WO2023180591A1 - Turbina impulsada por explosiones de hidrógeno o un hidrocarburo y vacío por precipitación acuosa - Google Patents
Turbina impulsada por explosiones de hidrógeno o un hidrocarburo y vacío por precipitación acuosa Download PDFInfo
- Publication number
- WO2023180591A1 WO2023180591A1 PCT/ES2022/070714 ES2022070714W WO2023180591A1 WO 2023180591 A1 WO2023180591 A1 WO 2023180591A1 ES 2022070714 W ES2022070714 W ES 2022070714W WO 2023180591 A1 WO2023180591 A1 WO 2023180591A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- suction
- injection
- tank
- drive
- joint
- 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.)
- Ceased
Links
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
- F01D1/34—Non-positive-displacement machines or engines, e.g. steam turbines characterised by non-bladed rotor, e.g. with drilled holes
-
- 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
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
- F02C3/22—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products the fuel or oxidant being gaseous at standard temperature and pressure
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C5/00—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
- F02C5/12—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the combustion chambers having inlet or outlet valves, e.g. Holzwarth gas-turbine plants
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/22—Fuel supply systems
- F02C7/232—Fuel valves; Draining valves or systems
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/48—Control of fuel supply conjointly with another control of the plant
- F02C9/50—Control of fuel supply conjointly with another control of the plant with control of working fluid flow
Definitions
- the device proposed here is a high-performance turbine with a great reduction in carbon emissions into the atmosphere, in case of burning a hydrocarbon fluid, or completely eliminating such waste if it is done with pure hydrogen; In addition, by never consuming atmospheric air, the production of polluting residues derived from the nitrogen that is part of said gas mixture is avoided, which means obtaining an optimal motive source capable of relieving nature of much or all of the damage it causes. Our mobility entails it.
- the device claimed here does not currently exist, so I request that you grant me the rights corresponding to the device that is described below in a practical case of industrial application, which is reinforced in its understanding with a series of schematic figures that represent it; In all of them, the lines with a dash followed by a dot indicate the hollowness of the space on which they are drawn and those with a discontinuous line indicate that the part thus reflected is hidden in that view.
- the device collected here is made up of three elements, connected in line by separate conduits whose respective links are sealed with the outside:
- a vacuum cleaner hereinafter known as.
- Figure 1 shows the profile of a rigid, compact, pressure and temperature resistant element, which is designated with the number 30; We know it as an impeller and in it (30) the following are opened:
- the oxygen tank (31) communicates with the outside, for eventual recharging, through a cylindrical conduit that has a spherical cavity in its middle part; We call this step oxygen loading and it is detailed with the number 39.
- Said tank (32) has a spherical opening reflected with the number 35.
- the number 37 indicates the combustion chamber of the material coming from the mixing chamber (33);
- the external walls of the combustion chamber (37) are suitable for radiating a large amount of heat to the surrounding medium.
- the combustion chamber (37) has a cylindrical cavity marked with the number 36 and another hexagonal one detailed with the number 40.
- Figure 2 shows the top view of the diametrically horizontal section of a container, which is similar in its geometric constitution to those of the hydraulic transmission system mentioned above, which we generically call casing; It includes, with the anagram 0, a rigid, dense cylindrical container resistant to high temperature and pressure; Its geometry is characterized by having: * Three equal protuberances, of which only two hidden views appear here, pierced by separate threaded cylindrical holes generically called hitch, under the respective designation 4 and 5.
- a cylindrical concavity generally called a sinus, opens in one of the bases of the casing, which is shown with notation 9.
- a cylindrical conduit represented under the sign 2, which we generically call a counter, communicates perpendicularly to the sinus (9) with the opposite base of the casing (0).
- the following semitoroidal ducts are reflected, open to different diameters on the circular surface of the sinus (9): • With the anagrams 7i and 7/, the upper and lower slopes respectively of the channel that we generally know as a major static joint.
