[특허]Exhaust silencer with baffles

Hamilton Sundstrand Corporation

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Exhaust silencer with baffles

국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	B64C-001/40 B64C-023/00
미국특허분류(USC)	244/001N; 244/058
출원번호	US-0094179 (2011-04-26)
등록번호	US-8596568 (2013-12-03)
발명자 / 주소	Francisco, Jay M. Napier, James C.
출원인 / 주소	Hamilton Sundstrand Corporation
대리인 / 주소	Kinney & Lange, P.A.
인용정보	피인용 횟수 : 1 인용 특허 : 35

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An exhaust silencer assembly includes an exhaust duct and an exhaust silencer. The exhaust silencer is disposed about the exhaust duct and has a plurality of solid baffles and at least one perforated baffle The exhaust silencer assembly is disposed downstream of an auxiliary power unit and at least partially attenuates the downstream noise of the combustion gases that result from operation of the auxiliary power unit. In one embodiment, at least one of the plurality of solid baffles is disposed to extend axially between generally radially extending solid...

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1. An exhaust silencer assembly comprising: an exhaust duct;an exhaust silencer disposed about the exhaust duct, the exhaust silencer including a plurality of solid baffles and at least one perforated baffle; andan auxiliary power unit arranged in communication with the exhaust duct, and wherein the at least one perforated baffle is disposed at a length along the exhaust duct from the auxiliary power unit that is 100% to 150% of an inner diameter of the exhaust duct,wherein one of the plurality of solid baffles connects to the at least one perforated baffle and extends generally axially to connect to an adjacent one of the plurality of solid baffles or a second similarly perforated baffle both of which extend generally radially around the exhaust duct. 2. The exhaust silencer assembly of claim 1, wherein the at least one perforated baffle includes perforations spaced across substantially an entire surface area thereof. 3. The exhaust silencer assembly of claim 1, wherein the at least one perforated baffle has a first solid portion with no perforations and a second portion with perforations. 4. The exhaust silencer assembly of claim 1, wherein the at least one perforated baffle includes perforations that are holes with a diameter of 0.125 inches (0.32 cm). 5. The exhaust silencer assembly of claim 1, wherein the exhaust duct is a solid structure upstream of the at least one perforated baffle and a perforated structure downstream of the at least one perforated baffle. 6. The exhaust silencer assembly of claim 1, wherein the solid baffles are positioned to form a plurality of chambers, and wherein the at least one perforated baffle is disposed in at least one of the plurality of chambers. 7. The exhaust silencer assembly of claim 6, wherein the perforations comprise between 20 percent and 30 percent of the entire surface area of the perforated baffle. 8. The exhaust silencer assembly of claim 1, further comprising an eductor disposed between the auxiliary power unit and the exhaust duct, wherein a first solid baffle of the plurality of solid baffles is disposed at or adjacent to the eductor. 9. The assembly of claim 8, wherein the at least one perforated baffle has perforations spaced across substantially an entire surface area thereof. 10. The assembly of claim 8, wherein the exhaust duct is a solid structure upstream of the at least one perforated baffle and a perforated structure downstream of the at least one perforated baffle. 11. The assembly of claim 8, wherein the at least one perforated baffle has a first solid portion with no perforations and a second portion with perforations. 12. The assembly of claim 11, wherein one of the plurality of solid baffles connects to the at least one perforated baffle between the first solid portion and the second portion with perforations and extends generally axially to connect to an adjacent one of the plurality of solid baffles or a second similarly perforated baffle both of which extend generally radially around the exhaust duct. 13. An auxiliary power unit assembly, comprising: an auxiliary power unit;an exhaust duct located downstream from the auxiliary power unit for receiving combustion gases emitted from the auxiliary power unit; andan exhaust silencer extending annularly to about the exhaust duct, the exhaust silencer including a plurality of axially spaced solid baffles and at least one perforated baffle, wherein the solid baffles are positioned to form a plurality of chambers, and wherein the at least one perforated baffle is disposed in one of the plurality of chambers at a length along the exhaust duct from the auxiliary power unit that is 100% to 150% of an inner diameter of the exhaust duct. 14. An aircraft tail section comprising: an auxiliary power unit;an eductor disposed downstream from the auxiliary power unit for receiving combustion gases emitted from the auxiliary power unit;an exhaust duct connected to the eductor and extending downstream therefrom to direct the combustion gases out of the aircraft tail section; andan exhaust silencer connected to and extending annularly around a portion of the exhaust duct, the exhaust silencer including a plurality of axially spaced solid baffles and at least one perforated baffle, wherein the solid baffles are positioned to form a plurality of chambers, and wherein the at least one perforated baffle is disposed in one of the plurality of chambers at a length along the exhaust duct from the auxiliary power unit that is 100% to 150% of an inner diameter of the exhaust duct,wherein one of the plurality of solid baffles connects to the at least one perforated baffle and extends generally axially to connect to an adjacent one of the plurality of solid baffles or a second similarly perforated baffle both of which extend generally radially around the exhaust duct. 15. The aircraft tail section of claim 14, wherein the exhaust duct is a solid structure upstream of the at least one perforated baffle and a perforated structure downstream of the at least one perforated baffle.

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이 특허를 인용한 특허 피인용횟수: 1

Todorovic, Predrag. Gas turbine exhaust cone. USP2014078776946.

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