49 results about "Hang-glider" patented technology

An Ultra Wideband (UWB) short-range radar system is used for the detection of targets in clutter. Examples of targets on the ground include human walkers, crawlers and runners, and vehicles. The UWB sensor can also be used to detect small approaching boats in different levels of sea clutter or airborne targets like hang gliders. One of the primary differences between this device and other UWB radar sensors is the manner in which the bias on the threshold detector is set as well as the logic circuitry used to find targets in clutter while maintaining a low false alarm rate. The processing is designed to detect targets in varying degrees of clutter automatically. There may be no front panel controls other than an ON-OFF switch. The system is lightweight, low-cost, and can be easily installed in minutes.

The invention discloses a tilt rotor vector propeller based on wave energy. The propeller comprises an airframe which is equipped with a wave energy conversion device, an accumulator, and at least two sets of tilt rotor vector propulsion devices. The wave energy conversion device and the tilt rotor vector propulsion devices are connected with the accumulator respectively, and the tilt rotor vector propulsion device comprises a hang-glider, a propulsion mechanism, a tilt drive motor and a tilt frame. One end of the hang-glider is fixed on the airframe, and the tilt frame is supported on the other end of the hang-glider. An output terminal of the tilt drive motor is connected with the tilt frame, and the propulsion mechanism is arranged on the tilt frame. The tilt rotor vector propeller based on the wave energy has the advantages of converting the wave energy into electric energy, supporting long-distance navigation, and realizing complicated actions such as rapid turning and horizontal tumbling and the like.

A man-powered ornithopter-sailplane, which has one or two pair of flapping wings and a hang-glider wing wherein substantially novel femoral and humeral muscular propulsion engines with the aid of which the body members connected thereto form integrated moving-flying and controlling-guiding mechanisms. Femoral arms are fixed to the torso base from which the movements for the wings flapping with respect to axles inclined to a horizontal direction are transmitted through the intermediate links of a kinematic chain. The wings comprise a row of rotational rods arranged therein and provided with elastic feather-like panels which produced during flapping, in a closed or turned position thereof, aerodynamic profiles and corresponding lifting and propulsion aerodynamic forces. The controlling-guiding movements are transmitted from the humeral arms to the flapping wings using movable ball joints. The diversity of movements of the femoral arms, humeral arms, hang-glider wing make it possible to control the flight.

A man-powered ornithopter-sailplane, which has one or two pair of flapping wings and a hang-glider wing wherein substantially novel femoral and humeral muscular propulsion engines with the aid of which the body members connected thereto form integrated moving-flying and controlling-guiding mechanisms. Femoral arms are fixed to the torso base from which the movements for the wings flapping with respect to axles inclined to a horizontal direction are transmitted through the intermediate links of a cinematic chain. The wings comprise a row of rotational rods arranged therein and provided with elastic feather-like panels which produced during flapping, in a closed or turned position thereof, aerodynamic profiles and corresponding lifting and propulsion aerodynamic forces. The controlling-guiding movements are transmitted from the humeral arms to the flapping wings by means of movable ball joints. The diversity of movements of the femoral arms, humeral arms, hang-glider wing make it possible to control the flight.

The invention discloses an airdrop type underwater glider based on water erosion separation extension wings. The airdrop type underwater glider based on the water erosion separation extension wings comprises a shell, a signal device, a buoyancy regulating device, a roll attitude regulating device, a pitch attitude regulating device, a control device and a hang glider extension device, wherein thebuoyancy regulating device, the roll attitude regulating device, the pitch attitude regulating device and the control device are arranged in the shell. The hang glider extension device comprises hanggliders, a first elastic member, water-soluble fiber members and a locking mechanism for locking the hang gliders in the unfolding state. One ends of the hang gliders are fixed in the shell through rotating shafts, the other ends of the hang gliders are fixed outside the shell through the water-soluble fiber members, and the first elastic member is arranged between the hang gliders and the shell and can unfold the hang gliders through elastic force. According to the airdrop type underwater glider based on the water erosion separation extension wings, the entry impact force of wings is reduced,and the airdrop type underwater glider based on the water erosion separation extension wings is more suitable for the application of air-drop. Before air-drop, the wings are in the retracted state, less space is occupied, the airdrop type underwater glider can be conveniently carried on an airplane, and the timeliness is high; and at the same time, a wing extension mechanism does not need to provide additional power devices, the mechanism is simple, and the feasibility is high.