- Figure 3 is the elevation drawing of a casing seen from the right side of the previous representation, of which it repeats the terminology, adding an upper protuberance, equal to the previous ones and also crossed by a new hitch, now with designation 3.
- Figure 4 shows an elevation view of a rigid, compact cylindrical piece resistant to high temperature and pressure detailed with the number 10, which we will call the driving rotor.
- the same (10) is identical to its analogue in the transmission system patent, unlike the fact that here it only has one turbine with its two isolation channels and not three with their respective sealing means as it does in that patent.
- a central hexagonal channel which we will call the power intake reflected with the number 16, communicates orthogonally in a coaxial manner both bases of the drive rotor (10).
- the drive rotor (10) is passed from base to base obliquely through a concentric series of holes, whose separating blades we will know as the motor turbine; of which we can see its upper openings identified with the anagram 14i, lower openings with the number 14 2 and the right quadrangular with the number 14 3 .
- a cylindrical hole that communicates perpendicularly the two bases of the drive rotor (10), which we call the drive counter, is indicated with the sign 15.
- Figure 5 is the profile of the drive rotor in which the designations of the previous figure are repeated, but particularizing here as follows:
- the 11' is made with what is known as the suction motor bearing channel.
- Figure 6 shows the profile of a rigid, compact element resistant to pressure and temperature marked with the number 50; We know it as a vacuum cleaner and in it (50) the following are opened:
- the number 53 indicates the exhaust tank.
- Figure 57 details the spherical hole that connects the exhaust tank (53) with the outside, which we call the remnant duct.
- the spherical hole that constitutes the suction conduit is designated with the number 59 and opens to the vacuum tank (51) to the outside.
- the vacuum tank (51) and the liquid water tank (52) communicate with each other through the spherical opening, which we know as the purge outlet, marked as 54; which (54) also opens to the outside through a cylindrical hole. »/
- a conduit of the same geometry opens with a spherical opening near its upper end; channel, which connects the latter (52) with the exhaust tank (53) and which we call the pressure connection designated with the number 55.
- Figure 7 represents the partial profile view of the electrical circuit installed in the present system since the figure only includes, with designation 61, an electric battery represented with the signs + and - and, under number 60, an electronic digital control which we call control; This (60) is connected to this (61) and to all the electrical components that make up the system by means of separate circuits that are sectioned here and will be detailed below.
- Figure 8 shows the profile of a section of the electrical ignition circuit, which we call the spark plug, shown as 80.
- Figure 9 shows the longitudinal section of a dense conduit, resistant to pressure and temperature, capable of radiating this towards the surrounding medium and which can be either rigid or flexible at will, which we call the injector under designation 47.
- Figure 10 shows the longitudinal section of a tee duct, dense, resistant to pressure and temperature that can be either rigid or flexible at will, which we call exhaust under designation 48.
- Figure 11 describes a thyme that, here under sign 70, will be known as a ligation.
- Figure 12 is the diametral cut of a tonca joint generally designated with the logo 45 since there will be different diameters as will be detailed.
- Figure 13 represents the side view of a rigid sphere polished on its surface, with the same diameter as all the bearing grooves present in the invention, which under the name bearing is designated with the number 41.
- Figure 14 shows with sign 42. the diametrical cut of a rigid sphere polished on its surface, opened diametrically by a straight cylindrical conduit of a certain radius; It is a rotary closing solenoid valve that we will generally know as management valve.
- Figure 15 specifies with sign 43 the diametral cut of a rigid sphere polished on its surface; Its body is opened diametrically by a square cylindrical conduit of a certain radius; It is a rotary closure solenoid valve that we will generally know as a purge management valve.
- Figure 16 represents, with the number 44, the profile of a manometer.
- Figure 17 shows the profile of an electronic level that incorporates a float attached to a rod.
- a photoelectric sensor is drawn in figure 18 under symbol 71; It (71) is connected to the electrical circuit, here present in a section, which connects it to the control (60).
- FIG 19 a light appears, which we call under designation 72; It (72) is connected to the electrical circuit, here present in a section, which connects it to the control (60).
