26 results about "Flight experience" patented technology

The invention relates to the technical field of unmanned aerial vehicle autonomous navigation, and discloses a mine unmanned aerial vehicle autonomous route dynamic adjustment system which comprises a multi-mode sensing module, a dynamic environment field potential modeling module, a field potential spatio-temporal evolution prediction module, a route wave function resolving and generating module, an unmanned aerial vehicle platform and flight control module and a self-adaptive calibration module. A safe and smooth air route expected position is generated in a predicted risk potential field by solving an air route wave function equation, and the core of the method is that a self-adaptive calibration module carries out closed-loop feedback adjustment on fusion weight of environment field potential by quantifying trajectory tracking deviation and flight stability deviation of actual flight of an unmanned aerial vehicle. According to the method, the problem that the risk model is solidified and cannot adapt to the dynamic environment in the prior art is solved, so that the unmanned aerial vehicle can autonomously learn and correct the cognition of the unmanned aerial vehicle on the environmental risk according to the actual flight experience, and the autonomous navigation adaptability and safety in the complex dynamic environment are remarkably improved.

The utility model discloses disposable aviation tableware, and relates to the field of disposable tableware, the disposable aviation tableware comprises a dinner plate, two sides of the dinner plate are provided with supporting handles, the dinner plate is internally provided with a supporting pipe, the upper end of the supporting pipe is provided with a clamping groove, and the lower ends of the dinner plate and the supporting pipe are provided with protruding points. A clamping strip ring is arranged at the upper end of the dinner plate, a dinner cover is arranged at the upper end of the dinner plate, a sealing edge is arranged at the side end of the dinner cover, and the dinner plate and the dinner cover are both made of full corn starch. Through the arrangement of the protruding points, the friction force between the dinner plate and the small table plate can be increased, the dinner plate can be effectively prevented from sliding due to jolting in the flying process, accidents such as food spilling or scalding can be avoided, the dining safety of passengers is guaranteed, the passengers can be more relieved during dining, and the service life of the dinner plate is prolonged. Through the detailed consideration, the flight experience of passengers can be improved, and the passengers can feel more comfortable and convenient.

The invention discloses a flight simulation training auxiliary system and method based on intelligent co-pilot, and the system comprises a data collection module which is used for collecting flight data and carrying out the operation monitoring of a college; the voice interaction interface is used for multi-mode state analysis voice interaction; the student model module is used for skill level evaluation and learning style identification; the emotion perception module is used for flight experience identification and risk prediction analysis; the personalized training module is used for training process monitoring, training result analysis and personalized training adjustment; and the decision engine module is used for deeply reinforcing a learning model and assisting a strategy generator. And intelligent and personalized auxiliary support is provided for pilot training. Through real-time data analysis and an adaptive learning algorithm, functions and behaviors of a real copilot are simulated, and targeted guidance is provided for flight trainees. And a complete training ecosystem is formed. And the flexibility and expandability of the system are ensured, and each functional component can be independently optimized and upgraded.

The invention provides a mooring type manned amusement aircraft based on aerodynamic force and a using method thereof, and relates to the technical field of amusement equipment, the mooring type manned amusement aircraft comprises an aircraft body provided with a manned cabin, and an undercarriage is connected to the lower portion of the aircraft body; the power system comprises a plurality of electric rotor devices which are arranged on the aircraft body and are used for providing lift force; one end of the mooring cable assembly is connected with the machine body, and the other end of the mooring cable assembly is connected to a ground base station; the mooring cable assembly comprises a power line used for supplying power to the electric rotor wing device. And the flight control system is arranged in the aircraft body and / or the ground base station, is electrically connected with the electric rotor devices, and is used for controlling the aircraft to lift off, hover and recover. Low-cost and high-frequency operation is achieved through ground power supply, real immersive flexible flight experience can be provided, multiple safety protection is achieved, and safe and reliable operation under various sites is ensured.

The invention discloses a safety system for low-altitude wing-mounted flight and an operation method, the safety system comprises a first steel cable, a swinging rope, a whole-body safety belt and a diving platform, the diving platform is used for being installed on a first supporting structure, the diving platform is used for allowing a user to stand and take off, and the first steel cable extends in the horizontal direction; the two ends of the first steel cable are used for being connected to first steel rings on the two opposite sides of the second supporting structure respectively, the first end of the swinging rope is detachably connected to a first connecting point on the first steel cable, and a whole-body safety belt is arranged at the second end of the swinging rope and can be worn on the trunk part of a user located on the diving platform. Therefore, after a user jumps out of the diving platform, the swinging rope can be driven to do pendulum swinging motion in a vertical plane around the first connecting point. According to the safety system, the pendulum principle is utilized, traditional high-altitude protection equipment is combined, a wing-mounted flight experience mode which is stimulated and relatively safe is provided, and therefore the high threshold needed by traditional wing-mounted flight is lowered, and the technical requirements of traditional wing-mounted flight are lowered.

