Industrial Consultancy & Sponsored Research (IC&SR) , IIT Madras

Anti Air Column Interaction Mounting for Multirotor Aerial Vehicles

Categories for this Invention

Category – UAV (Unmanned Aerial Vehicle), Aerospace & Defense Technologies

Applications – Aerial Photography, Agricultural Monitoring and Crop Management

Industry – Aerospace and Defense, E-commerce

Market – Global multirotor drone market is projected to grow at a CAGR of 13.1% during the forecast period of 2024-2031.

Image Gallery

Problem Statement

  • Increasing payload capacity by enlarging propellers results in undesirable size, weight, and stability issues.
  • While VOOPS allows larger propellers without increasing footprint, it introduces thrust loss and system vibrations due to rotor overlap.
  • Further, vibrations affect performance and stability, particularly in the accelerometer-dependent control systems used for flight stabilization and navigation.

Technology

  • Tilted Rotor Axes for Minimal Air Interaction: The quadcopter’s frame design includes longitudinal members with motor mounts that tilt the rotor axes toward the central axis, reducing air column interaction and improving stability.
  • Wedge-shaped or Inclined Motor Mounts: The motor mounts, which can be wedge-shaped or inclined plane devices, are set at a predetermined angle (5°-25°) to achieve minimal air column overlap and maintain low vibration amplitude (0.1 g or less).
  • Configurable and Modular Design: The quadcopter can feature four, six, or eight longitudinal members, with overlapping rotors (0-35%) to optimize space and performance, and includes components like ESC units, communication units, and landing gear for comprehensive functionality.

Key Features / Value Proposition

Enhanced Payload Capacity:

  • Innovative design allows larger propellers without increasing the quadcopter’s footprint, boosting payload capabilities.

Reduced Air Column Interaction:

  • Tilted rotor axes minimize downwash interference, ensuring smoother and more stable flight performance.

Low Vibration Levels:

  • Optimized rotor overlap and tilt angles achieve vibration amplitudes of 0.1 g or less, enhancing the reliability of accelerometer data.

Compact and Modular Design:

  • Configurable with four, six, or eight longitudinal members, offering flexibility and space efficiency for various applications.

Advanced Motor Mounts:

  • Wedge-shaped or inclined motor mounts set at angles between 5°-25° improve rotor efficiency and flight stability

Integrated Communication and Control Systems:

  • Equipped with ESC units and communication modules for precise speed control and robust data transmission.

Questions about this Technology?

Contact For Licensing

sm-marketing@imail.iitm.ac.in
ipoffice2@iitm.ac.in

Research Lab

Prof. Asokan T

Department of Engineering Design

Intellectual Property

  • IITM IDF Ref. 1383
  • IN 509585 – Patent Granted

Technology Readiness Level

TRL – 5

Technology validated in relevant environment.

error: Content is protected !!