Abstract: The present invention provides a power device generating greater propelling force and finds that traditional power devices do not include all propelling forces based on the fundamental core propelling force source problem. External pressure is guided to the traditional power devices since the inner speed is higher the outer speed, power consumption for overcoming fluid resistance is high, and mutual contradiction results are obtained.

Abstract: Embodiments include devices and methods for processing an image captured by an image sensor of a robotic vehicle. A processor of the robotic vehicle may calculate an image output orientation matrix for an image that is output by the image sensor. The processor may calculate image sensor orientation matrix the image sensor. The processor may calculate a body orientation matrix of the robotic vehicle. The processor may transform the image captured by the image sensor based on the image output orientation matrix, the image sensor orientation matrix, and the body orientation matrix.

Abstract: Disclosed in the present invention is a high-speed aircraft, comprising a shell and an engine, an outer fluid channel and an inner fluid channel being arranged in succession within the shell, the outer fluid channel and the inner fluid channel respectively connecting to the exterior by means of their own air vent; the outer fluid channel is connected to an air suction port of the engine, such that the pressure difference produced by the flow rate within the outer fluid channel being greater than the flow rate within the inner fluid channel acts as the driving force source of the aircraft. Also disclosed in the present invention is an aircraft having greater lift. The present invention provides an innovative method and apparatus for a driving force source obtained from fluid resistance, thus changing the mutual contradiction of a traditional driving apparatus directing external force to itself whilst also needing to use more driving force to overcome fluid resistance.

Abstract: The invention discloses a lift source for an aircraft comprising a fuselage and wings, wherein first channels are formed in the wings, a plurality of first inlets are formed in upper surfaces of the wings, a plurality of first pressure ports are formed in lower surfaces of the wings and are communicated with the first inlets via the first channels; and spoiler devices are arranged in the first channels and under the effect of the spoiler devices, form high-speed fluid layers on the upper surfaces of the wings, thereby generating a pressure difference from the lower surfaces of the wings which counteracts an external fluid pressure on the upper surfaces of the wings in the opposite direction, so a lift is generated by reduction of fluid resistance when fluid flows through the upper and lower surfaces of the wings, thereby developing a high-speed aircraft with a larger lift and thrust.

Abstract: The invention discloses an aircraft generating a larger thrust and lift by fluid continuity. First open channels used to extend fluid paths are formed in front parts and/or middle parts of windward sides of wings of the aircraft and extend from sides, close to the fuselage, of the wings to sides, away from the fuselage, of the wings, and the first open channels are concave channels or convex channels, so that a pressure difference in a direction identical with a moving direction is generated from back to front due to different flow speeds of fluid flowing over the windward sides of the wings in a lengthwise direction and a widthwise direction to reduce fluid resistance, and a larger pressure difference and lift are generated due to different flow speeds on the windward sides and leeward sides of the wings.

Abstract: Provided are embodiments of a suspension train comprising a shell body, wheels and a flow disturbing plate connected with the wheels, a suspension train operating system comprising a non-vacuum cover body and the suspension train traveling in the cover body in an ideal vacuum state at high speeds, and first and second propelling force sources converted from fluid resistance for multiplying propelling force of the train. A fluid channel communicating with the outside is formed between the upper surface of the flow disturbing plate with the lower surface being a concave-convex flow disturbing surface and the bottom of the shell body. The high-speed suspension train is completely driven by solar energy.

Abstract: The invention discloses a flight vehicle generating a lift from an interior thereof. The fluid channel inside the flight vehicle communicates with the engine and the ports on the upper surface of the outer shell. With the powerful suction of the engine, the fluid on the upper surface of the outer shell is quickly sucked into the fluid channel via respective ports under conditions of long path, large area, high speed and low air pressure, which results in large lift from the interior of the flight vehicle. In the course of generating the lift, the fluid resistances of the fluid wall and the fluid hole are sucked into the fluid channel through the ports at the front and the surrounding area of the flight vehicle, then high-speed fluid is emitted from the rear port. This approach contributes greatly to the transformation of the existing flight vehicle. The present invention significantly improves the lift, the speed and the carrying capacity of the existing flight vehicle with lowered energy consumption.