A crane anti-slipping control device which can prevent a heavy project from descending when the motor starting moment becomes small due to electricity or overweight. The invention is connected with the controller of the crane, and a rotating speed collecting device, an executive circuit, a programmable controller, a main order controller with signal interface are arranged on the crane. The CPU inside the programmable controller is stored with the signal of the move direction of the motor collected by the rotating speed signal collecting device, the program comparing rotating speed signal with the initial setting parameter, the program converting the rotating speed signal into travel signal and the comparative program. The invention collects the rotating speed data through a signal collector arranged on the transmission part and inputs the data into the programmable controller to compare with the data set in the controller. The system works normally when the rotating speed data matches the comparing condition; when the rotating speed data exceeds the set data, the order of the programmable controller executes the motion of the electro circuit so as to protect the whole machine.

The invention discloses a novel submersible with folding hang gliders. The novel submersible with the folding hang gliders comprises a hull body. A bow body of the hull body is provided with a bow rudder. Two sides of the middle of the hull body are provided with the symmetrical hang gliders. A tail part of the hull body is provided with a stern fin and a stern rudder. The stern rudder is connected with the hang gliders through the stern fin. The tail part of the hull body is further provided with a direction rudder through a vertical tail fin. The hull body is internally provided with a gravity adjusting mechanism. Two sides in the tail part of the hull body are provided with multiple groups of symmetrically installed hang glider folding and unfolding mechanisms. The submersible is simplein structure, the hang gliders are folded and unfolded in a rear part of the submersible, and a lift force for gliding is provided to the submersible. The hang gliders are longitudinally arranged along a length direction of the hull body of the submersible, and easily folded. Two sides of a gravity center of the submersible are provided with a water tank for adjusting a net buoyance of the submersible. A combined change of the gliding lift force and the net buoyance of the submersible can realize wave-shaped gliding movement of the submersible in the ocean, so the low-noise sailing is realized, and the underwater invisibility of the whole submersible is improved.

The invention relates to the technical field of rockets, in particular to an escape tower, a fairing cover and a booster rocket with remote control hang gliders and tail rudder wings. The escape tower, the fairing cover and the booster rocket are characterized in that the escape tower, the fairing cover and the booster rocket are each provided with one pair of hang gliders and each provided with one vertical tail wing, each vertical tail wing is arranged on the vertical symmetry central plane of the corresponding pair of hang gliders, the tail of one pair of hang gliders is provided with a gliding pose balance wing, the tail of each vertical tail wing is provided with one tail rudder wing, the escape tower, the fairing cover and the booster rocket are each provided with a remote control receiver, a corresponding remote control mechanical driving mechanism and a position signal wireless transmitter, and the escape tower, the fairing cover and the booster rocket can be controlled by a ground control center to land according to a specified site in the falling and gliding process. The recycling difficulty and cost for the remains of the escape tower, the fairing cover and the booster rocket are greatly lowered, and the phenomenon that the danger is brought when remains fall down to villages can be avoided.

The invention discloses an air drop type underwater glider based on electromagnetic span wings. The air drop type underwater glider comprises a shell body, a signal device, a buoyancy force adjustingdevice, a barrel roll attitude adjusting device, a pitch attitude adjusting device and a control device, wherein the buoyancy force adjusting device, the barrel roll attitude adjusting device, the pitch attitude adjusting device and the control device are arranged in the shell body. The air drop type underwater glider further comprises a hang glider stretching device which comprises hang gliders,an electromagnet, a piston, a piston sliding rail, a first elastic element, a second elastic element and a locking mechanism. Under the elastic action of the first elastic element, the magnetic magnitude of the electromagnet is controlled by the control device to enable the piston to slide on the piston sliding rail to realize the location and release of the hang gliders, when the hang gliders arereleased by the electromagnet, and the elastic action of the second elastic element enables the hang gliders to rotate and spread winding a rotary shaft. The air drop type underwater glider based onthe electromagnetic span wings reduces the water-entry impact force of wings, is more suitable for air drop application, the wings are in put-away states before the air drop, occupied space is small,plane carrying is convenient to carry out, and the timeliness is higher.