The utility model provides a linkage tracking device which comprises a fixed stand column, driving assemblies, a carrying cable and a cable-embracing winch connecting assembly, the driving assemblies are respectively fixed on the fixed stand column, each driving assembly comprises a motor and a driving wheel, two ends of the carrying cable are respectively arranged on the driving wheels, and the motor provides power for the driving wheels so as to drive the carrying cable to move. The rope clip winch connecting assembly comprises a rope clip, a hook and an electric winch assembly, the rope clip is located on the carrying rope and moves along with the carrying rope, and the upper end of the hook is rigidly connected with the rope clip; the utility model further provides a flight experience system, the flight experience system comprises a linkage tracking device, a cable and an aircraft, the length of the cable ensures that the aircraft does not make contact with the ground in the cable full-release state, and the cable moves along with the aircraft and conducts automatic induction take-up and pay-off through the electric capstan. A guarantee with an extremely high safety coefficient can be provided for the aircraft, and the safety guarantee problem and the application scene problem of the aircraft in flight are effectively solved.

The invention discloses winch suspension type experience manned flight amusement equipment, belongs to the field of amusement equipment, and aims at solving the problems that existing equipment is short in endurance and poor in safety. The equipment comprises a winch system, a traction rope, an unmanned aerial vehicle and a power supply, the winch system comprises a winch frame, a pulley and an electric winch; a tension sensor is arranged at the electric winch or a traction rope; the unmanned aerial vehicle comprises a body and an experience cabin, and the experience cabin is provided with an intercom device and an infrared distance sensor; the power source supplies power to the electric winch and the unmanned aerial vehicle through power lines. The pulling force sensor can monitor pulling force of the pulling rope, and the electric winch is automatically locked and unwound when the unmanned aerial vehicle breaks down; and the infrared distance sensor can trigger locking of the traction rope during landing. The equipment is stable in endurance, high in safety and capable of providing safe flight experience for experiencers for a long time.

An unmanned aerial vehicle (UAV) includes: a body including a nose and a tail opposite to the nose; a plurality of rotor devices respectively mounted on the body; and a rear obstacle avoidance sensor mounted on a top part of the body, the UAV has a backward flight state of flying in a direction towards the tail and a hover state of stably hovering in a wind-free environment; in the hover state, the body is tilted in a length direction relative to a horizontal direction, so that the nose is higher than the tail; the optical axis of the rear obstacle avoidance sensor is tilted at a greater angle relative to the horizontal direction when the UAV is in the hover state compared to the backward flight state. It can improve the flight efficiency, enhance the overall obstacle avoidance function, and improve the flight experience.

The invention discloses a system and a method for pre-generating a civil aviation electronic boarding pass, and a medium. The system comprises a passenger information module used for storing detail data of all passengers in a flight to be executed; the check-in invitation module is used for determining passengers who do not select seats before a preset moment and sending check-in invitation information; the all seat dispatching module is used for periodically determining passengers to be dispatched in a flight to be executed after a preset moment and automatically dispatching seats; the automatic check-in module is used for automatically handling check-in for the passengers who have selected seats or dispatched seats and meet the online check-in condition; the electronic boarding check module is used for providing electronic boarding checks for passengers who have already checked in and recording the latest data of the boarding checks in a client database, so that the passengers can still inquire and use the boarding checks in a network-free environment. According to the invention, a large amount of paper resources can be saved, the check-in efficiency of passengers can be effectively improved, the working pressure of on-site workers is relieved, and the riding experience of the passengers is optimized.

The application discloses a kind of based on skin electric signal's flight student psychological stress data acquisition method, it is related to machine learning technical field.The technical points of the present application include: collecting the skin electric signal of multiple flight students when flight simulation training, as physiological signal data set;The motion artifact removal is carried out to the skin electric signal collected;The skin electric signal after removing artifact is carried out frequency domain, time domain and nonlinear feature extraction, forms skin electric signal feature set;According to skin electric signal feature set, train psychological stress data acquisition model based on parallel neural network;The skin electric signal of new flight student is input in the psychological stress data acquisition model trained when flight simulation training, and the psychological stress data of new flight student is acquired.The present application can accurately express the fluctuation of psychological state of flight student when carrying out simulation flight training, help flight student summarizes flight experience, and provides help for subsequent flight training of flight student.

