Solar Balloon reel-down

Case ID:
2024-003

BACKGROUND

Heliotropes are simple unmanned aerial systems (UAS) that operate at zero pressure and deploy payloads for collecting data in fields such as environmental monitoring, aerospace research, emergency response, and infrastructure inspection. These payloads are attached to the UAS by “flight lines”, which are durable cords managed by tethers and reels (unwinders). Keeping the flight lines short during the initial ascent helps prevent unwanted swinging, spinning, or tangling of the payload, thus improving launch stability and control. After reaching a specified altitude or atmospheric layer, extending the flight lines increases the distance between the UAS and payload, helping to minimize spin-induced mechanical disturbances and signal interference. However, existing reel-down systems typically cannot automatically extend the flight lines in response to precise environmental triggers.

SUMMARY OF TECHNOLOGY

The novel reel-down technology developed by OSU engineers addresses these limitations by integrating sensory systems into the payload to automatically trigger line extension at a predetermined altitude. During takeoff, shorter flight lines maintain control and stability, while automatic elongation at optimal atmospheric conditions, detected by environmental and altitude sensors, reduces rotational forces and the potential for data corruption. This system does not require auxiliary power and adds minimal weight, ensuring that deployment is both safe and efficient. By adapting the flight line length in real-time to environmental conditions, the technology enhances payload stability and data quality through the entire mission.

POTENTIAL AREAS OF APPLICATION

  • Professional Drone Solutions
  • High-Altitude Payload for Balloons & Crafts
  • Aerospace Research & Development
  • Infrastructure Inspection Services- Bridges, Powerlines, Pipelines
  • Emergency Response & Disaster Management- Hazardous & Inaccessible Areas

MAIN ADVANTAGES

  • Minimal-Weight
  • Improves Payload Sensor Reliability
  • Improves Payload Stability- Reduces Payload Rotational Forces
  • Air-Traffic Management- Altitude Based Flight-Line Adjustments to Avoid Crowded Altitudes

STAGE OF DEVELOPMENT

  • Prototype

 

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Patent Information:
For Information, Contact:
Amanda Aker
Licensing Associate
Oklahoma State University
(405) 744-1450
amanda.aker@okstate.edu
Inventors:
Zachary Yap
Keywords:
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