20240043109. CENTRIFUGAL COMPRESSOR BASED ALTITUDE CONTROL DEVICE WITH ACTIVE VALVE SYSTEM simplified abstract (Aerostar International, LLC)

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CENTRIFUGAL COMPRESSOR BASED ALTITUDE CONTROL DEVICE WITH ACTIVE VALVE SYSTEM

Organization Name

Aerostar International, LLC

Inventor(s)

Kevin Anderson of Sunnyvale CA (US)

Keegan Gartner of Mountain View CA (US)

CENTRIFUGAL COMPRESSOR BASED ALTITUDE CONTROL DEVICE WITH ACTIVE VALVE SYSTEM - A simplified explanation of the abstract

This abstract first appeared for US patent application 20240043109 titled 'CENTRIFUGAL COMPRESSOR BASED ALTITUDE CONTROL DEVICE WITH ACTIVE VALVE SYSTEM

Simplified Explanation

The abstract of the patent application describes an altitude control system for an unmanned aerial vehicle (UAV). The system includes a compressor assembly with a plenum, a passive valve assembly connected to one part of the compressor assembly and in fluid communication with the plenum, and an active valve assembly connected to another part of the compressor assembly and in fluid communication with the plenum. The abstract also mentions a method of controlling the altitude of the UAV and the UAV itself.

  • The altitude control system is designed for unmanned aerial vehicles.
  • It includes a compressor assembly that has a plenum, which is a chamber for storing compressed air.
  • The system has a passive valve assembly connected to one part of the compressor assembly. This valve assembly is in fluid communication with the plenum, allowing the flow of air.
  • There is also an active valve assembly connected to another part of the compressor assembly. This valve assembly is also in fluid communication with the plenum.
  • The system provides a method for controlling the altitude of the UAV, allowing precise control over its vertical position.
  • The patent application also covers the UAV itself, which incorporates this altitude control system.

Potential Applications:

  • This altitude control system can be used in various types of unmanned aerial vehicles, such as drones or surveillance aircraft.
  • It can be utilized in applications that require precise altitude control, such as aerial photography, mapping, or scientific research.
  • The system can also be integrated into UAVs used for surveillance or monitoring purposes, allowing them to maintain a specific altitude for extended periods.

Problems Solved:

  • The altitude control system solves the problem of maintaining a specific altitude for unmanned aerial vehicles.
  • It provides a reliable and efficient method for controlling the vertical position of the UAV.
  • The system addresses the need for precise altitude control in various applications, ensuring stability and accuracy during flight.

Benefits:

  • The altitude control system allows unmanned aerial vehicles to maintain a specific altitude, improving their stability and maneuverability.
  • It provides a more efficient and reliable method for controlling altitude compared to traditional systems.
  • The system offers flexibility and adaptability, making it suitable for different types of UAVs and applications.
  • Precise altitude control enhances the accuracy and quality of data collected during aerial missions, such as mapping or scientific research.


Original Abstract Submitted

an altitude control system for an unmanned aerial vehicle includes a compressor assembly defining a plenum therein, a passive valve assembly coupled to a first portion of the compressor assembly and in fluid communication with the plenum, and an active valve assembly coupled to a second portion of the compressor assembly and in fluid communication with the plenum. a method of controlling an altitude of an unmanned aerial vehicle and an unmanned aerial vehicle are also provided.

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