14 results about "Artificial gravity" patented technology

To provide an excessive gravity facility that easily ensures freedom of movement for users under excessive gravity. [Solution] The hypergravity facility 1 is an hypergravity facility that generates an artificial gravity F on Earth that is greater than the Earth's gravity. It is equipped with a rotating body 5 that rotates around a vertical rotation axis A, and generates artificial gravity F on a floor surface 10 inside the rotating body 5 as a result of the combined force of the Earth's gravity F1 and the centrifugal force F2 due to the rotation of the rotating body 5. In a cross-sectional view perpendicular to the rotation axis A, the floor surface 10 extends along a circle centered on the rotation axis A, and in a cross-sectional view including the rotation axis A, the floor surface 10 forms a curve that bulges outward.

The AAMD was designed to address the concerns of deep space travel, in both the distance and time required. Today's rocket propulsion systems rely on expelling large amounts of fuel for short intervals and then coasting long intervals. This method is both expensive and time consuming where deep space is concerned.The AAMD is an alternative to rocket systems and it enables a vehicle to have a constant acceleration rates and deceleration rates. For instance, if the AAMD could provide a constant 1 G of acceleration and 1 G of deceleration, it would take less than a week to go from earth to mars, depending on their locations, whereas today's fastest rockets are 7 to 9 months, for the same trip.Slow and long travel times also are not good for the human body as the bones and muscle begin to deteriorate. The AAMD with its constant G applied to the occupants, will enjoy an artificial gravity produced by means of the constant acceleration. This would allow the occupants to have no breakdown in bones and muscle.The system uses of 2 counter rotating rotors and 8—orbital motors / generator per rotor, with—4 gyroscopes per orbital motor / generator. The moveable gyroscopes are capable of altering their location, from the main rotors axis. At the same time enable the other spinning mass to experience a balanced rotor the entire duration of the moveable weights altering their location of mass. The AAMD enables a means to impart linear movement in short increments of instantaneous directional linear thrust and follow the principle of the conservation of angular momentum.This is achieved and enables the vehicles propulsion system to have a 2 stage “push”-“pull” operation with controllable, directional thrust capability. If there was a need to move an object that is stationary, it is necessary to apply a force to influence it to do so. The AAMD can be powered by a nuclear reactor for extreme long range and ultra-high speeds to reach planets not feasible by means of rockets.

This hypergravity facility is a hypergravity installation on Earth for generating artificial gravity that is stronger than Earth's gravity, and comprises a rotary body that rotates about a vertical axis of rotation, wherein artificial gravity is generated on a floor surface on the inside of the rotary body as the combined force of Earth's gravity and the centrifugal force due to the rotation of the rotary body. In a cross-sectional view orthogonal to the axis of rotation, the floor surface extends along a circle centered on the axis of rotation, and in a cross-sectional view that includes the axis of rotation, the floor surface is curved in an outwardly bulging manner.

1. Name of the product in this design: Artificial Gravity Engine. 2. Application of this design: This design is used in gravity engines. 3. The key design feature of this product is its shape. 4. The image or photograph that best illustrates the design's key points: a 3D model.

The objective is to reduce the effects of Coriolis force in an artificial gravity generator. [Solution] An artificial gravity generating device comprising: a driving source 1; a rotating shaft member 2 that is rotated by the driving source 1; an arm 3 attached to the rotating shaft member 2; and a first box-body 6 that can accommodate a person and is connected to the arm 3 via a joint member 4 that can rotate in any direction and can be tilted in any direction by the joint member 4, thereby reducing the effects of the Coriolis force acting during rotation; and wherein the rotation of the rotating shaft member 2 causes the first box-body 6 to rotate around the rotating shaft member 2, thereby generating centrifugal force.

The invention discloses a device for passengers to rotate in a space capsule. The device comprises a supporting part on the space capsule, a supporting shaft, a crankshaft or a crank fixedly or movably connected with the supporting shaft, an elastic device and a loader capable of carrying people to rotate, wherein one end of the elastic device is movably connected with the crank pin or the crank pin, and the other connecting end of the elastic device is connected with the supporting part or other fixing devices; the loader is formed by connecting a suspension pull part and a manned part; the suspension pull part is directly or indirectly fixedly connected with the crankshaft or the crank, and swinging or rotating of the suspension pull part enables the linked crankshaft pin or crank pin to be subjected to correspondingly changed force of the elastic device; the manned part bears the body of a passenger or provides centripetal force required by circular motion of the passenger; the operating method of the device comprises the steps that the moving direction of the mass center of a passenger relative to the suspension pull part is preferably consistent with the direction of torque which is borne by the suspension pull part and transmitted by a crankshaft or a crank through an elastic device, or the movement in the direction is carried out when the torque borne by the suspension pull part is large or maximum; the swing amplitude or the rotation speed of the loader can be increased through repeated operation, and the effects of feeling the artificial gravity and building the body are achieved.

