Available Technologies
# of Displayed Technologies: 3 / 3
Adaptive Landing Pad System for Compact Emergency Aerial Vehicles
TS-072304 — The Need
Emergency aerial vehicles often require compact stowage for trailer transport and reliable landing capabilities on unpredictable terrain such as slopes, sand, or flooded areas. Conventional skid-based landing gear lacks the adaptability and stability needed for these conditions. A lightweig…
- College: College of Engineering (COE)
- Inventors: McCrink, Matthew; Berry, Spencer; Chittari, Aditya; Disotell, Kevin; Nietert, Carson; Park, Jace
- Licensing Officer: Ashouripashaki, Mandana
Compact Scissor-Boom Rotor Deployment for Portable Aerial Vehicles
TS-072303 — The Need
Current small aerial vehicles face significant design constraints when balancing compact storage with the need for sufficient rotor disk area for stable flight. This limitation hinders deployment in critical missions such as emergency personnel transport or humanitarian aid delivery, where …
- College: College of Engineering (COE)
- Inventors: McCrink, Matthew; Brucchieri, Alyssa; Disotell, Kevin; Holthouse, Alex; Jamshaid, Waleed; Park, Jace; Pisano, Anthony; Sharma, Arushi
- Licensing Officer: Ashouripashaki, Mandana
Method for real-time estimation of aeroelastic flutter using the parametric flutter margin
TS-062490 — An exemplary parametric flutter margin method and associated system that can be used to identify the structural dynamic characteristics of an Unmanned Aerial Vehicle’s wing in a series of Ground Vibration Tests (GVTs) and initial flight-testing study.
The Need
In the aerospace industry, ensuring the safety and certification of aircraft is of paramount importance. One critical challenge faced during the certification process is aeroelastic flutter, an unstable phenomenon that can lead to catastrophic consequences. Conventional flight-testing meth…
- College: College of Engineering (COE)
- Inventors: McCrink, Matthew
- Licensing Officer: Randhawa, Davinder