The invention provides an inflatable hang glider unmanned aerial vehicle and belongs to the technical field of unmanned aerial vehicles. The problems that the hang glider unmanned aerial vehicle storage and transportation space is limited, and rapid orbit transfer cannot be conducted are solved. The inflatable hang glider unmanned aerial vehicle comprises a fuselage and inflatable side wings arranged on the two sides of the fuselage. Each inflatable side wing is composed of a plurality of variable section inflating pipes in a combined mode. The radius of the cross section of each variable section inflating pipe is gradually increased from the front end to the back end. The radiuses of the cross sections of the front ends of all the variable section inflating pipes are the same. The radiuses of the cross sections of the back ends of all the variable section inflating pipes of each inflatable side wing are gradually increased from the outer sides to the inner sides. All the variable section inflating pipes of each inflatable side wing are sequentially connected in a linear mode. The front end of each inflatable side wing is fixedly connected with the fuselage. An X-shaped telescopic mechanism is arranged on the back side of each inflatable side wing. A center shaft of each X unit of the X-shaped telescopic mechanisms is fixedly connected with the corresponding inflatable side wing. Rigid windward plates are arranged on the outer side windward sides of the two inflatable side wings.

The invention relates to a hang glider device with cross-flow fans, which comprises a main body skeleton, wings and an operating lever. The cross-flow fans are installed at the front edges of the wings. Cowlings are arranged below the cross-flow fans. Driving devices are installed on one side of the cowlings. A cabin hanger is hinged with the central part of the main body skeleton. The hang glider device with cross-flow fans has the beneficial effects that the hang glider device can realize vertical lifting and lowering, a runway is not required and a space with area being several square meters only is required; the energy consumption is low and a fraction of the energy consumption of a helicopter; the safety is excellent and the hang glider device can glide under the situation of no power; and when power is available, the stall speed is zero; clean energy such as electric energy and solar energy is used; the linear speed of fan blades is low and the noise is low relative to a propeller structure; the manufacturing cost is low, the hang glider device is simple and convenient to disassemble and assemble and facilities such as hangars are not required; and the hang glider device is simple to control.

The invention provides an inflatable hang glider unmanned aerial vehicle and belongs to the technical field of unmanned aerial vehicles. The problems that the storage and transportation space of a hang glider unmanned aerial vehicle is limited, and quick orbital transfer cannot be achieved are solved. The inflatable hang glider unmanned aerial vehicle comprises a vehicle body and inflatable side wings arranged on the two sides of the vehicle body. Each inflatable side wing is formed by connecting a plurality of ribbed plates which are arrayed in a fan shape through flexible skin in a sealed mode, the flexible skin is adhered to the ribbed plates, and air chambers are formed between every two adjacent ribbed plates through sealing of the flexible skin of the front face, the rear face, the upper face and the lower face. The width of each ribbed plate is gradually increased from the front end to the rear end, the front end widths of all the ribbed plates are the same, and the rear end widths of all the ribbed plates of each inflatable side wing are gradually increased from the outside to the inside. The ribbed plates adopt flat plates which are each of a hollow structure, air holes are formed in the side walls of the ribbed plates of the two sides of each air chamber, the front end of each ribbed plate is connected with a high-pressure air bottle and an inflating control system which are arranged in the vehicle body, and an air discharging electromagnetic valve is arranged at the rear end of each air chamber. The inflatable hang glider unmanned aerial vehicle is applied to the field of unmanned aerial vehicles.

