JP2018167813A - Protrusive substance propelled by body product having a plurality of protrusive faces and streamline shape generated by acceleration at alongside flow of fluid on protrusive face - Google Patents

Abstract

To provide a streamline shape which can obtain a propulsion force without using a power supply, and can save energy.SOLUTION: A three-dimensional substance including a constitution which is formed of a plurality of protrusive faces including faces having wing shapes formed by a protrusive face action which is accelerated when fluids flow alongside on the protrusive faces, and the protrusive faces including streamline shapes is propelled by a three-dimensional substance 1 including protrusive faces having rear edges of shapes with which fluids flowing alongside on the three-dimensional substance including the protrusive faces merge in a direction which is the closest to a parallel with direction.SELECTED DRAWING: Figure 1

Description

  The present invention relates to a convex object driven by a body having a plurality of convex surfaces and streamlined shapes.

  A wing whose length is shorter than the upper length from the leading edge to the trailing edge of the wing is referred to as a "flying wing", a wing having the same shape as a bird wing is referred to as a "bird wing", and Symmetrical wings with symmetrical bottom shapes are called “symmetrical wings”, and each wing is called “propulsion wing”. The length from the leading edge to the trailing edge of the wing is “chord chord length”, and the chord length is In the case of a flying wing of 10m, when the head wind is 50km / h from the stationary state and passes through the wing in 0.72 seconds (3600 ÷ 50000 × 10), the length of the upper curve of the wing is 11m When the average speed is 55 km / h (3600 ÷ 0.72 × 11) and the length of the lower curve is 10.5 m, it passes the trailing edge at an average speed of 52.5 km / h (3600 ÷ 0.72 × 10.5) However, there has previously been an `` isochronous passage '' theory in which the main wind of the heading wind at the trailing edge and the wind at the top and bottom of the wing pass at the same time. It shows that the air resistance is "0 (zero)", and now when the head wind separates from the leading edge of the wing to the upper and lower parts and arrives at the trailing edge along the surface, the chord length However, the longer the distance, the higher the speed than the heading wind before separation, and it has been confirmed by wind tunnel experiments that the upper part, which is longer than the lower part, passes through the trailing edge much faster. Although the passing theory is denied, this phenomenon indicates that the air resistance of the entire flight wing is "-(minus)", but it is common sense that the resistance is not considered to be zero or minus However, the head wind is the flow of air along the surface from the leading edge to the trailing edge of the wing, and the upper part passes through the trailing edge earlier than the lower part of the wing, and is ejected to the rear of the wing. However, the air mass in the upper part of the wing is less than that in the lower part. It seems that there is not much change when comparing the mass of air reduced at the top of the wing with the mass of air received by the atmosphere on the entire wing, and a certain amount of force is required to lift the entire airplane including the wing. Although it must be secured, it is difficult to think that the amount of air at the top of the wing has decreased slightly and that it will be converted to a lift that lifts the entire airplane due to the pressure difference generated on the wing. The leading edge (d) and the trailing edge (e) are displayed at the same position in the longitudinal direction of the propeller blade cross section (a), and the upper part (b) and the lower part (c) of each blade cross section are chord lengths (f 2 is a diagram written so that it can be contrasted with FIG. 2, and FIG. 2 shows that the speed increases due to the flow of the air along the curved surfaces of the upper and lower parts due to the shape of the propulsion blade, and passes from the upper surface to the trailing edge (e) The upper propulsive force (g) indicating the direction of air travel and momentum, and the rear edge (e ) The resultant propulsive force (i) is displayed as a result of the lower propulsive force (h) indicating the traveling direction and momentum of the air as it passes through, and the flying wing and the bird wing are propelled forward by the reaction. The force and upward lift force are obtained, and it is understood that the forward thrust is acting on the symmetric wing, and this action is called "curve along the curved surface". It is defined as having a force, and the target of lift and propulsion is the shape of the propulsion blade (see Patent Document 1).