This utility model relates to the field of tabletop technology and discloses a multifunctional aviation seat dining table, including a tabletop, a screw adjustment mechanism, a hinge assembly, and a rotatable panel. The screw adjustment mechanism is installed inside the tabletop, and the rotatable panel is hinged to the screw adjustment mechanism. Turning a handwheel drives the screw adjustment mechanism to move, causing the rotatable panel to rotate around the seat body, thereby adjusting the angle of the rotatable panel. The multifunctional aviation seat dining table provided by this utility model, through innovative design and reasonable structural layout, achieves both multifunctionality and high adjustability, providing passengers with a more convenient and comfortable flight experience.

1. Name of the product in this design: Flight Simulator (Two-person Frame Type). 2. Purpose of this design: for flight training and flight experience. 3. The key design feature of this product is its shape. 4. The image or photograph that best illustrates the design's key points: 3D view 1.

1. The name of the design product: aircraft (parrot shuttle AeroPilotX). 2. The use of the design product: This product is designed for sports racing and low-altitude flight experience, suitable for flight performance, flight competition and individual flight entertainment activities in specific venues or open airspace. 3. The design points of the design product: the combination of shape and pattern. 4. The picture or photo that best shows the design points: perspective view 1.

1. Name of the product in this design: Powered Suspension Glider. 2. Intended use of this design: for aviation sports, recreational flying, and flight experiences. 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. 5. The bottom surface of this product is a part that is not easily seen or cannot be seen during use, so the bottom view is omitted.

The invention discloses unmanned aerial vehicle driven flight experience amusement equipment, and belongs to the technical field of amusement equipment. The equipment comprises a pod, an unmanned aerial vehicle, a connecting mechanism, a suspension system and a control system, the pod is used for an experiencer to sit and is provided with a seat, a safety belt and a transparent cabin body; the unmanned aerial vehicle is connected with the pod through a connecting mechanism and can be controlled by an experiencer to deflect front, back, left and right; the suspension system comprises a steel wire rope, an electric hoist and a hanging bracket and is used for lifting the pod; the control system comprises an electric hoist controller and an unmanned aerial vehicle remote controller; the anti-knotting assembly adopts a universal rotating connector and is arranged at the joint of the steel wire rope and the pod. An experiencer can control the unmanned aerial vehicle to drive the pod to move in a limited space to experience flight pleasure, and the unmanned aerial vehicle is suitable for children, parents, lovers and other groups and has the advantages of being high in interestingness and safety.

The utility model belongs to the technical field of flight seat adjustment, particularly relates to a simulated flight seat adjusting device, and aims to solve the problems that an existing traditional simulated flight seat adjusting device generally can only move in a single direction and cannot meet individual requirements of different players in different scenes, simulated flight experience is not real enough, and the simulation effect is poor. In order to solve the problems that in the prior art, the precision and stability of motion control are insufficient, the following scheme is provided, the device comprises a base, a front-back motion mechanism is arranged at the top of the base, a support is installed at the top of the front-back motion mechanism, the front-back motion mechanism is used for driving the support to move front and back, and a support is installed on the support; according to the multi-direction simulation flight platform, the operation requirements of players in multiple directions can be met, the simulation flight experience is more real, the movement direction of the seat can be accurately controlled, and the stability of movement control is improved.

The utility model relates to the technical field of space flight and aviation, in particular to a retractable nose landing gear structure which comprises a nose wheel cabin door, a fuselage body is arranged on one side of the nose wheel cabin door, screws are connected to the surface of the nose wheel cabin door in a threaded mode, and reinforcing angle aluminum is installed on the inner wall of the fuselage body through the screws. And pedal push rods are arranged on one sides of the nose wheel cabin doors. When the undercarriage structure is used, the air flight resistance can be effectively reduced, the flight efficiency is greatly improved, the fuel consumption rate is reduced, better flight experience is provided for pilots, the flight safety is greatly improved, and the undercarriage is prevented from being damaged in the flight process.

The embodiment of the invention discloses a flight experience information electronization method and device. The specific embodiment of the method comprises the following steps: acquiring captain experience information and copilot experience information; the front end checks whether seats in the captain experience information and the copilot experience information conform to a preset rule or not; the background checks whether the experience time, the operation type and the flight stage in the captain experience information and the copilot experience information conform to preset rules or not; and submitting the verified data to an airline for auditing. According to the implementation mode, the electronic filling scheme of the pilot experience time is completed according to the operation condition. And the verification efficiency of the limitation constraint is improved, and a better feedback mode is achieved.

1. Name of the product in this design: Flight Simulator Cabin. 2. Purpose of this design: For use in a flight simulator to provide a more open and immersive flight experience. 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 progress of the official aircraft interior design explicitly addresses the limitations of traditional physical windows within the aircraft cabin. Passenger experience is renovated by integrating advanced hybrid techniques, duplicating an open external field of view, facilitating a sense of connectivity with the surrounding environment, and by simulating an immersive sailing experience of a virtual display.

