7 results about "Hang-glider" patented technology

This invention discloses an aerial traction propulsion system with beacon guidance function and its control method. The system includes a guidance control end carried by the towed object and a guided propulsion end serving as the aerial flight power source. The two ends are physically connected by a traction rope and transmit data through a communication link. The guidance control end generates guidance information and sends it to the guided propulsion end, which adjusts its flight state accordingly to maintain the traction configuration. The system has a manual mode and an automatic mode. In the automatic mode, the guided propulsion end performs a two-layer control of speed feedforward following and lateral deviation correction. The automatic mode includes two stages: heading hold and heading follow-up. Once heading follow-up is entered, it is irreversible. The system achieves safety protection through distance anomaly detection of the dual-end position data and communication disconnection timeout. This invention does not require complex sensors or dedicated thrust devices on the propulsion end and can be implemented using a general-purpose flight platform, making it suitable for various scenarios such as hang gliding, surfing, and skiing.

An interface apparatus for providing a user with a hang gliding experience in a virtual space includes: a control bar which the user is to grip; a tilt mechanism which supports the control bar from above such that the control bar is tiltable; a force sensor that is provided to the tilt mechanism and that detects a force and a moment which are applied from the user to the control bar; and an input and output section that provides a signal indicative of the force and the moment to a simulation apparatus configured to generate the virtual space and that acquires, from the simulation apparatus, a control signal for controlling the tilt mechanism so as to tilt the control bar.

The invention discloses a split type long-hovering airship type aircraft, relates to the technical field of airship aircrafts, and solves the technical problems of high cost and low safety in the existing technical scheme. The split type long-hovering airship type aircraft comprises a pod, an airship body frame is arranged on the upper wall surface of the pod, and an airship body is arranged on the airship body frame; sub boat bodies are arranged on the boat body frame, the sub boat bodies are connected with the boat body frame through independent mooring ropes and arranged above a pod, and the multiple sub boat bodies are arranged in a staggered mode in the vertical space; by means of the split type design and safety distance isolation of the sub boat bodies, disastrous consequences caused by explosion of a single hydrogen air bag are fundamentally avoided; in combination with a standby hull rapid deployment system, fault redundancy and online repair capability are realized; and expensive helium is replaced by cheap and easily available hydrogen, and airborne equipment can be used for preparation, so that the manufacturing cost and the operating cost of the whole life cycle are greatly reduced.

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.

1. Name of the product in this design: Amusement machine (glider). 2. Intended use of this design: animation and amusement equipment. 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.

The utility model discloses a hang glider separating and releasing mechanism. The mechanism comprises a hoop which is arranged outside an aircraft body in a sleeving mode and comprises a left half hoop and a right half hoop, the left half hoop is connected with a left side hang glider, and the right half hoop is connected with a right side hang glider; one ends of the left half hoop and the right half hoop are fixedly connected, and the other ends of the left half hoop and the right half hoop are inserted and elastically connected through a compressed first-stage separation spring; the piston cylinder is arranged in the aircraft body and is fixedly connected with the aircraft body; a memory alloy circular ring capable of being contracted by heating is arranged in the piston cylinder; a piston is arranged on the memory alloy circular ring; a compressed secondary separation spring is arranged on the periphery of the piston; the limiting stud is used for sequentially penetrating through the hoop and the aircraft body to be fixedly connected with the piston; when the memory alloy circular ring is heated and contracted, the piston drives the limiting stud to move downwards under the action of the second-stage separation spring to release connection between the left half hoop and the right half hoop, and the left half hoop and the right half hoop are opened under the action of the first-stage separation spring to be separated from the aircraft body.