A surface formed by a curved line with an arc having a center point is called an "arc surface", a set of the arc surfaces is called a "curved surface", and a curved surface bulging outward is a "convex surface" and a curved surface bulging inward is "concave The viscous fluid substance such as air or water is referred to as “viscous body”, the state where the viscous body and the object are in direct contact with each other is referred to as “closely”, `` Flow '', the pressure applied by air or water due to gravity is `` external pressure '', the force pushing toward the center of the arc on the arc is `` centripetal force '', and the combined force and force to move is `` synthetic force ''
When the sticky body runs along the object, the sticky body is in close contact with the object, and there is nothing between the sticky body and the object and the sticky body is integrated. Conventionally, when the external pressure applied to the object acts from above the viscous body, the object and the viscous body flowing along the object are integrated by the external pressure. It is obvious that it is along the same shape as the shape, and external pressure acts on the whole including the viscous body and the object that are flowing along, but the pressure acting on the viscous body that is in close contact with the object in particular. Is the “incident pressure”.
When the sticky body flows along the arc surface, the sticky body tries to go straight from the contact point of the arc surface by inertia in the same direction as the direction of the centrifugal force perpendicular to the direction of the center point of the arc surface. The force is `` inertial straight force '', the incidental pressure received within the range of the direction of inertia straight force starting from the contact point with the viscous body on the arc surface and the arc surface on the direction side is `` internal pressure '', The incidental pressure received from outside this range is called "external pressure"
When a sticky body flows along an arc surface, the sticky body that is in contact with the arc surface acts in a direction that separates from the arc surface due to inertial linear force, but this action is in contact with the arc surface and the arc surface. In order to avoid a large force that causes a vacuum state due to the peeling pressure reduction, the incident pressure corresponds,
When peeling due to the inertial linear force of the sticky body, if the distance to the center point in the arc surface along which the sticky body flows is long, or if the inertial straight-forward force is weaker than the incidental pressure, it will not peel off to avoid pressure reduction. The external pressure of the incidental pressure becomes a centripetal force and presses the viscous body, and the action of pressing the viscous body continues as long as the described conditions are satisfied, and the continuous action causes the viscous body to continuously arc. The flow along the convex surface is accelerated by the combined force of inertia linearity and centripetal force due to the flow velocity of the conventional sticky body at the same time while pressing against the surface. Power,
When the sticky body is peeled off by the inertial straight force, if the distance to the center point in the arc surface along which the sticky body flows is short or if the inertial straight force is stronger than the incident pressure, the sticky body is Although it peels from the surface, in order to avoid peeling pressure reduction after the sticky body peels off, the internal pressure compensates the sticky body in the range where the internal pressure acts by the attached pressure on the trace surface. The filling direction and the direction in which the sticky body peels are opposite to each other, and a vortex is generated when the directions are different from each other. The factor acts continuously as long as the described conditions are satisfied, and the eddy is continuously generated by the intermittent action, and the generated vortex is from the point where the sticky body that has flowed along the convex surface is separated. The vortex will be circulated, and the speed of the viscous material that has flowed along the convex surface will be absorbed by the circulation of the vortex.
When the sticky substance running along the body leaves, the flow velocity is impaired by joining the upper and lower surfaces along the parallel and sharp angles as much as possible, like the tip of the flap that is actually the trailing edge of the blade. However, due to the difference in the flow velocity from the upper surface and the lower surface at the actual blade trailing edge, the wing itself generates propulsive force and rise while generating unnecessary vortices. However, the lower surface of the wing is constituted by the same shape as the upper surface of the wing, and the lifting force that lifts the wing is obtained in order to obtain the action of the driving force and the lifting force acting on the same convex surface as the upper surface. The illusion of ascending force is canceled out, the unnecessary vortex generated in the diagonally downward direction of the wing disappears, and it is possible to obtain the effect of amplifying the force propelled forward, and the upper and lower surfaces are Like the symmetrical wing with the same shape, the acceleration along the convex surface is obtained by the upper and lower convex surfaces. As shown by the shape of the flap along the convex surface, the wing with a shape that is configured so that the trailing edges merge as parallel and at a sharp angle as possible is referred to as a "propulsion wing". Including not only asymmetric but also a shape that can obtain acceleration along the convex surface on the lower surface,
Although there is no lift, it has been used during take-off and landing by adjusting the strength of the lift by lowering the tip of the flap at the trailing edge of the wing. Propelling force and ascending force are obtained by jetting, but by lowering the flap tip, the propulsive force of the wing is reduced by the reaction caused by strengthening the downward jetting and the ascending force is amplified. Since the strength of the ascending force is used for assisting takeoff and landing, the flap has a rudder function that adjusts the flow, and the propulsion wing has the function of the rudder, and the same function and progress as the propulsion wing. A rudder equipped with a function to change the direction is called a "propulsion rudder"
There is a streamline type that shows the shape to reduce air resistance and a tear suitable type that shows the shape by submarines, etc., similar to the shape of fish and dolphins, etc. By occupying a large amount, the effect of the acceleration force along the convex surface is obtained, and at the end, the viscous bodies flowing along the surface are concentrated at one point at a sharp angle and are ejected in a concentrated manner on the line. The shape formed as “flowing type”, and the object formed by the flow type as “flowing body”,
The propulsion blade is a flow type, and the propulsion rudder belongs to the flow assembly. By providing the flow control body with a propulsion rudder, it is possible to obtain further propulsive power, and by power in the external pressure of airplanes, automobiles, etc. A moving object is a “self-propelled body”, and the self-propelled body is formed as a “self-propelled fluidized type” by providing a flowable type in the shape of the self-propelled body. Is a self-propelled flow body, and the self-propelled flow body is equipped with a propulsion wing. Containing a ligation body, including a flow type or a flow body in a part or a plurality of parts of an object including a self-propelled body, and having a flow type or a flow body in a part or a plurality of the flow type. In addition, the present invention is characterized in that a part or a plurality of the joined bodies are provided with a casting type or a joined body (see Patent Document 2).