The utility model discloses an unequal-pitch propeller type rubber string model plane which comprises a plane body, a rotary connecting piece is rotatably arranged at the front end of the plane body, radial unequal-pitch propellers are arranged in the circumferential direction of the rotary connecting piece, detachable wings are movably connected to the upper surface of the middle of the plane body, and a sleeve is rotatably clamped to the tail of the plane body. The tail end of the sleeve extends backwards and is connected with a tail rod, and the tail end of the tail rod is provided with a vertical empennage and a turnover horizontal empennage. According to the technical scheme, through the novel propeller structure, the flight stability is remarkably improved, remote control fusing or countdown fusing can be achieved, and therefore remote control over tilting of an empennage and forced landing are achieved, and the flight experience of a model airplane enthusiast is remarkably improved.

1. Name of the product in this design: Flying Cinema Equipment. 2. Application of this design: This design is intended for use in the field of flight simulation, amusement equipment, flight simulators, driving simulators, dynamic flight theaters, etc., to provide users with a realistic flight experience. 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 invention discloses a game flight control method and device and electronic device.The method comprises the steps that the flight direction and the flight speed of a current virtual player are obtained; according to the flight direction and the flight speed of the current virtual player, in the process of controlling the current virtual player to fly in the game picture, determining a set angle of a blocking surface according to a flight angle of the flight direction of the current virtual player relative to a world coordinate system and a pre-configured first included angle interval, the pre-configured first included angle interval is used for limiting the included angle between the blocking surface and the flight direction, and the blocking surface is used for simulating the resistance of the current virtual player in the flight process; and setting the blocking surface in a preset range of the current virtual player according to the setting angle of the blocking surface, and in the process, simulating real flight by setting the blocking surface, and providing real flight experience for the player.

The invention relates to the technical field of aircraft equipment, in particular to an aircraft passenger cabin cooling system and method.The cooling device comprises a ventilation mechanism, an air supply pipe, a buffer tank, a ventilation box and the like; the branching pipe is matched with the shifting piece on the twisting adjusting disc, so that direct air supply becomes irregular natural air, the influence on air supply of different people is effectively reduced, cold caused by blowing is avoided, meanwhile, the air supply range can be divided through the air adjusting piece, the requirement for cold air in different areas is effectively met, the flight feeling of passengers is improved, and the safety of the passengers is improved. The device is simple in structure, the functions can be achieved without extra power, good practicability and economical efficiency are achieved, and popularization and use of the device are facilitated.

The utility model provides an aircraft roof hanging device, including tensile cable subassembly, cardan joint subassembly, power supply communication conversion subassembly and aircraft roof adapter bracket subassembly, tensile cable subassembly includes support tube and support tube connecting piece, cardan joint subassembly both ends are connected with support tube connecting piece and power supply communication conversion subassembly respectively, and the support tube connecting piece is connected with the power supply communication conversion subassembly. The power supply communication conversion assembly is fixedly provided with a roof adapter bracket assembly, the roof adapter bracket assembly is provided with a hoop, the hoop is connected with an aircraft, and the tensile cable provides safety guarantee and / or power supply and communication for the aircraft through the tensile cable assembly, the universal joint assembly, the power supply communication conversion assembly and the roof adapter bracket assembly respectively. The aircraft top suspension device is applied to multi-degree-of-freedom, power supply and communication aircraft tests and other commercial applications, meets the requirements of flight control debugging such as unlimited endurance, pitching, rolling and yaw turning of an aircraft under different working conditions, ensures normal development of flight tests or flight experiences such as flight control debugging of the aircraft, and is safe and reliable.

The invention provides a logistics guarantee method, device and equipment based on an unmanned aerial vehicle cluster, and a storage medium, and the method comprises the steps: obtaining the coordinates of a supply point and a no-fly zone, recognizing and sorting the passing no-fly zones through a layer-by-layer bypassing algorithm, and calculating a feasible bypassing coordinate point from the nearest no-fly zone, all the feasible points are gathered to form a complete path planning map, the system calculates the shortest path from each supply base to the supply point and forms a distance matrix, the optimal supply base is intelligently matched by combining the cruising ability of the unmanned aerial vehicle, and the surplus material amount is recognized through accurate sortie calculation. When surplus materials are detected, the system searches other reachable to-be-replenished points by using an established distance matrix, judges the secondary replenishment feasibility by comparing flight time with endurance time, continuously collects actual flight path data, counts an optimal flight path according to flight segments and updates a recommended path; and a dynamic optimization mechanism based on actual flight experience is formed, so that unmanned aerial vehicle cluster logistics guarantee is realized.