The invention discloses an underwater glider with memory-alloy driving attitude control. The underwater glider comprises a body, a left hang glider, a right hang glider and an empennage. A bow buoyancy chamber, a central buoyancy chamber, a stern buoyancy chamber, a left wing buoyancy chamber and the right wing buoyancy chamber are provided with underwater attitude control devices respectively. The underwater attitude control devices include variable buoyancy chambers and variable adjustment assemblies. A cavity is formed in a cylinder body in a hollow manner; a plunger is installed in a movable passage in the middle of the cylinder block and is in sealed connection with the movable passage; a water storage tank is installed in the movable passage of the cylinder body at the outer end surface of the plunger and is communicated with an external water environment through a through hole; and the plunger moves in the movable passage to drive the water storage tank to expand or contract. Atleast two variable adjusting assemblies are connected and installed between the plunger and the inner wall surrounding the cylinder body. According to the invention the variable buoyancy chamber is pulled to change the buoyancy by the phase change of the memory alloy wire; the deep water pressure can be carried; no moving sealing is involved; the response is fast and the energy consumption is low; and the underwater glider is suitable for the deep-water working environment.

The invention relates to an underwater flight method of a multi-legged robot. The multi-legged robot comprises a main body structure, a first left mechanical leg, a second left mechanical leg, a thirdleft mechanical leg, a first right mechanical leg, a second right mechanical leg, a third right mechanical leg, a control system, a battery pack, a propeller and a sliding board. The multi-legged robot drives a motor to rotate through the mechanical legs in order to make the mechanical legs be merged and form a complete hang glider, realizes free switching between a walking mode and an underwaterflying under the action of the propeller and the sliding board, has self-driving adaptability, and can automatically control working in an optimal power-saving mode. The method has the advantages ofwide operating range, strong environmental adaptability and diverse sports modes, near-distance multidirectional observation can be achieved through crawling during the inspection of an offshore platform pedestal, and convenient switching of working places is achieved in the underwater flying mode, so the exploration research in the project are of great significance for the inspection of offshoreplatforms.

An amusement ride includes a plurality of main arms which are moved by at least one motor along a circular path about a central rotation axis arranged substantially vertical to the ground, or to a platform. The main arms are rotatable about a rotation axis so that a first portion, which extends with respect to the rotation axis, can be raised or lowered with respect to the ground. The ride further includes at least one seat for at least one rider connected to the first portion of the main arm, at least one movable aerodynamic surface, and a control device for modifying the angle of incidence of the aerodynamic surface with respect to the air flow impacting it during the rotation of the main arm about the central axis.

The invention belongs to the technical field of wading robots, particularly relates to a vector propulsion hybrid drive underwater robot, and solves the technical problems in the background technology. The robot comprises a robot body, a rotatable camera, a hang glider, a plurality of side propelling devices, a horizontal propelling device, a plurality of tail stabilizing wings, a gravity center adjusting mechanism, a control box, a power source, a horizontal foot stool and a buoyancy adjusting mechanism. When the underwater robot sails, the underwater robot can sail in water by adjusting the position of the gravity center and the buoyancy and by means of the hang glider and the tail stabilizing wing, and the underwater robot has the advantages of being low in energy consumption, low in noise, large in moving range, high in concealment and the like. The foot stool of the underwater robot is telescopic, so that underwater landing can be realized in complex submarine topography, and underwater operation is facilitated; when the underwater robot performs high-precision operation, local propulsion can be realized through the side propulsion device and the tail propulsion device; in case of emergency, quick transfer can be realized.

The invention provides an inflatable hang glider unmanned aerial vehicle and belongs to the technical field of unmanned aerial vehicles. The problems that the hang glider unmanned aerial vehicle storage and transportation space is limited, and rapid orbit transfer cannot be conducted are solved. The inflatable hang glider unmanned aerial vehicle comprises a fuselage and inflatable side wings arranged on the two sides of the fuselage. Each inflatable side wing is composed of a plurality of rib plates which are arranged in a fan-shaped mode and are in sealing connection through flexible skins. The flexible skins and the rib plates are bonded. Every two adjacent rib plates are sealed through the front-surface flexible skin, the back-surface flexible skin, the upper-surface flexible skin and the lower-surface flexible skin to form an air chamber. The width of each rib plate is gradually increased from the front end to the back end. The widths of the front ends of all the rib plates are the same. The widths of the back ends of all the rib plates of each inflatable side wing are gradually increased from the outer sides to the inner sides. Each rib plate adopts a triangular plate of a hollow structure. Air holes are formed in the side walls of the rib plates on the two sides of each air chamber. The front end of each rib plate is connected with a high-pressure gas cylinder and an inflating control system which are arranged in the fuselage. An exhaust electromagnetic valve is arranged at the back end of each air chamber.