JP 2017-19391 A Japanese Patent Application No. 2016-166359

  In airplanes and the like, the wings that have the shape of a bird's wings should be used for flying by generating a lift by dividing the flowing airflow into two directions, up and down, but as an effect of lift, Although the air pressure difference sucks up the wings upward, it is impossible to suck up and lift the heavy wings upward because physically lighter air is absorbed first. However, from the fact that “the airflow at the top of the wing arrives at the trailing edge of the wing faster than the airflow at the bottom”, “the airflow accelerated at the top of the wing is ejected diagonally downward and rearward at the speed accelerated by the trailing edge of the wing. It is understood that the wings are propelled diagonally up and forward because the airflow is ejected diagonally downward and rearward, and the fluid flowing along the curved surface is used without knowing that it will accelerate. For symmetrical wings, lift cancels out, so the convexity ratio of the convex surface does not increase. Have been, was the use of the subject the occurrence of lift only in one direction with respect to the upper surface so made up the wing.

  A fluid that has a convex surface effect that accelerates when a fluid flows along the convex surface, and that includes a plurality of convex surfaces including a surface due to the shape of a wing, or a solid object that includes a streamlined shape, and that flows along the three-dimensional object including the convex surface. Convex object that is propelled by a three-dimensional object including a convex surface with a trailing edge that merges in a direction as close to parallel as possible

  In general, it tries to reduce air resistance by design (shape), but it is recognized that the resistance value never becomes zero. However, by having a flow type in the design, a force propelled by the acceleration force along the convex surface is added, and the resistance value can be less than zero, and the flow type can be incorporated into the shape of the self-propelled body. It is possible to obtain a propulsive force without using a power source by configuring the self-propelled body itself with a fluidized body or by providing the self-propelled body with a fluidized body, thereby saving energy.

  There is a theory that `` the airflow along the upper surface of the wing increases from the leading edge to the front in the traveling direction, but then decelerates toward the trailing edge '', which is a function different from the present invention, but actually As a phenomenon acting on the wing, a force other than the centripetal force acts on the sticky body flowing along the front edge or the front surface in the traveling direction, and no peeling phenomenon occurs, but it has not been confirmed.