Abstract: Embodiments include devices and methods for processing an image captured by an image sensor of an unmanned autonomous vehicle (UAV). A processor of the UAV may determine a body coordinate matrix of the UAV. The processor may determine an estimated rotation of the image sensor of the UAV. The processor may determine an estimated rotation of the UAV. The processor may transform an image captured by the image sensor based on the body coordinate matrix, the estimated rotation of the image sensor, and the estimated rotation of the UAV.

Abstract: Embodiments include devices and methods for adaptive image processing in an unmanned autonomous vehicle (UAV). In various embodiments, an image sensor may capture an image, while a processor of the UAV obtains attitude information from one or more attitude sensors. Such information may include the relative attitude of the UAV and changes in attitude. The processor of the UAV may determine a UAV motion mode based, at least in part, on the obtained attitude information. The UAV motion mode may result in the modification of yaw correction parameters. The processor of the UAV may further execute yaw filtering on the image based, at least in part, on the determined motion mode.

Abstract: Embodiments include devices and methods for adaptive image processing in an umnanned autonomous vehicle (UAV). In various embodiments, an image sensor may capture an image. Images may be obtained during motion or hover modes of the UAV. The UAV may determine whether stabilizing a line of the image causes a breach of an image crop margin. That is, the UAV may estimate or begin to adjust image distortion and crop the image, and may evaluate during or after the estimation/adjustment whether an image crop margin is breached by the result. The UAV may reduce stabilizing of the line of the image in response to determining that stabilizing the line of the image causes a breach of the image crop margin.

Abstract: The present disclosure relates to a bladeless fan, which includes a housing and a power device, wherein the power device communicates with a fluid passage and a negative pressure passage disposed in the housing respectively; the fluid passage communicates with the outside through a plurality of exhaust ports, and the negative pressure communicates with the outside through a plurality of suction ports; a middle region inside the fluid passage is provided with a spoiler device so that a path along which the fluid passes through the spoiler device is larger than a path along which the fluid passes around the corresponding inner wall, thereby generating a pressure difference. The present disclosure enables a higher-speed flow of the fluid inside the fluid passage through pressure difference without adding extra power, and generates a faster air speed in a more energy-saving way, thereby achieving a remarkable effect of cooling.

Abstract: Disclosed is an automobile, comprising an automobile body, wheels, a suspension device and a spoiler. The path of a fluid flowing through a lower spoiler surface is longer than the path of the fluid flowing through the upper spoiler surface, so that a lift force generated in the driving process of the automobile is reduced or even eliminated. The general understanding that the wheels bear the dead weight of the automobile, loads and all weights generated by the gravitational acceleration is changed. The dead weight of the automobile body is reduced by the lift force generated by the automobile body, the road holding of the automobile is improved after the wheels eliminate the lift force, and thus, the automobile can save more energy and can run more safely.

Abstract: A suspension automobile comprising an automobile body, wheels and a flow disturbing plate, the wheels connect the flow disturbing plate through connecting devices, and a fluid channel communicating with the outside is formed between the upper surface of the flow disturbing plate and a bottom shell of the automobile body; a power device used for driving the automobile is contained in the body and is suspended along with lift force generated by the body. The invention changes the common sense that the wheels bear all weight generated by the self-weight, loads, and gravitational acceleration of the automobiles when traveling; the body which exceeds 90% by weight of the automobile generates lift force to suspend, the wheels eliminate lift force; meanwhile, a novel propelling force source is found from fluid resistance; the suspension automobile can be driven by various energy including engines and clean energy, thus effectively reduce energy loss.

Abstract: A fluid supercharging device, comprising: a rotating shaft; a vane disc coaxially fixed to the rotating shaft; a plurality of fan blades fixed around a perimeter of the vane disc; the back side of the fan blades being provided with at least one fluid guiding inlet, an end of the back side distal from the vane disc is provided with a fluid guiding outlet, a fluid channel communicating the fluid guiding inlet with the fluid guiding outlet is provided along a lengthwise direction inside the fan blades; the fan blades rotate to generate a centrifugal force such that a fluid flows into the fluid channel via the fluid guiding inlet on the back side, and flows out of the fluid guiding outlet along the lengthwise direction of the fan blades.