1. LIFTING FORCE NGUYEN BALY: N*BALY Fn*Baly = av2; KG.Mm / s2 See figure 1, A and C 2. 2. NEW GENERATION AIRCRAFT AND SPACECRAFT NGUYEN VAN LY: N*VAN LY AND COMPATIBLE DEVICES See figures 2 and 3. 3. NGUYEN NGOC BAO NEW SPACEPORT: N*BAO-S See figures 2 and 3. 4. ARTIFICIAL EARTH NGUYEN NGOC BAO: N*BAO ARTIFICIAL GRAVITY AND SHIP PROPULSION ORBIT DIRECTOR DO THI QUY: N*QUY. See figures 2, 3, 4 and 4-3D. 5. NEW PARALLEL SATELLITE SYSTEM DOMINATES THE SPACE NGUYEN LEVY: N*LEVY 30 SEPTEMBER 2024. NEW SAT N*Levy 2025 See figures D, E and F. 6. NGUYEN LEVY: N*LEVY NEW FORMULA ACCURACY: - SPHERICAL SURFACE: Sn*Levy = π 2.R2; m2 and - SPHERICAL VOLUME: Vn*Levy = π 2.R3 / 3; m3. See figures H, I, J and K. 7. NEW THEORY NGUYEN KIMBERLY: N*KIMBERRLY STRUCTURE AND FUNCTION OF THE SOLAR SYSTEM AND THE UNIVERSE. FLAT GRAVITATIONAL FIELD. See figures A, B and D.

The invention relates to the technical field of spacecraft structure design, in particular to a maximum-scale space factory optimization design method and system. The method comprises the following steps of performing dynamic stability design optimization based on a maximum-scale space factory space structure; constructing a macroscopic configuration multi-level optimization objective function, and solving a design variable array through the macroscopic configuration multi-level optimization objective function; carrying out microstructure design by combining strength, rigidity and a thermal expansion effect; and reverse design optimization of typical components is carried out through macroscopic design and microstructure design results. According to the method, the space factory is controlled through the dynamic stability, then the macroscopic configuration and the microstructure are combined for multi-level design optimization, the complex requirements of the space factory can be effectively met, the macroscopic configuration of the space factory is optimized, and the dynamic stability and the artificial gravity requirements of the structure are ensured. Meanwhile, according to the lattice structure design of the micro-level, the additive manufacturing technology is utilized, and unification of light weight and high strength is achieved.

The invention relates to the technical field of space station cabins, in particular to a structure for generating artificial gravity of a space station and a working method of the structure. According to the cabin structure for generating the artificial gravity in the space station and the working method of the cabin structure, in order to achieve the purpose, the following technical scheme is provided, and the cabin structure for generating the artificial gravity in the space station comprises a cabin body, comprising a connecting cabin, a radial connecting rod, at least one radial channel, an outer cabin, an inner cabin and a transfer cabin, wherein the connecting cabin is static relative to other cabins of the space station; the inner cabin rotates at a certain angular speed relative to the outer cabin; and the transfer cabin is used for transferring personnel or materials between the inner cabin and the outer cabin. And the inner cabin is controlled by a motor to rotate at a certain angular speed on a track fixed in the outer cabin. And the rotating state of the transfer cabin is changed through a motor on a track fixed on the outer cabin, so that the transfer cabin is synchronized with the outer cabin or the inner cabin. And the connecting cabin, the radial channel and the outer cabin are of an integral sealing structure.

