Acoustic panel with corrugated baffles and septums
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
G10K-011/168
G10K-011/172
B64C-001/40
F02C-007/24
G10K-011/16
B64C-001/00
B64D-033/02
F02K-001/34
출원번호
US-0130398
(2016-04-15)
등록번호
US-9704467
(2017-07-11)
발명자
/ 주소
Nampy, Sreenivas Narayanan
출원인 / 주소
Rohr, Inc.
대리인 / 주소
O'Shea Getz P.C.
인용정보
피인용 횟수 :
0인용 특허 :
13
초록▼
A panel for attenuating noise includes a core, which forms a plurality of cavities vertically between a perforated first skin and a second skin. The core includes an array of corrugations that include a first baffle, a second baffle and a first septum. The cavities include a first cavity that is for
A panel for attenuating noise includes a core, which forms a plurality of cavities vertically between a perforated first skin and a second skin. The core includes an array of corrugations that include a first baffle, a second baffle and a first septum. The cavities include a first cavity that is formed longitudinally between the first baffle and the second baffle and is fluidly coupled with perforations in the first skin. The first septum extends from the first skin and the first baffle to the second skin and the second baffle, and divides the first cavity into fluidly coupled sub-cavities. The first baffle includes a lateral array of baffle ribs. The first septum includes a lateral array of septum ribs that are laterally offset from the baffle ribs.
대표청구항▼
1. A panel for attenuating noise, comprising: a perforated first skin;a second skin; anda core forming a plurality of cavities vertically between the first skin and the second skin, the core including an array of corrugations that include a first baffle, a second baffle and a first septum;the caviti
1. A panel for attenuating noise, comprising: a perforated first skin;a second skin; anda core forming a plurality of cavities vertically between the first skin and the second skin, the core including an array of corrugations that include a first baffle, a second baffle and a first septum;the cavities including a first cavity that is formed longitudinally between the first baffle and the second baffle and is fluidly coupled with perforations in the first skin; andthe first septum extending from the first skin and the first baffle to the second skin and the second baffle, and dividing the first cavity into fluidly coupled sub-cavities;wherein the first baffle includes a lateral array of baffle ribs, and the first septum includes a lateral array of septum ribs that are laterally offset from the baffle ribs. 2. The panel of claim 1, wherein a first of the septum ribs is disposed laterally between a laterally adjacent pair of the baffle ribs. 3. The panel of claim 1, wherein a first of the septum ribs is laterally aligned with a groove portion formed in the first baffle between a laterally adjacent pair of the baffle ribs. 4. The panel of claim 1, wherein the baffle ribs and the septum ribs extend to an interface between the first baffle and the first septum thereby providing the interface with an undulating geometry; andthe first baffle and the first septum are connected to the first skin at the interface. 5. The panel of claim 4, wherein the interface includes a plurality of apertures respectively between adjacent peaks of the undulating geometry. 6. The panel of claim 1, wherein the corrugations are configured to enable draping of the core about a laterally extending axis. 7. The panel of claim 1, wherein the baffle ribs extend along an entire length of the first baffle between the first skin and the second skin; andthe septum ribs extend along an entire length of the first septum between the first skin and the second skin. 8. The panel of claim 1, wherein the first septum includes a plurality of perforations in the septum ribs. 9. The panel of claim 1, wherein the first septum includes a plurality of groove portions, each of the groove portions formed between a respective laterally adjacent pair of the septum ribs; andthe first septum includes a plurality of perforations in the groove portions. 10. The panel of claim 1, wherein the first baffle and the first septum have corrugated configurations. 11. The panel of claim 1, wherein each of the baffle ribs has a trapezoidal cross-sectional geometry; andeach of the septum ribs has a trapezoidal cross-sectional geometry. 12. The panel of claim 1, wherein the first baffle is offset from the first skin by an acute first angle; andthe first septum is offset from the first skin by a second angle. 13. The panel of claim 12, wherein the second angle is substantially equal to the first angle. 14. The panel of claim 12, wherein the second angle is different from the first angle. 15. The panel of claim 1, wherein the panel is configured as a component of an aircraft propulsion system. 16. The panel of claim 1, wherein the array of corrugations is a first array of corrugations, the core further includes a second array of corrugations, and peaks of the first array of corrugations are longitudinally offset from peaks of the second array of corrugations. 17. The panel of claim 1, wherein the array of corrugations is a first array of corrugations, the core further includes a second array of corrugations, and orientations of the first array of corrugations and the second array of corrugations alternate with one another. 18. A panel for attenuating noise, comprising: a perforated first skin;a second skin; anda core forming a plurality of cavities vertically between the first skin and the second skin, the core including an array of corrugations that include a first baffle, a second baffle and a first septum;the cavities including a first cavity that is formed longitudinally between the first baffle and the second baffle and is fluidly coupled with perforations in the first skin; andthe first septum extending from the first skin and the first baffle to the second skin and the second baffle, and dividing the first cavity into fluidly coupled sub-cavities;wherein the first baffle includes a lateral array of baffle ribs that extend along an entire length of the first baffle between the first skin and the second skin; andwherein the first septum includes a lateral array of septum ribs that extend along an entire length of the first septum between the first skin and the second skin. 19. A panel for attenuating noise, comprising: a perforated first skin;a second skin;a core forming a plurality of cavities vertically between the first skin and the second skin, the core including a plurality of baffles and a plurality of septums respectively interposed between the baffles thereby forming an array of corrugations, the baffles including a first baffle and a second baffle, and the septums including a first septum;the cavities including a first cavity formed longitudinally between the first baffle and the second baffle, wherein the first septum longitudinally divides the first cavity into fluidly coupled sub-cavities; anda first end of the first septum connected to the first skin and the first baffle, and a second end of the first septum connected to the second skin and the second baffle;wherein each of the baffles includes a lateral array of baffle ribs, and each of the septums includes a lateral array of septum ribs; andwherein the baffle ribs are configured with the baffles and the septum ribs are configured with the septums to enable draping of the core about a laterally longitudinally extending axis. 20. The panel of claim 1, wherein the baffle ribs project out from the first baffle towards the first skin, and the septum ribs project out from the first septum towards the first skin.
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이 특허에 인용된 특허 (13)
Porte, Alain; Lalane, Jacques; Gantie, Fabrice; Barillot-Creuzet, Jacques, Acoustic processing structure particularly adapted to the air inlet of an aircraft nacelle.
Akishev, Niaz Irekovich; Zakirov, Ildus Muhametgaleevich; Nikitin, Alexandr Vladimirovich, Method for production of sandwich panels with zigzag corrugated core.
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