Experimental investigation of an engine quick-start system with compact air supply for rotorcraft application

Keyphrases

• Accelerated Testing 33%
• Acceleration Engine 33%
• Air Supply 100%
• Air Supply System 66%
• Engine Operation 33%
• Engine Start-up 66%
• Entry Pressure 33%
• Experimental Testing 33%
• Fast Startup 100%
• Flight Operations 33%
• Gas Generator 33%
• Helicopter 33%
• Idle Speed 33%
• Nozzle 66%
• Operation Range 33%
• Rotorcraft 100%
• System Constraints 33%
• System Parameters 33%
• Turboshaft Engine 33%

Engineering

• Air Supply 100%
• Experimental Investigation 100%
• Flight Operation 25%
• Gas Generator 25%
• Idle Speed 25%
• Numerical Study 25%
• Proof-of-Concept 25%
• Rotorcraft 100%
• Supply System 50%
• System Parameter 25%