- Figure 20 shows the assembly of all the system components detailed so far.
- the respective sinuses (9) of both casings (0 and 0') contain the drive rotor 5 (10), which details its power take-off (16), a compartment for the motor turbine 14i and the drive counter (15). ).
- 411 and 413 represent spheres that make up the collapsing series of bearings located in the injection motor bearing channel (11).
- 1544i represents the oxygen tank manometer (31).
- 44 3 indicates the pressure gauge located in the combustion chamber (37).
- 44 4 represents the vacuum manometer (51).
- 42i represents the solenoid valve installed in the upper duct (35) which we call oxygen management.
- 2542 2 indicates the solenoid valve installed in the spherical opening of the lower duct (36), which we call fuel management.
- 42 4 represents the solenoid valve installed in the injection duct (38), 30 being called the injection management valve.
- 42 8 indicates the solenoid valve installed in the spherical opening of the carryover duct (57), which we know as the carryover management valve.
- 42 9 indicates the solenoid valve installed in the spherical opening of the suction duct (59) called the suction management solenoid valve. 42 represents the solenoid valve installed in the spherical opening of the spray conduit (56) called spray management.
- 42i2 presents the solenoid valve installed in the spherical opening of the drain conduit (58) known as the drain management valve.
- 42u indicates the solenoid valve installed in the fuel charging passage (40) known as the fuel charging solenoid valve.
- 45i indicates the lower slope of the larger injection joint.
- 45 2 indicates the smaller injection joint on the lower side.
- 45i' indicates the lower slope of the larger suction joint.
- the sign 43 indicates the solenoid valve, called purge, installed in the purge pipe (54).
- the battery (61) maintains electrical communication with the control (60), which shows a series of sections of electrical circuits coming out of it (60), which connect, each one of them in particular with a solenoid valve (42 n ), level (46 n ), pressure gauge ((44 n ) or spark plug (80) either receiving information from them or managing their action.
- the oxygen (31) and fuel (32) tanks are filled by connecting to their respective oxygen loading steps (39) and fuel (40) from respective supply sources, which are filled at the load pressure. maximum, under direction of the control (60) that carries out the opening and closing of the respective oxygen supply electro valves (42) and fuel (42I 4 ), in order to achieve said objective.
- the precision of said gaseous supplies is determined thanks to the analysis in the control (60) of the variation of pressures existing in the oxygen tank (31) and the fuel tank (32) recorded by their respective manometers (44i) and (44 2 ).
- the control (60) sends an electrical pulse to the spark plug (80) that ignites the aforementioned gas mixture; which produces, in the event of a hydrogen explosion, pure water vapor and, if it is hydrogenated hydrocarbon, also said vapor with a minor addition of carbon monoxide and carbon dioxide.
- control (60) opens the intermediate management solenoid valve (42 3 ) so that the product of the previous reaction flows into the expansion chamber (33), where the pressure gauge ( 44 3 ) of said chamber (33 ) communicates to the control (60) the rise in pressure reached, with which it (60) closes the intermediate management solenoid valve (42 3 ) once the density of the gas housed in the combustion chamber (34) has decreased to the adequate level for its gaseous refeeding by repetition of the supply cycle detailed above, thus starting the driving part of the engine that concerns us here.
- the injection management solenoid valve (42 4 ) is opened during the required engine actuation time, to a greater or lesser extent, as requested further. or less power, passing the product of the explosions through the injection duct (47), from which it impacts with the blade of the engine turbine (28) that is located in its path, thus exerting its pressure on the contact surface between the two, creating a depression on the opposite face of said vane, which gives powerful rotation to the drive rotor (20), subsequently dividing the water vapor its path inside the suction conduit (48) towards the vacuum tank (51) and exhaust tank (53); traffic that is regulated by the control based on the values offered by the pressure gauges vacuum (44 4 ) and exhaust (44 6 ) operating the suction management solenoid valves (42 9 ) and remnant (42 8 ).