  The flow along the concave surface decelerates against the acceleration along the convex surface, but the deceleration action is called "concave surface deceleration force", and the speed due to the viscous material flowing along the convex and concave surfaces is increased or decreased. The action to be performed was called “curved surface up / down force”.

  By using symmetrical wings, the lifting force such as lift is offset and the useless vortex disappears. By setting the angle of attack on the wing, the same ascending force can be obtained, and cruise flight can be adjusted by adjusting the angle of attack and flap. It becomes possible.

In the present invention, a sectional view of a propulsion blade in which the shape of the upper surface of the conventional blade is applied to the lower surface In the present invention, a cross-sectional view of a flow type constituted by an arc surface on which a convex surface acceleration force acts. In the present invention, a cross-sectional view of a self-propelled flow body equipped with a propulsion rudder with a self-propelled flow structure.

  In FIG. 1, propulsive force was obtained by the acceleration along the convex surface by the airflow flowing from the leading edge (4a) to the trailing edge (5a) on the upper surface (2) having the same shape as the upper side of the conventional wing. The vortex was generated due to the difference between the angle and the flow velocity at which the air flow was ejected from the trailing edge (5a), and the momentum was wasted. However, the air flow was created by forming the lower surface (3) with the same shape as the upper surface (2). FIG. 2 is a cross-sectional view of a propulsion blade (1) that can prevent generation of useless vortices and can obtain more propulsive force because the angle at which the gas is ejected and the flow velocity are the same.

  FIG. 2 shows the effect of the acceleration force along the convex surface from the front edge (4b) to the rear edge (5b) by the upper or right arc surface (7a) and the lower or left arc surface (7b). It is sectional drawing of the flow type | mold (6) comprised by the shape obtained.

  FIG. 3 shows a propulsion rudder (9) provided with a propulsive force due to the acceleration along the convex surface due to the fact that the self-propelled flow body (8) is formed of a convex surface. FIG.

  1, 2, and 3 can also be handled as a cross-sectional view in the shape of a sphere like a rugby ball, and the action of the acceleration along the convex surface changes depending on the degree of the convex surface area.

  For planes, gliders, hang gliders, paragliders, hydrofoil, etc., which usually have lift-causing factors, the surface corresponding to the plane is made of a convex surface to obtain a convex surface acceleration force. Can do.

  Reduce the power burden on the self-propelled body by obtaining the propulsive force of the joint body by providing the joint body on the self-propelled body, such as the roof and left and right sides of the car, the ship's shipboard and the bottom. Can do.

DESCRIPTION OF SYMBOLS 1 Propulsion blade 2 Upper surface 3 Lower surface 4a, 4b, Front edge 5a, 5b, Rear edge 6 Flow type 7a, 7b, Arc surface 8 Flow body 9 Propulsion rudder

Claims (1)

