Integration method

Abstract

To integrate a large number of propulsion force generating devices accompanied by an air current as reaction in a propulsion force direction while avoiding the air current.SOLUTION: In one embodiment of the present invention, a centrifugal force is applied to the air flow in a direction perpendicular to the direction of the propulsive force, and the path of the air flow is controlled so that the air flow does not hit other components of the stack. As a propulsive force generating device, there is a technique for obtaining a propulsive force by breaking the balance of atmospheric pressure in the device by diffraction of gas molecules derived from the wave nature of matter waves based on the quantum theory. Since this technology is in the field of fine technology including nano-technology, the device size is small, and it is necessary to integrate a large number of devices in order to obtain a practical driving force. A practical propulsion force can be obtained by the accumulation method of the present invention.SELECTED DRAWING: Figure 18

Description

[Technical Field]

[0001] The present invention relates to a method for integrating a propulsion generating device that uses an airflow as a reaction force. The present invention also relates to a propulsion device integrated using the integration method and various applied technologies incorporating the same. With regard to the propulsion generating device, the present invention can be related to the utilization of a technology that generates anisotropic pressure on an object by utilizing the properties of matter waves (de Broglie waves) of oxygen molecules and nitrogen molecules in the air, thereby obtaining propulsion. [Background technology]

[0002] Technologies have been proposed that use the diffraction properties of matter waves from oxygen and nitrogen molecules in the air to disrupt the balance of atmospheric pressure on a device and generate propulsive force (Patent Documents 1 to 3 and 5 to 8). Patent Document 4 also proposes a technology that uses water surface waves instead of matter waves to generate propulsive force for ships. Both technologies involve the generation of airflow (in Patent Document 4, water surface waves generated as a reaction) as a reaction to the propulsive force generated. For this reason, when devices are stacked in the direction of the propulsive force, the reactive airflow hits the other devices that make up the stack, which poses a problem of reducing the propulsive force obtained. [Prior art documents] [Patent documents]

[0003] [Patent Document 1] Japanese Patent Application Laid-Open No. 2009-270578 [Patent Document 2] Japanese Patent Application Laid-Open No. 2009-019264 [Patent Document 3] Japanese Patent Application Laid-Open No. 2010-053869 [Patent Document 4] JP 2010-089781 A [Patent Document 5] Japanese Patent Application Laid-Open No. 2010-096186 [Patent Document 6] Japanese Patent Application Laid-Open No. 2010-101323 [Patent Document 7] Japanese Patent Application Laid-Open No. 2011-202650 [Patent Document 8] Japanese Patent Publication No. 2021-067181 Summary of the Invention [Problem to be solved by the invention]

[0004] In a thrust generating device that generates a reactive airflow, if such devices are stacked in the direction of the thrust, the reactive airflow will hit the other components that make up the stack, reducing the thrust obtained by the entire system. The objective of the present invention is to control the path of the airflow and reduce the amount of air hitting the other components. [Means for solving the problem]

[0005] The present invention is a method for integrating propulsion generating devices that generate an airflow as a reaction, by controlling the path of the airflow by centrifugal force and reducing the amount of the airflow that strikes other components that make up the assembly. As a typical example, a cylindrical tubular structure is prepared, and its depth direction is aligned with the direction of the airflow.

[0006] The airflow is caused to flow within the tubular structure while rotating along the circumference of the inner wall. Note that this is merely a typical example, and the rotation vector of the rotational motion is parallel to the flow of the airflow. This means that the rotating motion is not a force that changes the momentum of the airflow in the flow direction. Meanwhile, centrifugal force acts on the airflow, forcing it to rotate while being pressed against the inner wall of the tubular structure, and it flows in the depth direction of the tubular structure. In other words, centrifugal force can limit the path of the airflow to the vicinity of the inner wall of the tubular structure. Furthermore, the stronger the rotational motion, the smaller the area occupied by the airflow on the cross section of the tubular structure (due to centrifugal force). Using this method, the airflow can be guided to a path that is less likely to hit other components of the assembly, allowing it to be exhausted outside the assembly. As a result, the propulsive force obtained by the entire assembly can be maximized.