- the purge valve (43) which is, as shown in figure 20, making room for the arriving water but, due to its absence, communication of this liquid with any other space, the level of the vacuum tank (46i) communicates to the control (60) the overflow of the capacity of said valve (43), and this (60) is responsible for transferring that liquid to the tank of liquid water (52) ordering it (43) to rotate 270 degrees hourly, with which the water falls into the liquid water tank (52) by acquiring atmospheric air from its other end, now open to the outside through the purge conduit (54) after which the purge valve (43) returns to its original position by order of the control (60).
- the level of the liquid water tank (46 2 ) indicates the amount of water that said container (52) occupies, data that is communicated to the control (60) for the purpose of emptying it when exceeding a certain volume, which will be carried out by opening the drain management valve (42I 2 ) towards the outside to close it after the water level has dropped to the amount desired by the driver.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Fluid Mechanics (AREA)
- Physics & Mathematics (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
- Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
- Measuring Volume Flow (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Abstract
Description
Claims
Priority Applications (5)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US18/832,552 US20250137402A1 (en) | 2022-03-23 | 2022-11-08 | Turbine driven by confrontation of explosions of oxygen and hydrogen, or any hydrogenated hydrocarbon, under pressure and vacuum by aqueous precipitation of the resulting water vapor |
| JP2024539624A JP2025509027A (ja) | 2022-03-23 | 2022-11-08 | 酸素および水素、または任意の水素化炭化水素の爆発を、圧力下で衝突させ、得られた水蒸気の水性沈殿による真空により駆動するタービン |
| EP22933222.6A EP4497912A4 (en) | 2022-03-23 | 2022-11-08 | TURBINE DRIVEN BY EXPLOSIONS OF HYDROGEN OR HYDROCARBON AND VACUUM BY AQUEOUS PRECIPITATION |
| AU2022449269A AU2022449269A1 (en) | 2022-03-23 | 2022-11-08 | Turbine driven by of hydrogen or a hydrocarbon and vacuum by aqueous precipitation |
| CA3242436A CA3242436A1 (en) | 2022-03-23 | 2022-11-08 | Turbine driven by confrontation of explosions of oxygen and hydrogen, or any hydrogenated hydrocarbon, under pressure and vacuum by aqueous precipitation of the resulting water vapor |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| ES202230254A ES2923449B2 (es) | 2022-03-23 | 2022-03-23 | Turbina de explosion de oxigeno e hidrogeno o cualquier hidrocarburo hidrogenado y condensacion acuosa del vapor de agua resultante |
| ESP202230254 | 2022-03-23 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| WO2023180591A1 true WO2023180591A1 (es) | 2023-09-28 |
Family
ID=83361365
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/ES2022/070714 Ceased WO2023180591A1 (es) | 2022-03-23 | 2022-11-08 | Turbina impulsada por explosiones de hidrógeno o un hidrocarburo y vacío por precipitación acuosa |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US20250137402A1 (es) |
| EP (1) | EP4497912A4 (es) |
| JP (1) | JP2025509027A (es) |
| AU (1) | AU2022449269A1 (es) |
| CA (1) | CA3242436A1 (es) |
| ES (1) | ES2923449B2 (es) |
| WO (1) | WO2023180591A1 (es) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| AU2022454520A1 (en) * | 2022-04-18 | 2024-07-18 | Sebastián Enrique Bendito Vallori | Electromagnetically controlled hydraulic transmission system with gears for vehicles, with optional electrical generation and propulsion |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1658422A1 (fr) | 2004-06-18 | 2006-05-24 | Claude-Louis Adam | Moteur torique de revolution |
