Eccentric exhaust muffler for use with auxiliary power units
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F01N-001/02
F01N-001/08
F01N-001/00
F01N-001/10
출원번호
US-0198443
(2005-08-05)
등록번호
US-7367424
(2008-05-06)
발명자
/ 주소
Brown,Daniel V.
Asplund,Kyle D.
Michalski, Jr.,Joseph W.
출원인 / 주소
Honeywell International, Inc.
대리인 / 주소
Ingrassia Fisher & Lorenz
인용정보
피인용 횟수 :
21인용 특허 :
21
초록▼
A muffler system is provided for use with an auxiliary power unit. In one embodiment, and by way of example only, the system includes an outer can, an annular baffle, and a tube. The outer can has a sidewall including a forward end, an aft end, and a cavity extending therebetween. The sidewall is d
A muffler system is provided for use with an auxiliary power unit. In one embodiment, and by way of example only, the system includes an outer can, an annular baffle, and a tube. The outer can has a sidewall including a forward end, an aft end, and a cavity extending therebetween. The sidewall is disposed about a first longitudinal axis, and the cavity has a first cross-sectional area and a smaller second cross-sectional area. The annular baffle is coupled to and extends radially inward from the outer can sidewall and has an opening that is disposed about a second longitudinal axis that is non-coincident with the first longitudinal axis. The tube extends through the annular baffle opening and is spaced apart from the annular baffle to define a radial gap therebetween, comprises acoustic material, and has a length and a substantially uniform cross-sectional area along the length.
대표청구항▼
We claim: 1. A muffler system comprising: an outer can having a sidewall including a forward end, an aft end, and a cavity extending therebetween, the forward end of the sidewall disposed symmetrically about a first longitudinal axis, and the cavity having a first cross-sectional area proximate the
We claim: 1. A muffler system comprising: an outer can having a sidewall including a forward end, an aft end, and a cavity extending therebetween, the forward end of the sidewall disposed symmetrically about a first longitudinal axis, and the cavity having a first cross-sectional area proximate the forward end and a second cross-sectional area proximate the aft end that is smaller than the first cross-sectional area; an annular baffle coupled to and extending radially inward from the outer can sidewall, the annular baffle having an opening that is disposed symmetrically about a second longitudinal axis, the second longitudinal axis being non-coincident with the first longitudinal axis; and a tube extending through the annular baffle opening and spaced apart from the annular baffle to define a radial gap therebetween, the tube having a length and a substantially uniform cross-sectional area along the length and comprising acoustic material having a resistance of greater than zero. 2. The system of claim 1, wherein the outer can farther comprises a forward annular wall coupled to and extending radially inward from the outer can sidewall, the forward annular wall having an opening that is disposed about the second longitudinal axis. 3. The system of claim 2, wherein the outer can farther comprises an aft annular wall coupled to and extending radially inward from the outer can sidewall, the aft annular wall having an opening that is disposed about the second longitudinal axis. 4. The system of claim 1, wherein the outer can is conical. 5. The system of claim 1, further comprising at least one fixed joint coupled to an outer peripheral surface of the annular baffle. 6. The system of claim 1, further comprising a compressible seal disposed in the radial gap. 7. The system of claim 1, wherein the acoustic material comprises fiber metal. 8. The system of claim 1, wherein the acoustic material comprises perforated metal. 9. The system of claim 1, wherein the annular baffle is suspended from the outer can sidewall. 10. The system of claim 9, further comprising at least one fixed joint coupled between an outer peripheral surface of the annular baffle and the outer can sidewall. 11. A muffler system for use with an auxiliary power unit disposed in an aircraft, the system comprising: an outer can having a sidewall, a forward annular wall, an aft annular wall, and a cavity extending between the forward annular wall and the aft annular wall, the sidewall having a forward end and an aft end, the forward end disposed symmetrically about a first longitudinal axis, and the sidewall having a first section and a second section, the forward annular wall extending radially inward from the sidewall first section and including an opening formed therein that is disposed symmetrically about a second longitudinal axis, the second longitudinal axis being non-coincident with the first longitudinal axis, the aft annular wall extending radially inward from the sidewall second section and including an opening formed therein that is disposed about the second longitudinal axis, and the cavity having a first cross-sectional area proximate the forward end and a second cross-sectional area proximate the aft end that is smaller than the first cross-sectional area; an annular baffle extending radially inward from the outer can sidewall and disposed between the forward annular wall and the aft annular wall, the baffle having an opening disposed about the second longitudinal axis; and a tube extending through the annular baffle opening and spaced apart from the annular baffle to define a radial gap therebetween, the tube having a length and a substantially uniform cross-sectional area along the length and comprising acoustic material having a resistance of greater than zero. 12. The system of claim 11, further comprising a compressible seal disposed in the radial gap. 13. The system of claim 12, wherein the compressible seal is coupled to the outer can sidewall. 14. The system of claim 12, wherein the compressible seal is coupled to the tube. 15. The system of claim 11, wherein the acoustic material comprises fiber metal. 16. The system of claim 11, wherein the acoustic material comprises perforated metal. 17. A muffler system for use with an auxiliary power unit disposed in an aircraft, the aircraft having a sidewall, the system comprising: an outer can having a sidewall having a forward end, an aft end, and a cavity extending therebetween, the forward end disposed symmetrically about a first longitudinal axis, and the cavity having a first cross-sectional area proximate the forward end and a second cross-sectional area proximate the aft end that is smaller than the first cross-sectional area; a forward annular wall coupled to and extending radially inward from the outer can sidewall, the forward annular wall having an opening that is disposed symmetrically about a second longitudinal axis, the second longitudinal axis being non-coincident with the first longitudinal axis; an aft annular wall coupled to and extending radially inward from the outer can sidewall, the aft annular wall having an opening that is disposed about the second longitudinal axis; an annular baffle coupled to and extending radially inward from the outer can sidewall, the annular baffle disposed between the forward annular wall and the aft annular wall and having an opening that is disposed about the second longitudinal axis; a tube extending through the annular baffle opening and spaced apart from the annular baffle to define a radial gap therebetween, the tube having a length and a substantially uniform cross-sectional area along the length and comprising acoustic material having a resistance of greater than zero; and a compressible seal disposed in the radial gap. 18. The system of claim 17, wherein the annular baffle is suspended from the outer can sidewall. 19. The system of claim 17, wherein the acoustic material comprises fiber metal. 20. The system of claim 17, wherein the acoustic material comprises perforated metal.
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