[0007] However, oxygen and nitrogen molecules that make up air behave as electromagnetically neutral molecules, making it difficult to use electromagnetic force to control their paths. The present invention has the technical advantage of using centrifugal force for path control.

[0008] In one embodiment of the integration method of the present invention, a technology is proposed for the propulsion generating device, which uses the wave properties of quantum mechanical matter waves (de Broglie waves) of oxygen and nitrogen molecules (hereinafter referred to as "air molecules") that make up air to disrupt the balance of atmospheric pressure acting on the device, thereby obtaining propulsion. This technology for obtaining propulsion using quantum mechanical properties is implemented on a microscopic scale, such as nanotechnology or picotechnology. Therefore, in order to obtain propulsion of a practical magnitude, device integration is essential, which is highly compatible with the integration method of the present invention. Therefore, an invention that combines these two is proposed. [Effects of the Invention]

[0009] The assembly obtained by this invention essentially uses atmospheric pressure to obtain propulsion, so it can be used not only on the ground but also in the sky, as long as it is in the air. This will accelerate humanity's advance into the sky and make it easier to escape into outer space. Furthermore, depending on the configuration, the energy source can be limited to atmospheric pressure alone, making it the ultimate energy-saving technology. It has the potential to not only curb global warming, but also lead to global cooling. Furthermore, there are few material restrictions when it comes to implementation, making it an ideal technology for Japan, a country with limited resources. [Brief explanation of the drawings]

[0010] [Figure 1] FIG. 1 is an explanatory diagram illustrating the invention described in claim 1 or 2 by way of a specific example. [Figure 2] FIG. 10 is an explanatory diagram illustrating the invention described in claim 3. [Figure 3] 1 is a diagram illustrating an embodiment of the invention described in claim 4, 9 or 10. FIG. [Figure 4] 1 is a diagram illustrating an embodiment of the invention described in claims 5 to 8, 11, and 12.

[0033] FIG. [Figure 5] FIG. 5 is a supplementary view to FIG. 4, illustrating the positional relationship of the first opening portion. [Figure 6] 5, this is a supplementary view to FIG. 4, and is a view for explaining the positional relationship of the first opening portion. [Figure 7] FIG. 6 is a diagram supplementing FIG. 5 and showing the positional relationship of the second opening portion. [Figure 8] 1 is a diagram for explaining an embodiment of the invention as set forth in claims 5 to 8, 11, and 12. It is also a diagram for explaining an embodiment of the invention as set forth in claim 13 or 14. [Figure 9] 1 is an explanatory diagram illustrating an embodiment of the invention according to claim 16 or 17.

[0033] FIG. [Figure 10] FIG. 2 is an explanatory diagram illustrating an embodiment of a first centrifugal force generating device. [Figure 11] FIG. 2 is an explanatory diagram illustrating an embodiment of a first centrifugal force generating device. [Figure 12] FIG. 2 is a diagram showing an example of the configuration of a second stack. [Figure 13] FIG. 10 is a diagram showing an example of the configuration of the second stack, particularly illustrating the support columns that support rotation. [Figure 14] This shows one embodiment of the invention described in claim 18. [Figure 15] 15 is a cross-sectional view of the second stack in the embodiment shown in FIG. 14. [Figure 16] As an embodiment of the invention described in claim 18, a configuration utilizing magnetic charges is shown. [Figure 17] As an embodiment of the invention described in claim 18, a configuration utilizing electric charge is shown. [Figure 18] FIG. 1 is an explanatory diagram for explaining an outline and an overall picture of the present invention. [Figure 19] 10 is an explanatory diagram illustrating a mechanism for generating a thrust force based on the principles of quantum mechanics in the inventions described in claims 19 to 33. FIG. [Figure 20] FIG. 20 is a diagram illustrating a configuration in which a boarding space is provided as an example in the invention described in claim 18. DETAILED DESCRIPTION OF THE INVENTION

[0011] Hereinafter, a mode for carrying out the invention according to the present application (hereinafter referred to as "embodiment") will be described with reference to the drawings. Note that the invention according to the present application is not limited to this embodiment. Furthermore, in the following embodiment, the same components are given the same reference numerals, and duplicated explanations will be omitted.