| US20130239920A1 (en) | 2011-05-06 | 2013-09-19 | Lawrence McMillan | Rotary energy transducer |
| US20200318538A1 (en) | 2017-08-02 | 2020-10-08 | Tascosa Advanced Services, Inc. | Hydrogen Hybrid Cycle System |
| ES2857423A2 (es) | 2021-04-21 | 2021-09-28 | Bendito Vallori Sebastian Enrique | Sistema hidráulico de trasmisión con desarrollos por control electromagnético para vehículos, con generación y propulsión eléctrica discrecional |
Family Cites Families (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3459953A (en) * | 1967-03-20 | 1969-08-05 | Univ Oklahoma State | Energy storage system |
| GB1213551A (en) * | 1968-06-14 | 1970-11-25 | Rolls Royce | Improvements relating to detonation wave combustion |
| BE790403A (fr) * | 1971-10-21 | 1973-04-20 | Gen Power Corp | Turbo-compresseur integral a onde |
| US3750395A (en) * | 1971-10-22 | 1973-08-07 | Westinghouse Electric Corp | Overspeed protection system for a turbo-generator unit |
| US4620414A (en) * | 1983-07-27 | 1986-11-04 | Dieter Christ | Gas turbine engine |
| JPH0665053B2 (ja) * | 1985-04-22 | 1994-08-22 | 株式会社日立製作所 | 燃料電池システム |
| CA2604610C (fr) * | 2007-11-05 | 2015-03-31 | Nabil H. Frangie | Machine hydroelectrique |
| US8671687B2 (en) * | 2011-02-18 | 2014-03-18 | Chris Gudmundson | Hydrogen based combined steam cycle apparatus |
| WO2015159956A1 (ja) * | 2014-04-18 | 2015-10-22 | 大石 光江 | 燃焼ガスを駆動力として噴出するエンジン |
| EP3056820B1 (en) * | 2015-02-11 | 2019-03-13 | Rolls-Royce North American Technologies, Inc. | Wave rotors with temperature control features |
| JP6815415B2 (ja) * | 2016-11-25 | 2021-01-20 | 株式会社Ihi | 再生型燃料電池システム及び水電解システム |
| US20210003072A1 (en) * | 2018-12-04 | 2021-01-07 | Look For The Power, Llc | Rotary internal combustion engine |
| US11635022B1 (en) * | 2022-02-11 | 2023-04-25 | Raytheon Technologies Corporation | Reducing contrails from an aircraft powerplant |
-
2022
- 2022-03-23 ES ES202230254A patent/ES2923449B2/es active Active
- 2022-11-08 CA CA3242436A patent/CA3242436A1/en active Pending
- 2022-11-08 JP JP2024539624A patent/JP2025509027A/ja active Pending
- 2022-11-08 AU AU2022449269A patent/AU2022449269A1/en active Pending
- 2022-11-08 WO PCT/ES2022/070714 patent/WO2023180591A1/es not_active Ceased
- 2022-11-08 EP EP22933222.6A patent/EP4497912A4/en active Pending
- 2022-11-08 US US18/832,552 patent/US20250137402A1/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1658422A1 (fr) | 2004-06-18 | 2006-05-24 | Claude-Louis Adam | Moteur torique de revolution |
| US20130239920A1 (en) | 2011-05-06 | 2013-09-19 | Lawrence McMillan | Rotary energy transducer |
| US20200318538A1 (en) | 2017-08-02 | 2020-10-08 | Tascosa Advanced Services, Inc. | Hydrogen Hybrid Cycle System |
| ES2857423A2 (es) | 2021-04-21 | 2021-09-28 | Bendito Vallori Sebastian Enrique | Sistema hidráulico de trasmisión con desarrollos por control electromagnético para vehículos, con generación y propulsión eléctrica discrecional |
Non-Patent Citations (1)
| Title |
|---|
| See also references of EP4497912A4 |
Also Published As
| Publication number | Publication date |
|---|---|
| US20250137402A1 (en) | 2025-05-01 |
| AU2022449269A1 (en) | 2024-07-04 |
| ES2923449R1 (es) | 2023-01-25 |
| ES2923449B2 (es) | 2024-03-20 |
| EP4497912A1 (en) | 2025-01-29 |
| CA3242436A1 (en) | 2023-09-28 |
| JP2025509027A (ja) | 2025-04-11 |
| EP4497912A4 (en) | 2026-01-28 |
| ES2923449A2 (es) | 2022-09-27 |
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