.3A patent/EP3619402A1/fr not_active Withdrawn
- 2018-05-03 RU RU2019139105A patent/RU2019139105A/ru unknown
- 2018-05-03 AU AU2018262592A patent/AU2018262592A1/en not_active Abandoned
- 2018-05-03 CN CN201880040435.5A patent/CN110770414A/zh active Pending
- 2018-05-03 CA CA3062227A patent/CA3062227A1/fr not_active Abandoned
- 2018-05-03 WO PCT/EP2018/061255 patent/WO2018202738A1/fr not_active Ceased
- 2018-05-03 JP JP2019560095A patent/JP2020520429A/ja active Pending
-
2019
- 2019-11-20 ZA ZA2019/07677A patent/ZA201907677B/en unknown
Also Published As
| Publication number | Publication date |
|---|---|
| LU100192B1 (fr) | 2018-11-05 |
| US20200325779A1 (en) | 2020-10-15 |
| RU2019139105A3 (fr) | 2021-10-21 |
| RU2019139105A (ru) | 2021-06-04 |
| JP2020520429A (ja) | 2020-07-09 |
| BR112019023155A2 (pt) | 2020-06-02 |
| WO2018202738A1 (fr) | 2018-11-08 |
| ZA201907677B (en) | 2020-10-28 |
| CA3062227A1 (fr) | 2018-11-08 |
| AU2018262592A1 (en) | 2019-12-12 |
| CN110770414A (zh) | 2020-02-07 |
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