[0012] FIG. 1 shows one embodiment of the invention described in claim 1 or 2, and is an example in which two devices are integrated to generate an airflow and obtain a first propulsive force as a reaction to the airflow. The direction of integration is the first direction, and the integrated body is the first integrated body. As shown in FIG. 1, the direction of the first propulsive force and the first direction form an angle θ, but the invention described in claim 1 corresponds to the case where θ<90°, and the invention described in claim 2 corresponds to the case where θ=0°.

[0013] If left unchecked, the reactive airflow from the upper device will hit the lower device, resulting in the resulting thrust of the entire first assembly being less than the sum of the individual first thrusts. Furthermore, because airflow behaves approximately as a neutral gas in the air, it is difficult to change the direction of the airflow using electromagnetic force to prevent it from hitting the lower device. The present invention uses centrifugal force to reduce the amount of airflow that hits other devices that make up the first assembly. As shown in the figure, by applying centrifugal force to the airflow in the right direction, the amount of airflow that hits the vertically adjacent device can be reduced.

[0014] FIG. 2 explains the meaning of the invention described in claim 3, and illustrates a first stack similar to that shown in FIG. 1. Since the first direction is the direction of stacking, in order to reduce the amount of reaction airflow generated in the upper device that strikes the lower device, it is most effective for the direction of centrifugal force to be perpendicular to the first direction. This figure illustrates this. The invention described in claim 3 proposes this configuration.

[0015] It may be considered more effective to apply centrifugal force in a direction that cancels the first directional component of the airflow. However, because the airflow is generated as a reaction to the first propulsive force, the centrifugal force generating body is subjected to this reaction. In this configuration, the total propulsive force obtained by the entire system, including the upper and lower devices as well as the centrifugal force generating body, is reduced. While this configuration is acceptable as an embodiment of the invention described in claim 1, it cannot be said to be the most effective.

[0016] Figure 3 is a diagram showing one embodiment of the invention described in claim 4, 9, or 10. In this figure, a specific configuration (two walls with slits facing each other) is shown as the configuration of the device that generates the first propulsive force, but this is merely an example, and any configuration may be used as long as the device generates an airflow as a reaction to the propulsive force. Furthermore, in this example, for simplicity, a configuration in which the entire system rotates is adopted, but in the invention described in claim 4, a configuration in which only the first plate-like member rotates and the first assembly does not rotate is also possible.

[0017] The downward airflow generated as a reaction to the upward first thrust is given a rotational angular velocity on the horizontal plane by the first plate-like member, and the direction is changed by centrifugal force, reducing the amount of the downward airflow that strikes the adjacent device below. The embodiment shown in the figure clarifies the role and significance of the first plate-like member in the present invention.

[0018] FIG. 4 is a diagram illustrating one embodiment of the invention described in any one of claims 5 to 8, 11, and 12. As with FIG. 3, in this example, the entire system is assumed to have a rotating disk structure, but for convenience of explanation, FIG. 4 shows its cross section. The disk is divided into layers at regular intervals of radius, and each layer is a first assembly. Here, the radial direction corresponds to the second direction described in claim 5, and the second assembly is formed in this direction.

[0019] Figures 5 and 6 show the first stack of Figure 4 further separated in the height direction, showing an example of the positional relationship of the first openings, and Figure 7 shows two adjacent first stacks, showing an example of the positional relationship of the second openings.

[0020] FIG. 8 illustrates the roles of the first opening and the second plate-like member. In FIG. 8, the rotation directions of the eleventh and twelfth stacks are opposite to each other. However, in this description, it is not necessary to distinguish whether the rotation directions are opposite or not; they may be the same. Centrifugal force acts on the airflow, and its path is drawn toward the second plate-like member. It is desirable to configure the airflow so that the centrifugal force continues as long as possible while it passes through the first stack. Due to the centrifugal force, the airflow moves downward along the second plate-like member. This path desirably overlaps with the first opening. The airflow passes through the first opening and exits the first stack from the bottom, avoiding the components of the first stack. Therefore, the effect of the airflow generated by the reaction hitting the components of the first stack and weakening the resultant propulsive force can be reduced. This is the significance of the technology proposed by claims 5 to 7.

