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公开(公告)号:US4848514A
公开(公告)日:1989-07-18
申请号:US106618
申请日:1987-10-06
申请人: Stephen Snyder
发明人: Stephen Snyder
CPC分类号: B32B15/04 , Y10S428/92 , Y10T428/24331 , Y10T428/31681 , Y10T428/3171
摘要: The present invention relates to a novel sound attenuating system. More particularly, the invention relates to a simpler, lighter, and more effective noise attenuating laminate which is made up of five specific layers of material. The laminate includes a duct liner, a moisture barrier, a fire barrier, acoustic attenuating material, and a solid backing sheet. The laminate is readily inserted into various sections of a jet engine compartment in order to attenuate the sound produced by the jet engine. Hollow rivets are used to conduct acoustical energy to the noise attenuating laminate. This novel means for conducting the acoustical energy to the laminate of the jet engine compartment allows for an improved anti-icing system, for more efficient jet engine operation, and for more efficient dissipation of acoustic energy.
摘要翻译: 本发明涉及一种新型的声音衰减系统。 更具体地说,本发明涉及一种由五个特定材料层组成的更简单,更轻和更有效的噪声衰减层压板。 层压板包括管道衬垫,防潮层,防火屏障,声衰减材料和固体背衬片材。 层压板容易地插入到喷气发动机室的各个部分中,以便减弱由喷气发动机产生的声音。 空心铆钉用于对噪音衰减层压板进行声能。 这种用于对喷气发动机舱的层压板进行声能的新颖手段允许改进的防冰系统,用于更有效的喷气发动机操作,以及更有效地消散声能。
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公开(公告)号:US2312502A
公开(公告)日:1943-03-02
申请号:US33334640
申请日:1940-05-04
发明人: NICHOLAS TESTI
IPC分类号: B65D83/10
CPC分类号: B65D83/10
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公开(公告)号:US4926963A
公开(公告)日:1990-05-22
申请号:US333346
申请日:1989-04-05
申请人: Stephen J. Snyder
发明人: Stephen J. Snyder
CPC分类号: B32B15/04 , B64D2033/0206 , E04B2001/8461 , E04B2001/848 , E04B2001/8495 , G01N2291/02491 , Y10S428/92 , Y10T428/24331 , Y10T428/31681 , Y10T428/3171
摘要: The present invention relates to a novel sound attenuating laminate. More particularly, the invention relates to a simpler, lighter, and more effective noise attenuating laminate which is made up of seven layers of material. The laminate includes a duct liner, a moisture barrier, a first protecting layer, a screen, acoustic attenuating material, a second protecting layer, and a solid backing sheet. The laminate is readily incorporated into various sections of a jet engine compartment in order to attenuate the sound produced by the jet engine. Hollow rivets are used to conduct acoustical energy to the intermediary layers of the noise attenuating laminate.
摘要翻译: 本发明涉及一种新型的减震层压板。 更具体地说,本发明涉及一种由七层材料组成的更简单,更轻,更有效的噪声衰减层压板。 层压板包括管道衬垫,防潮层,第一保护层,筛网,声衰减材料,第二保护层和固体背衬片材。 层压板容易地结合到喷气发动机室的各个部分中,以便减弱由喷气发动机产生的声音。 空心铆钉用于对噪声衰减层压板的中间层传导声能。
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公开(公告)号:US4947958A
公开(公告)日:1990-08-14
申请号:US333345
申请日:1989-04-05
申请人: Stephen J. Snyder
发明人: Stephen J. Snyder
CPC分类号: B32B15/04 , E04B2001/8461 , E04B2001/848 , E04B2001/8495 , G01N2291/02491
摘要: The present invention relates to a novel installation of a sound attenuating laminate. More particularly, the invention relates to the installation of a simpler, lighter, and more effective noise attenuating laminate which is made up of seven layers of material. The laminate includes a duct liner, a moisture barrier, a first protecting layer, a screen, acoustic attenuating material, a second protecting layer, and a solid backing sheet. The laminate is readily incorporated into various sections of a jet engine compartment in order to attenuate the sound produced by the jet engine. Hollow rivets are used to conduct acoustical energy to the intermediary layers of the laminate. This novel means for conducting the acoustical energy to the intermediary layers of the laminate also allows for an improved anti-icing system, for more efficient jet engine operation, and for more efficient dissipation of acoustic energy.
摘要翻译: 本发明涉及一种声音衰减层压板的新颖安装。 更具体地,本发明涉及由七层材料构成的更简单,更轻和更有效的噪声衰减层压板的安装。 层压板包括管道衬垫,防潮层,第一保护层,筛网,声衰减材料,第二保护层和固体背衬片材。 层压板容易地结合到喷气发动机室的各个部分中,以便减弱由喷气发动机产生的声音。 空心铆钉用于向层压板的中间层传导声能。 这种用于对层压体的中间层进行声能的新颖手段还允许改进的防冰系统,用于更有效的喷气发动机操作以及更有效地消散声能。
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公开(公告)号:US2727877A
公开(公告)日:1955-12-20
申请号:US33334653
申请日:1953-01-26
申请人: MONSANTO CHEMICALS
发明人: PARK HAROLD F
CPC分类号: C08G12/46 , C08F8/00 , C08L61/20 , C08L2666/04 , C08F28/00
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公开(公告)号:US1507734A
公开(公告)日:1924-09-09
申请号:US33334619
申请日:1919-10-25
申请人: SINGER MFG CO
发明人: MARTIN HEMLEB
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