The wings that are shorter in the lower part than the upper part from the leading edge to the trailing edge of the middle wing are called “flight wings”, and the wings that have the same shape as the bird wings are called “bird wings”. The wings with symmetrical shapes at the bottom and the bottom are called “symmetric wings”, and each wing is called a “propulsion wing”, but the length from the leading edge to the trailing edge of the wing is “chord chord length”. In the case of a flying wing with a height of 10 m, a headwind of 50 km / h passes through the wing in 0.72 seconds (3600 ÷ 50000 × 10), and the upper curve length of the wing is 11 m. If the average speed is 55 km / h (3600 ÷ 0.72 × 11) and the length of the lower curve is 10.5 m, the trailing edge will be 52.5 km / h (3600 ÷ 0.72 × 10.5) Previously, there was an `` isochronous passage '' theory in which the main wind of the heading wind at the trailing edge, the wind at the top of the wing, and the wind at the bottom of the wing passed at the same time. The air resistance is 0 (zero), and when the head wind is separated from the leading edge of the wing to the top and bottom and reaches the trailing edge along the surface, the chord length As the distance is longer, the speed is higher than the head wind before separation, and it has been confirmed by wind tunnel experiments that the upper part, which is longer than the lower part, passes the trailing edge much faster. Although the time passing theory is denied, this phenomenon indicates that the air resistance of the entire flight wing is "-(minus)", but it is common sense that the resistance is zero or negative. Phenomenon, the head wind is the flow of air along the surface from the leading edge to the trailing edge of the wing, and the upper part passes through the trailing edge earlier than the lower part of the wing, and is ejected to the rear of the wing. However, since the air mass at the top of the wing is less than that at the bottom, the difference in pressure between the bottom and top of the wing However, there is not much change when comparing the mass of air reduced at the top of the wing and the mass of air received by the atmosphere on the entire wing, and it takes some force to lift the entire airplane including the wing. However, it is unlikely that the air pressure at the upper part of the wing has decreased slightly, and it is unlikely that it will be converted to a lift that lifts the entire airplane due to the pressure difference generated in the wing. Each type of propulsion blade cross section (a) is displayed in the longitudinal direction with the leading edge (d) and the trailing edge (e) at the same position, and the upper part (b) and the lower part (c) of each blade cross section are chord lengths ( Figure 2 is a diagram that can be contrasted with f). Figure 2 shows the propulsion blade shape that increases the speed of air flowing along the upper and lower curved surfaces, and passes through the trailing edge (e) from the upper surface. The upper propulsive force (g) showing the direction and momentum of the air when you e) The resultant propulsive force (i) obtained by combining the lower propulsive force (h) indicating the traveling direction and momentum of the air when passing through is displayed. By obtaining the propulsive force and the upward lift force, it is understood that the symmetric wings are acting in the forward direction, and this action is called “curved along the curved surface”. It is defined as having propulsive force, and the target of lift and propulsive force is the shape of the propulsion wing,
A surface formed by a curved line with an arc having a center point is called an "arc surface", a set of the arc surfaces is called a "curved surface", and a curved surface bulging outward is a "convex surface" and a curved surface bulging inward is "concave The viscous fluid substance such as air or water is referred to as “viscous body”, the state where the viscous body and the object are in direct contact with each other is referred to as “closely”, `` Flow '', the pressure applied by air or water due to gravity is `` external pressure '', the force pushing toward the center of the arc on the arc is `` centripetal force '', and the combined force and force to move is `` synthetic force ''
When the sticky body runs along the object, the sticky body is in close contact with the object, and there is nothing between the sticky body and the object and the sticky body is integrated. Conventionally, when the external pressure applied to the object acts from above the viscous body, the object and the viscous body flowing along the object are integrated by the external pressure. It is obvious that it is along the same shape as the shape, and external pressure acts on the whole including the viscous body and the object that are flowing along, but the pressure acting on the viscous body that is in close contact with the object in particular. Is the “incident pressure”.
When the sticky body flows along the arc surface, the sticky body tries to go straight from the contact point of the arc surface by inertia in the same direction as the direction of the centrifugal force perpendicular to the direction of the center point of the arc surface. The force is `` inertial straight force '', the incidental pressure received within the range of the direction of inertia straight force starting from the contact point with the viscous body on the arc surface and the arc surface on the direction side is `` internal pressure '', The incidental pressure received from outside this range is called "external pressure"
When a sticky body flows along an arc surface, the sticky body that is in contact with the arc surface acts in a direction that separates from the arc surface due to inertial linear force, but this action is in contact with the arc surface and the arc surface. In order to avoid a large force that causes a vacuum state due to the peeling pressure reduction, the incident pressure corresponds,