[0021] The second opening proposed by the invention of claim 8 serves as a vent for feeding air from the atmosphere into the device that generates the first propulsive force. The device is located between the first and second openings, and the first opening is a path for exhausting the airflow generated by the reaction (the airflow caused by the reaction and that should be avoided from being taken into the device). On the other hand, air entering through the second opening, which is located closer to the center of the rotational motion than the device, is more likely to reach the device due to centrifugal force. The device is configured to generate propulsive force by taking in air entering from the top of the device and the second opening.

[0022] Furthermore, for structural reasons, a further first stack (referred to as the "tenth stack") is placed closer to the center of rotational movement than the second open section within the eleventh stack (if the eleventh stack rotates at the innermost position, there is no corresponding tenth stack). The airflow flowing through the first open section within this tenth stack is blocked by the second plate-like member of the tenth stack, and is prevented from reaching the eleventh stack.

[0023] The inventions described in claims 9 to 12 propose various patterns for rotating a system. The key to this invention is to rotate the airflow generated as a reaction, thereby exerting centrifugal force. If this goal can be achieved by rotating the first plate-like member, the other devices, parts, and components that make up the system do not necessarily need to be rotated. As will be described later, increasing the number of points in the system where rotation occurs can cause friction in the support parts that support the rotation, increase the intensity of electromagnetic waves, and increase energy loss. On the other hand, minimizing the number of rotating parts (for example, the second plate-like member can be configured to not rotate), can complicate the configuration by separating the rotating and non-rotating parts to minimize contact. It is important to implement the invention by using the rotating and non-rotating parts in different patterns as needed.

[0024] Continuing with reference to Figures 7 and 8, an embodiment of the invention according to claim 13 or 14 is shown. The figures show a case where the rotation directions (rotation vectors) are opposite. By reversing the rotation directions of the adjacent 11th and 12th aggregates, the torque of the entire system can be reduced.

[0025] In addition, if the rotation direction is to be reversed, it is possible to have a structure in which the rotation direction is reversed not between adjacent first aggregates that make up the second aggregate, but between distant first aggregates. The invention described in claim 15 proposes this configuration.

[0026] The inventions recited in claims 13 to 15 are examples that use disks (first aggregates) that rotate in opposite directions, and this configuration makes it possible to practically control the strength of the effective thrust obtained by the entire system. Specifically, if you want to weaken the effective thrust, you can simply cause the rotational motions of the disks that rotate in opposite directions to interfere with each other, thereby reducing the rotational angular velocity. In this respect, the inventions recited in claims 13 to 15 can be said to have a safe structure in the event of an abnormality.

[0027] Fig. 4 illustrates an embodiment of the first centrifugal force creating device claimed in claim 16. Fig. 10 and Fig. 11 show the structure of components obtained by further dividing each of the circular first aggregates in Fig. 4. In these figures, an example of the first centrifugal force creating device is shown.

[0028] 4, 10, and 11 are all located on the opposite side of the second plate-shaped member from the device that generates the first thrust (referred to as the "first positional relationship"). The first positional relationship is not necessarily required, and the first centrifugal force generating device may be located on the same side of the second plate-shaped member as the device that generates the first thrust.

[0029] The first positional relationship is a configuration proposed by the invention described in claim 17. In the invention described in claim 13 or 14, the invention described in claim 17 leads to an embodiment as shown in FIG. 9. FIG. 9 shows two adjacent stacks, the eleventh and twelfth stacks, which rotate in opposite directions. The first centrifugal force generating device of the eleventh stack generates an airflow in the opposite direction as a reaction to the thrust that generates the rotation. The airflow is emitted in the same direction as the rotation of the twelfth stack at a position adjacent to the second open portion of the twelfth stack. Therefore, due to the first positional relationship, the airflow promotes the rotational motion of the twelfth stack. Meanwhile, because the airflow is divided by the second plate-like member of the eleventh stack, the airflow does not interfere with the rotation of the air near the device that generates the first thrust of the eleventh stack.

