Patent ID: 9528468
Filing Date: 2016-12-27
CPC Classification: F02C,F02K,F05D

Claim Text:
1. A noise reduction system comprising: a microjet ring provided at an exhaust side peripheral edge of a main nozzle of a jet engine, and has a plurality of injection pipes formed in a circumferential direction thereof at regular intervals; and a supply path configured to take part of compressed air in from a flow path in an upstream side of a combustor in the jet engine, and to guide the part of compressed air to the plurality of injection pipes, wherein the plurality of injection pipes is configured to inject the part of compressed air to a jet flow exhausted from the main nozzle, the microjet ring is formed so as to be gradually reduced in diameter from an upstream side toward a downstream side of the jet flow, an arc surface is formed at a tip, in the downstream side of the jet flow, of the microjet ring so that the arc surface connects an inner peripheral surface and an outer peripheral surface of the microjet ring, the whole of the arc surface increases in diameter from the upstream side toward the downstream side of the jet flow, a point where the arc surface intersects the inner peripheral surface of the microjet ring is located where a diameter of the inner peripheral surface of the microjet ring is a minimum, a surface of each of the plurality of injection pipes intersects the arc surface at the point where the arc surface intersects the inner peripheral surface of the microjet ring, and openings of the plurality of injection pipes are provided in the arc surface.