1. LIFTING FORCE NGUYEN BALY: N*BALY Fn*Baly = av2; KG.Mm / s2 See figure 1, A and C 2. 2. NEW GENERATION AIRCRAFT AND SPACECRAFT NGUYEN VAN LY: N*VAN LY AND COMPATIBLE DEVICES See figures 2 and 3. 3. NGUYEN NGOC BAO NEW SPACEPORT: N*BAO-S See figures 2 and 3. 4. ARTIFICIAL EARTH NGUYEN NGOC BAO: N*BAO ARTIFICIAL GRAVITY AND SHIP PROPULSION ORBIT DIRECTOR DO THI QUY: N*QUY. See figures 2, 3, 4 and 4-3D. 5. NEW PARALLEL SATELLITE SYSTEM DOMINATES THE SPACE NGUYEN LEVY: N*LEVY 30 SEPTEMBER 2024. NEW SAT N*Levy 2025 See figures D, E and F. 6. NGUYEN LEVY: N*LEVY NEW FORMULA ACCURACY: - SPHERICAL SURFACE: Sn*Levy = π 2.R2; m2 and - SPHERICAL VOLUME: Vn*Levy = π 2.R3 / 3; m3. See figures H, I, J and K. 7. NEW THEORY NGUYEN KIMBERLY: N*KIMBERRLY STRUCTURE AND FUNCTION OF THE SOLAR SYSTEM AND THE UNIVERSE. FLAT GRAVITATIONAL FIELD. See figures A, B and D.

Method and Apparatus for Creating Artificial Gravity in Spacecraft and Space Stations Using Anti-Parallel Reaction Engines is disclosed. The reaction engines are activated to spin the spacecraft or the space station and generate centrifugal gravity. The spacecraft is designed to be cylindrical in shape to maximize the surface area available for the installation of the engines. The station is designed to be circular in shape as well. The method has several applications in astronautics and space exploration, specifically for long-duration space missions where exposure to microgravity can cause adverse health effects to crew members. The method is highly efficient, providing a sustainable and controlled gravity environment without the need for large, heavy, and power-hungry traditional gravity generation systems. The invention also offers a high degree of flexibility with scalability for spacecraft of different sizes and shapes. The anti-parallel arrangement of the reaction engines ensures stability and a controlled spin rate, mitigating the risks associated with traditional mechanical alternatives. The invention offers significant improvement in the field of space exploration, providing safe, sustainable, and cost-effective solutions for generating artificial gravity in spacecraft.

The present disclosure provides an apparatus comprising a first outer ring module and a second outer ring module configured to produce artificial gravity environments when revolved about a rotational axis. At least one circumferential access tube may connect the first and second outer ring modules. A central hub may be connected to the first and second outer ring modules via first and second radial access tubes, respectively. A microgravity module may be located coaxial with the rotational axis and connected to the central hub via a rotary union. The apparatus may enable simultaneous provision of artificial gravity and microgravity environments within a single space vehicle structure, allowing for diverse research, manufacturing, and habitation capabilities in space.

A modified technology of spin coating which is named Two-Axis spin coating is disclosed. The innovative Two-Axis spin coating apparatus is a rotary device that spins the substrate horizontally the same as conventional spin coaters while the whole horizontal spinning system can be rotated vertically. The vertical rotation of the substrate generates a vertical centrifugal force perpendicular to the surface of the substrate which allows the coating face with an elevated artificial gravity acceleration. The elevation of gravity acceleration adjusts and normalizes the local high and low surface tension stresses on the surface of the coated film. This elevation of gravity also increases the weight of coating elements artificially and obliges the wavy surface convex regions to flow toward the concave areas. The elevation of gravity also obliges the lighter probable air bubbles inside the layer, immediately before the coating surface skinning process, move toward the surface and drain out from the layer. The invention provides a method to level the layer's edge beads, level the coated surface, drain out probable micro sized air bubbles inside the layer and form denser film simultaneously.

To provide a hypergravity facility capable of easily securing freedom of movement of users under hypergravity.SOLUTION: There is provided a hypergravity facility 1 for generating on the earth, artificial gravity F that is greater than the earth's gravity. The hypergravity facility includes a rotating body 5 for rotating around a vertical rotation axis A, and generates the artificial gravity F on a floor surface 10 inside the rotating body 5 as resultant force of the earth's gravity F1 and centrifugal force F2 generated by the rotation of the rotating body 5, where the floor surface 10 extends along a circle centered on the rotation axis A in a cross-sectional view orthogonal to the rotation axis A, and the floor surface 10 forms a curved line bulging outward in a cross-sectional view including the rotation axis A.SELECTED DRAWING: Figure 2