[0030] The second assembly shown in FIG. 12 is based on the embodiments of the invention described above. Each of the constituent first assembly has a second plate-like member arranged thereon, which exhausts the reaction airflow of the first thrust force from the bottom of the system. However, the outermost first assembly within the second assembly does not necessarily have to exhaust the reaction airflow from the bottom of the system. In one embodiment, the outermost first assembly does not have the second plate-like member, and is structured to exhaust the airflow laterally.

[0031] In the example shown in Fig. 12, each of the first stacks having a circumferential structure rotates with a rotation vector normal to the circumferential surface, as an example. To prevent adjacent first stacks from contacting each other, in the embodiment shown in Fig. 13, supports are provided to support the rotation of each first stack.

[0032] On the other hand, in addition to the method of fixing the first assembly within the second assembly with supports, there is also a method using electromagnetic force. The invention described in claim 18 uses this method, and Figure 14 shows bird's-eye views of one embodiment from various angles, with the topmost view being a bird's-eye view from diagonally above. As the views progress, the views become more horizontal, and the bottommost view is a view from diagonally below. The second-lowest view is a view from an almost horizontal direction, and a cross-sectional view of the dotted line in the figure is shown separately in Figure 15.

[0033] The cross-sectional view in Figure 15 shows the system levitating due to the propulsive force derived from the present invention, as explained in the above-mentioned embodiments. It also shows the airflow, which is a reaction to the propulsive force, being expelled diagonally downward due to centrifugal force. The first assemblies constituting the second assembly are arranged so that adjacent first assemblies do not come into contact with each other due to electromagnetic repulsion, as proposed in claim 18. A typical example using magnetic repulsion is shown in Figure 16, and a typical example using charge repulsion is shown in Figure 17 (both Figures 16 and 17 are cross-sectional views. The detailed structure of the system is not depicted, and only the arrangement of the electromagnetic charges is simplified). In this embodiment, where the system structure is stabilized and maintained by electromagnetic force, the rotational motion of the electromagnetic charges accompanies the emission of electromagnetic waves (Figure 15 shows an example of the generated electromagnetic waves). This results in energy consumption to maintain the rotational motion (in the previously described support method, energy consumption occurs due to friction at the contact points of the support parts. Which method is preferable depends on the situation). It is also possible to use a structure that does not rotate the electromagnetic charge and does not generate electromagnetic waves, since the only purpose is to maintain the system configuration and prevent the first aggregates from coming into contact with each other. If a structure is used that does not rotate the electromagnetic charge, the electromagnetic waves will not be generated and the associated energy consumption will not occur.

[0034] Fig. 20 is a cross-sectional view of an example of a configuration with a boarding space in the invention described in claim 18. By utilizing electromagnetic repulsion, a usable structure can be placed on the center line of the disk.

[0035] The inventions described in claims 19 to 33 utilize the above-described integration method to obtain an assembly of a thrust generating device using prior art, which uses the diffraction properties of matter waves (de Broglie waves) of oxygen and nitrogen molecules in the air to disrupt the balance of atmospheric pressure and thereby generate thrust. The individual thrust generating devices are extremely small in size due to the use of nanotechnology and picotechnology. Therefore, it is essential to establish integration technology to generate thrust of practical magnitude, which is highly compatible with the integration method proposed by the present invention. For this reason, the scope of the present invention includes the application of the integration method to the thrust generating device. While the prior art is described in detail in Patent Documents 1 to 3 and 5 to 8, the configuration shown in Figure 19 will be described here as a representative example.

[0036] Figure 19 is an example of Figure 5, but shows an enlarged cross section of the first thrust generating section of one of the devices that generates the first thrust on the right side. In this example, the first thrust generating section employs a structure in which a wall with a single slit and a wall with a double slit are arranged so that the slits face each other and are connected (the cross-sectional drawing in this figure does not show the connection between the two walls, but the bird's-eye view on the left of the figure makes it clear that the two walls are connected). For simplicity, the example shows a case in which the width of the single slit and the combined width of the double slits are the same (even if these widths are different, the same thrust is generated). The two cross-sectional views in the upper right of the figure depict the behavior of matter waves when oxygen molecules and nitrogen molecules (hereinafter referred to as "air molecules"), which make up air, enter through the slits. The left cross-sectional view shows the case in which air molecules enter through the double slit, and the right cross-sectional view shows the case in which air molecules enter through the single slit.