A hang glider control device may include a cross bar having a first end, a second end, a central region, a first central arm, and a second central arm. The first central arm and the second central arm may be coupled opposingly to the central region. The first end may be formed by a portion of the first central arm distal to the central region, and the second end may be formed by a portion of the second central arm distal to the central region. The first end of the cross bar may be configured to couple the cross bar to the first upright above the base tube, and the second end of the cross bar may be configured to couple the cross bar to the second upright above the base tube so that the crossbar may be generally parallel to the base tube.

Detachable heat-retaining gloves apply to baby carriages, silver cars, wheelchairs, hand cars, pet carriages, hang gliders, bicycles, sticks, and so on in order to keep hands warm and make them cold resistance in the winter season, which is detachably mounted on any baby carriage, which allows a user to freely moves his or her hands, and which can prevent a loss of the gloves through the user's carelessness since there is no need to separately keep the gloves after taking off them. Each of the detachable heat-retaining gloves includes a body of a tumbling doll shape symmetrically formed and being foldable at a central portion thereof; a heat-retaining member joined along the inner face of the body; an outer skin member joined along the outer face of the body; first and second zippers joined along both side edges of the body to form a receiving portion inside the body; and a separation-preventing ring mounted at one side of the inner face of the body, wherein the body further comprises a cross-shaped (+) or straight-shaped (−) fitting portion formed on one side of a lower portion of the body.

The invention discloses a tilt rotor vector propeller based on wave energy. The propeller comprises an airframe which is equipped with a wave energy conversion device, an accumulator, and at least two sets of tilt rotor vector propulsion devices. The wave energy conversion device and the tilt rotor vector propulsion devices are connected with the accumulator respectively, and the tilt rotor vector propulsion device comprises a hang-glider, a propulsion mechanism, a tilt drive motor and a tilt frame. One end of the hang-glider is fixed on the airframe, and the tilt frame is supported on the other end of the hang-glider. An output terminal of the tilt drive motor is connected with the tilt frame, and the propulsion mechanism is arranged on the tilt frame. The tilt rotor vector propeller based on the wave energy has the advantages of converting the wave energy into electric energy, supporting long-distance navigation, and realizing complicated actions such as rapid turning and horizontaltumbling and the like.

The invention discloses a low-power-consumption self-heaving submerged buoy based on a hang glider, and belongs to the field of underwater fixed-point observation platforms. The submerged buoy comprises a submerged buoy body, wherein an unpowered hang glider is arranged above the submerged buoy body; the unpowered hang glider comprises a delta wing, the axis of the delta wing is parallel to the axis of the submerged buoy body, the tip of the delta wing is located over the bow of the submerged buoy body, and an empennage is rigidly fixed to the center of the tail of the delta wing. A battery pack and a driving mechanism used for driving the battery pack to move back and forth in the axis direction of the submerged marker body are arranged in the submerged marker body. A water depth control module is arranged on the bow portion of the submerged buoy body and comprises an inner oil bag, an outer oil bag, an oil way and a hydraulic pump. According to the underwater buoy, the large-area triangular hang gliders are additionally arranged above the underwater buoy body, and the pitching attitude of the underwater buoy body is adjusted in cooperation with the movable battery pack and the water depth control module, so that the fluid generates heaving force on the hang gliders, the floating and diving processes of the underwater buoy are accelerated, and the total power consumption is reduced.

The present disclosure describes a multipurpose airfoil assembly including a body, at least one pair of wings, and a control system. The body provides a structural connection for the wings. At least one of the pairs of wings has forward swept leading edges and forward swept trailing edges. The shape of the airfoil assembly can range from that of a traditional airframe to a natural leaf like structure. The airfoil assembly can also include a rudder. A control system is provided for directionally controlling the airfoil assembly during its operation. The airfoil assembly can be readily adapted to configurations suitable for a kite, a hang glider, a parachute, and a sail.