When peeling due to the inertial linear force of the sticky body, if the distance to the center point in the arc surface along which the sticky body flows is long, or if the inertial straight-forward force is weaker than the incidental pressure, it will not peel off to avoid pressure reduction. The external pressure of the incidental pressure becomes a centripetal force and presses the viscous body, and the action of pressing the viscous body continues as long as the described conditions are satisfied, and the continuous action causes the viscous body to continuously arc. The flow along the convex surface is accelerated by the combined force of inertia linearity and centripetal force due to the flow velocity of the conventional sticky body at the same time while pressing against the surface. Power,
When the sticky body is peeled off by the inertial straight force, if the distance to the center point in the arc surface along which the sticky body flows is short or if the inertial straight force is stronger than the incident pressure, the sticky body is Although it peels from the surface, in order to avoid peeling pressure reduction after the sticky body peels off, the internal pressure compensates the sticky body in the range where the internal pressure acts by the attached pressure on the trace surface. The filling direction and the direction in which the sticky body peels are opposite to each other, and a vortex is generated when the directions are different from each other. The factor acts continuously as long as the described conditions are satisfied, and the eddy is continuously generated by the intermittent action, and the generated vortex is from the point where the sticky body that has flowed along the convex surface is separated. The vortex will be circulated, and the speed of the viscous material that has flowed along the convex surface will be absorbed by the circulation of the vortex.
When the sticky substance running along the body leaves, the flow velocity is impaired by joining the upper and lower surfaces along the parallel and sharp angles as much as possible, like the tip of the flap that is actually the trailing edge of the blade. However, due to the difference in the flow velocity from the upper surface and the lower surface at the actual blade trailing edge, the wing itself generates propulsive force and rise while generating unnecessary vortices. However, the lower surface of the wing is constituted by the same shape as the upper surface of the wing, and the lifting force that lifts the wing is obtained in order to obtain the action of the driving force and the lifting force acting on the same convex surface as the upper surface. The illusion of ascending force is canceled out, the unnecessary vortex generated in the diagonally downward direction of the wing disappears, and it is possible to obtain the effect of amplifying the force propelled forward, and the upper and lower surfaces are Like the symmetrical wing with the same shape, the acceleration along the convex surface is obtained by the upper and lower convex surfaces. As shown by the shape of the flap along the convex surface, the wing with a shape that is configured so that the trailing edges merge as parallel and at a sharp angle as possible is referred to as a "propulsion wing". Including not only asymmetric but also a shape that can obtain acceleration along the convex surface on the lower surface,
Although there is no lift, it has been used during take-off and landing by adjusting the strength of the lift by lowering the tip of the flap at the trailing edge of the wing. Propelling force and ascending force are obtained by jetting, but by lowering the flap tip, the propulsive force of the wing is reduced by the reaction caused by strengthening the downward jetting and the ascending force is amplified. Since the strength of the ascending force is used for assisting takeoff and landing, the flap has a rudder function that adjusts the flow, and the propulsion wing has the function of the rudder, and the same function and progress as the propulsion wing. A rudder equipped with a function to change the direction is called a "propulsion rudder"
There is a streamline type that shows the shape to reduce air resistance and a tear suitable type that shows the shape by submarines, etc., similar to the shape of fish and dolphins, etc. By occupying a large amount, the effect of the acceleration force along the convex surface is obtained, and at the end, the viscous bodies flowing along the surface are concentrated at one point at a sharp angle and are ejected in a concentrated manner on the line. The shape formed as “flowing type”, and the object formed by the flow type as “flowing body”,
The propulsion blade is a flow type, and the propulsion rudder belongs to the flow assembly. By providing the flow control body with a propulsion rudder, it is possible to obtain further propulsive power, and by power in the external pressure of airplanes, automobiles, etc. A moving object is a “self-propelled body”, and the self-propelled body is formed as a “self-propelled fluidized type” by providing a flowable type in the shape of the self-propelled body. Is a self-propelled flow body, and the self-propelled flow body is equipped with a propulsion wing. Containing a ligation body, including a flow type or a flow body in a part or a plurality of parts of an object including a self-propelled body, and having a flow type or a flow body in a part or a plurality of the flow type. , Characterized by having a flow type or flow body in part or multiple of the flow body,
A fluid that has a convex surface effect that accelerates when a fluid flows along the convex surface, and that includes a plurality of convex surfaces including a surface due to the shape of a wing, or a solid object that includes a streamlined shape, and that flows along the three-dimensional object including the convex surface. Is characterized by a convex object propelled by a three-dimensional object including a convex surface with a trailing edge that merges in a direction that is as parallel as possible, and the fluid is streamlined with multiple convex surfaces by accelerating as it flows along the convex surface Convex object to be propelled by a body equipped with