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

An Air Swirler Fuel Atomizer Assembly with Variable Hub to Tip Aspect Ratio

Technology Category/ Market

Category- Combustion Technology

Applications – Gas turbine engines, liquid rocket engines, marine combustors, burners, and any combustor requiring improved fuel-air mixing and atomization.

Industry – Aerospace and Energy

Market -The global internal combustion engine market demand size reached 181,836 thousand units in 2022 and is anticipated to expand at a (CAGR) of 9.2% from 2023 to 2030.

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Problem Statement

  • Current gas turbine combustors suffer from inadequate fuel-air mixing and atomization due to limited control over radial velocity components in existing swirler designs.
  • A novel swirler is needed to introduce variable radial velocity components, addressing the shortcomings of conventional designs and meeting the demand for finer atomization and improved droplet dispersion in diverse combustion systems

Technology

Variable Aspect Ratio Design:

  • The invention introduces a swirler with a varying aspect ratio from entry to exit, allowing control over axial, tangential, and crucially, radial velocity components, enhancing fuel-air mixing.

Sheet Cutter:

  • The design incorporates sheet breakers at the swirler exit, disrupting liquid sheets into ligaments and droplets, facilitating finer atomization even at lower injection pressures.

Improved Flow Guidance:

  • The swirler’s smooth nozzle shape with a variable flow area guides the flow effectively, resulting in higher exit velocity components, contributing to enhanced combustion efficiency.

Enhanced Spray Characteristics:

  • Flexibility to adapt trust computation to specific security requirements.

Adaptability in Design:

  • The invention allows for flexibility in implementing the variable aspect ratio design on either the hub or tip side of the swirler, providing versatility to suit specific combustor requirements.

Key Features/ Value Proposition

User Perspective:

  • Provides combustor engineers with a swirler design enhancing fuel-air mixing and atomization, improving combustion efficiency in applications like gas turbine engines.

Technical Perspective:

  • Introduces a novel swirler with variable aspect ratio, enabling control over axial, tangential, and radial velocities, addressing limitations in current combustor designs.

Questions about this Technology?

Contact for Licensing

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

Research Lab

Prof. Sundararajan T

Department of Mechanical Engineering

Intellectual Property

  • IITM IDF Ref. 1666
  • IN 396359 (PATENT GRANTED)

Technology Readiness Level

TRL- 4

 Technology validated in lab

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