The invention provides a novel photovoltaic panel solar aircraft which comprises wings, an empennage and a fuselage, solar photovoltaic panels are arranged on the upper side faces of the wings, a storage bin arranged along the fuselage is arranged on the side edge of the fuselage, and folding type photovoltaic film hang gliders are stored in the storage bin. First equidistant telescopic parts and second equidistant telescopic parts are arranged on the front sides and the rear sides of the photovoltaic film hang gliders correspondingly, by arranging the first equidistant telescopic parts, the second equidistant telescopic parts and the folding type photovoltaic films, the conversion capacity of photovoltaic cells can be effectively improved, more power is provided, and therefore the bearing capacity is improved; by arranging the self-adjusting seat, a self-adjusting effect can be achieved when the airplane jolts, so that the riding comfort is improved; the take-off and landing site can cooperate with the information photovoltaic panel solar aircraft to take off and land, so that structures such as an undercarriage and the like can be omitted, and the bearing capacity is further improved.

The invention discloses an air drop type underwater glider based on electromagnetic span wings. The air drop type underwater glider comprises a shell body, a signal device, a buoyancy force adjustingdevice, a barrel roll attitude adjusting device, a pitch attitude adjusting device and a control device, wherein the buoyancy force adjusting device, the barrel roll attitude adjusting device, the pitch attitude adjusting device and the control device are arranged in the shell body. The air drop type underwater glider further comprises a hang glider stretching device which comprises hang gliders,an electromagnet, a piston, a piston sliding rail, a first elastic element, a second elastic element and a locking mechanism. Under the elastic action of the first elastic element, the magnetic magnitude of the electromagnet is controlled by the control device to enable the piston to slide on the piston sliding rail to realize the location and release of the hang gliders, when the hang gliders arereleased by the electromagnet, and the elastic action of the second elastic element enables the hang gliders to rotate and spread winding a rotary shaft. The air drop type underwater glider based onthe electromagnetic span wings reduces the water-entry impact force of wings, is more suitable for air drop application, the wings are in put-away states before the air drop, occupied space is small,plane carrying is convenient to carry out, and the timeliness is higher.

An inflatable hang gliding UAV belongs to the field of UAV technology and solves the problems of limited storage and transportation space and inability to quickly change orbits of the hang gliding UAV. It includes a fuselage and inflatable Each inflatable wing is composed of a plurality of fan-shaped ribs sealed and connected by a flexible skin, the flexible skin is bonded to the ribs, and the front, rear, upper, lower The four sides of the flexible skin are sealed to form an air chamber. The width of each rib gradually increases from the front end to the rear end, and the width of the front end of all the ribs is the same. Large, the ribs are triangular plates with a hollow structure, air holes are set on the side walls of the ribs on both sides of each air chamber, and the front end of each rib is connected with the high-pressure gas cylinder and the inflation control system installed in the fuselage An exhaust solenoid valve is arranged at the rear end of each air chamber; the invention is used for drones.

The invention discloses an exhibition item device for simulating wing-mounted flight extreme sports. A simulation gliding mechanism of the device comprises a hang glider model, a universal joint, a support, a holding rod and a nine-axis sensor, the universal joint is arranged on the top surface of the hang glider model, the support is connected with the universal joint and enables the hang glider model to be erected in front of a display screen, the holding rod is arranged on the bottom surface of the hang glider model, the nine-axis sensor is embedded in the hang glider model, the nine-axis sensor, the display screen and the audio playing device are in communication connection with a multimedia workstation, and after the holding rod drives the hang glider model to move with the universal joint as the fulcrum, the nine-axis sensor outputs signals and transmits the signals to the multimedia workstation, the multimedia workstation controls the display screen to play corresponding pictures according to output signals of the nine-axis sensor and controls the audio playing device to play corresponding audios at the same time. According to the exhibition item device, the virtual reality technology is combined with the flight equipment, so that an experiencer feels the fun of wing-mounted flight, potential safety hazards are avoided, and the interestingness and competitiveness of the exhibition item are enhanced.