[0037] Although it is illustrated in the cross-sectional view of FIG. 19, due to the wave nature, the diffraction effect is greater when incident from a double slit than when incident from a single slit. Therefore, for [A. the probability of exiting from the single slit without colliding with the inner wall even once when incident from the double slit] and [B. the probability of exiting from the double slit without colliding with the inner wall even once when incident from the single slit], A < B. On the other hand, due to the isotropy of atmospheric pressure, the number of air molecules incident from the single slit per unit time is equal to the number of air molecules incident from the double slit. Therefore, due to A < B, the balance of atmospheric pressure inside the device is disrupted. As a result, an upward propulsive force acts on the device, and as a reaction, an air current is generated downward (this state is illustrated in the lower part of the cross-sectional view of FIG. 19).

[0038] The quantum mechanical diffraction phenomenon can occur not only with slits but also with small holes. Therefore, an invention using holes instead of slits has also been proposed. Also, instead of the first propulsive force generating section, the propulsive force generating technology described here can be applied to the second propulsive force generating section. The invention according to claim 19 uses the propulsive technology utilizing the properties of matter waves described here to provide the first propulsive force, while the invention according to claim 20 uses the said propulsive technology to generate rotational motion.

[0039] The inventions according to claims 34 and 35 propose obtaining energy greater than the losses due to friction where the struts rub against each other and radiation of the electromagnetic waves, etc. from the atmosphere in the form of a propulsive force. With this invention, it becomes possible to extract effective energy from atmospheric heat.

[0040] The inventions according to claims 36 to 48 propose a configuration having technical elements necessary when implementing the invention of the above-described integration method, and forms of utilization of the propulsive force brought about by the invention of the above-described integration method. Since the content of these is self-evident, the description is omitted. <着

[0041] The above describes in detail the embodiments of the present application based on several drawings, but these are merely examples, and the present invention can be implemented in other forms that include the embodiments described in the Disclosure of the Invention section and that have been modified and improved in various ways based on the knowledge of those skilled in the art. [Industrial Applicability]

[0042] In addition to being a power source, it is expected that it will be used for floating transportation, floating housing, and atmospheric escape engines for spacecraft and powered elevators. It can also be used as a power generation technology that extracts energy from atmospheric heat. Humanity's sphere of activity will expand into the sky, making it possible to avoid earthquake damage. Wars and conflicts over land will decrease. The usable space per person will expand dramatically, and an explosive population growth is expected. [Explanation of symbols]

[0043] 10 equipment 20 First Cluster 30 First plate-shaped member 40 Second Cluster 50 second plate-shaped member 60 1st opening 70 2nd open part 80 11th Cluster 90 12th Cluster 100 First centrifugal force generating device 110 Post 120 air molecules 130 Matter waves of air molecules 140 Single Slit 150 Double Slit 160 boarding spaces

Claims

1. A device that generates an air current and obtains the primary thrust as a reaction to the air current. A method for obtaining a first aggregate by accumulating in a first direction that is not perpendicular to a first driving force direction, comprising: An accumulation method, characterized in that centrifugal force is applied to the airflow between adjacent devices that constitute a first accumulation body in a direction that is not parallel to the first direction.

2. The method of claim 1 , wherein the first direction is parallel to a first motive force direction.

3. 3. The method according to claim 1, wherein the direction of the centrifugal force is perpendicular to the first direction.

4. The accumulation method according to any one of claims 1 to 3, An accumulation method characterized by arranging a first plate-like member that rotates, capturing the reactive airflow with said plate configuration, and applying the centrifugal force to said airflow.

