5 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.

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.