Abstract: Provided is a clothing as well as a clothing article having a similar structure of the clothing, the clothing comprising a base layer (200) having an inner surface and an outer surface; the inner surface being substantially planar and forming a first fluid passage (400) with human skin (200); the outer surface being formed as a flow-disturbing face or the outer surface being attached with components having flow-disturbing face; the base layer being provided with at least one through opening (500), through which the first fluid passage being communicated with the flow-disturbing face. The clothing and the clothing article of the present invention is particularly suitable for sports.

Abstract: A fluid supercharging device (3, 5), comprising: a rotating shaft (7); a vane disc (308) coaxially fixed to the rotating shaft (7); a plurality of fan blades (301) fixed around a perimeter of the vane disc (308); the back side of the fan blades 301 being provided with at least one fluid guiding inlet (305), an end of the back side distal from the vane disc (308) is provided with a fluid guiding outlet (306, 307), a fluid channel (304) communicating the fluid guiding inlet (305) with the fluid guiding outlet (306, 307) is provided along a lengthwise direction inside the fan blades; the fan blades (301) rotate to generate a centrifugal force such that a fluid flows into the fluid channel via the fluid guiding inlet on the back side, and flows out of the fluid guiding outlet along the lengthwise direction of the fan blades.

Abstract: The present invention provides a movement device comprising a shell, and an outer fluid channel and an inner fluid channel are sequentially formed in the shell; the outer fluid channel communicates with the outside through a plurality of first ports, and the inner fluid channel communicates with the outside through a plurality of second ports; flow disturbing devices concave and convex relative to the surface are arranged in the outer fluid channel; the pressure difference generated due to different flow speeds between the outer fluid channel and the inner fluid channel serves as the propelling force source of the movement device. A pressure difference transferring circle formed around the shell by the pressure difference between the inner layer and the outer layer is used by the present invention for increasing the traveling speed of the movement device.

Abstract: The invention discloses a flight vehicle generating a lift from an interior thereof. The fluid channel inside the flight vehicle communicates with the engine and the ports on the upper surface of the outer shell. With the powerful suction of the engine, the fluid on the upper surface of the outer shell is quickly sucked into the fluid channel via respective ports under conditions of long path, large area, high speed and low air pressure, which results in large lift from the interior of the flight vehicle. In the course of generating the lift, the fluid resistances of the fluid wall and the fluid hole are sucked into the fluid channel through the ports at the front and the surrounding area of the flight vehicle, then high-speed fluid is emitted from the rear port. This approach contributes greatly to the transformation of the existing flight vehicle. The present invention significantly improves the lift, the speed and the carrying capacity of the existing flight vehicle with lowered energy consumption.

Abstract: The invention discloses an aircraft generating a larger lift from its interior. The fluid channel inside the aircraft communicates with the engine and the ports on the upper surface of the outer shell. With the powerful suction of the engine, the fluid on the upper surface of the outer shell is quickly sucked into the fluid channel via respective ports under conditions of long path, large area, high speed and low air pressure, which results in large lift from the interior of the aircraft. In the course of generating the lift, the fluid resistances of the fluid wall and the fluid hole are sucked into the fluid channel through the ports at the front and the surrounding area of the aircraft, then high-speed fluid is emitted from the rear port. This approach contributes greatly to the transformation of the existing aircraft. The unified big wing significantly improves the lift, the speed and the carrying capacity of the existing aircraft with lowered energy consumption.

Abstract: Disclosed in the present invention is a high-speed aircraft, comprising a shell and an engine, an outer fluid channel and an inner fluid channel being arranged in succession within the shell, the outer fluid channel and the inner fluid channel respectively connecting to the exterior by means of their own air vent; the outer fluid channel is connected to an air suction port of the engine, such that the pressure difference produced by the flow rate within the outer fluid channel being greater than the flow rate within the inner fluid channel acts as the driving force source of the aircraft. Also disclosed in the present invention is an aircraft having greater lift. The present invention provides an innovative method and apparatus for a driving force source obtained from fluid resistance, thus changing the mutual contradiction of a traditional driving apparatus directing external force to itself whilst also needing to use more driving force to overcome fluid resistance.