5. A method for obtaining a second stack by stacking the first stack in a second direction that is not perpendicular to the centrifugal force, in combination with the stacking method according to any one of claims 1 to 4, comprising: The second stack is characterized in that a plate-shaped second plate-shaped member is inserted between any adjacent first stacks in the second direction to separate the first stacks, Of the two first stacks adjacent to each other with the second plate-like member sandwiched between them, the one located on the side of the second plate-like member facing the direction of the centrifugal force is designated as a 12th stack, and the one located on the side facing the opposite direction to the centrifugal force is designated as an 11th stack, An accumulation method characterized in that a first open portion having an open structure incorporated therein is provided between the second plate-shaped member and the eleventh accumulation body.

6. 6. The method of claim 5, wherein the second direction is parallel to the centrifugal force.

7. The accumulation method according to claim 5 or 6, The accumulation method is characterized in that the first open portion has an open structure at a portion that overlaps with the airflow path.

8. The accumulation method according to any one of claims 5 to 7, An accumulation method characterized in that a second open portion incorporating an open structure is provided between the second plate-shaped member and the twelfth accumulation body.

9. The method of any one of claims 4 to 8, further comprising: An assembly method characterized in that the first plate-like member has a structure connected to the first assembly.

10. 10. The method of claim 9, further comprising: An accumulation method, characterized in that the first plate-like member and the first accumulation unit rotate together.

11. The accumulation method according to any one of claims 5 to 10, An assembly method characterized in that the second plate-like member has a structure connected to the first assembly.

12. The method of claim 11, further comprising: An accumulation method, characterized in that the first plate-like member, the first stack, and the second plate-like member rotate integrally.

13. The method of any one of claims 5 to 12, further comprising: a rotation vector (first vector) of a rotational motion that causes the centrifugal force that is brought about in the eleventh airflow, which is a reaction of the propulsive force acting on the eleventh accumulation; An accumulation method characterized in that the angle formed by the rotational vector (second vector) of the rotational motion that causes the centrifugal force on the 12th airflow, which is a reaction to the propulsive force acting on the 12th accumulation body, is greater than a right angle.

14. 14. The method of claim 13, wherein the first vector and the second vector are opposite in direction.

15. The method of any one of claims 5 to 12, further comprising: An accumulation method characterized in that in any two first accumulations that constitute a second accumulation, the rotation vectors of the rotational motion that causes centrifugal force on the airflow generated as a reaction to the first propulsion force are in opposite directions to each other.

16. 16. The method according to claim 4, wherein the rotational movement of the first plate-shaped member is An accumulation method characterized by being brought about by a first centrifugal force generating device that obtains a second propulsive force while accompanying a reactive airflow to propel the object.

17. 17. The method of claim 16, further comprising: An accumulation method characterized in that a first centrifugal force generating device that generates centrifugal force in the 11th airflow is arranged on the side of the 12th accumulation body, sandwiching the second plate-shaped member therebetween.

18. 18. The method of any one of claims 5 to 17, comprising: An assembly method characterized in that first assemblies adjacent to each other in the second direction are prevented from contacting each other by electromagnetic repulsion.

19. 19. The method of any one of claims 1 to 18, comprising: the first thrust is generated by disrupting the isotropy of atmospheric pressure acting on the first thrust generating unit in the device due to a diffraction phenomenon of gas molecules resulting from the wave nature of quantum mechanical matter waves; Accumulation method.

20. 20. The method of any one of claims 1 to 19, comprising: the second thrust is generated by disrupting the isotropy of atmospheric pressure acting on the second thrust generating unit due to a diffraction phenomenon of gas molecules resulting from the wave nature of quantum mechanical matter waves; Accumulation method.

21. 21. The method of claim 19 or 20, The first thrust generation unit or the second thrust generation unit includes: An accumulation method characterized by having a structure in which a first wall surface having N-fold slits (N is 1 or more) and a second wall surface having M-fold slits (M is 1 or more) are arranged facing each other and connected so that the slit directions of the opposing parts are aligned.

22. 22. The method of claim 21, further comprising: Regarding the N-fold slits (N is 1 or more) on the first wall surface and the M-fold slits (M is 1 or more) on the second wall surface, An accumulation method characterized in that N and M do not match.

23. 23. The method of claim 22, further comprising: Regarding the N-fold slits (N is 1 or more) on the first wall surface and the M-fold slits (M is 1 or more) on the second wall surface, An accumulation method characterized in that the total length of the slit widths of the first wall surfaces of the opposing portions is equal to the total length of the slit widths of the second wall surfaces.

24. 24. The method of any one of claims 21 to 23, comprising: An accumulation method, characterized in that the N-fold slits on the first wall surface and the M-fold slits on the second wall surface are linear slits.

25. 25. The method of any one of claims 21 to 24, comprising: An accumulation method, characterized in that the first wall surface and the second wall surface are such that a straight line connecting the centers of the multiple slits or single slits in the slit width direction of each wall surface is perpendicular to both wall surfaces.

26. 26. The method of any one of claims 21 to 25, comprising: An accumulation method, characterized in that, when the first wall surface and the second wall surface each have multiple slits, the slit widths of the slits that make up the first wall surface and the second wall surface are the same.

27. 21. The method of claim 19 or 20, The first thrust generation unit or the second thrust generation unit includes: An integration method characterized in that a third wall surface on which P adjacent holes (P is 1 or more) are arranged faces a surface on which Q adjacent holes (Q is 1 or more) are arranged.

28. 28. The method of claim 27, further comprising: For P adjacent holes on the third wall and Q adjacent holes on the fourth wall, A method of accumulation characterized in that P and Q do not match.

29. 29. The method of claim 28, further comprising: An accumulation method, characterized in that the total area of ​​the P adjacent holes on the third wall surface is equal to the total area of ​​the Q adjacent holes on the fourth wall surface.

30. 30. The method of any one of claims 27 to 29, comprising: The accumulation method is characterized in that the third wall surface and the fourth wall surface are characterized in that a straight line connecting the centers of gravity of the holes in each wall surface is perpendicular to both wall surfaces.

31. 31. The method of any one of claims 27 to 30, comprising: An accumulation method, characterized in that when there are multiple holes in each of the third wall surface and the fourth wall surface, the areas of the holes that constitute them are the same.

32. 32. The method of any one of claims 19 to 31, comprising: An integration method, characterized in that the size of the first impulse generating unit or the second impulse generating unit is on the nano-order, at which quantum mechanical properties become prominent.

33. 32. The method of any one of claims 19 to 31, comprising: An integration method, characterized in that the size of the first impulse generating unit or the second impulse generating unit is on the pico-order, at which quantum mechanical properties become prominent.

34. 34. The method of any one of claims 1 to 33, The power required to generate the centrifugal force is An accumulation method characterized in that the power output by the accumulation is the same as that produced by the resultant force of the first propulsion force that can be effectively extracted excluding losses.

35. 34. The method of any one of claims 1 to 33, than the power used to generate the centrifugal force, An accumulation method characterized in that the power produced by the resultant force of the first thrust forces that can be effectively extracted excluding losses through said accumulation is greater.

36. A first assembly implementing the assembly method of any one of claims 1 to 35.

37. A second assembly implementing the assembly method of any one of claims 5 to 35.

38. A first plate-shaped member that implements the integration method according to any one of claims 4 to 35.

39. A second plate-like member that implements the integration method according to any one of claims 5 to 35.

40. A thrust generating device comprising a second assembly that implements the assembly method according to any one of claims 5 to 35, a first plate-like member, and a second plate-like member.

41. A gravity action reducing device, characterized in that it uses the thrust generating device according to claim 40 to reduce the falling speed of an object against gravity.

42. A levitation device that uses the thrust generating device according to claim 40 to levitate an object against gravity.

43. A power generating device that extracts energy from atmospheric heat using the thrust generating device according to claim 40.

44. 41. An atmospheric cooling system that extracts energy from atmospheric heat using the thrust generating system according to claim 40.

45. An airflow generating device using the thrust generating device according to claim 40.

46. A space elevator using the thrust generating device according to claim 40.

47. An atmospheric escape system for a spacecraft, using the thrust generating device according to claim 40.

48. A floating residence using the thrust generating device according to claim 40.

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