Acoustics – Sound-modifying means – Muffler – fluid conducting type
Patent
1995-05-18
1996-12-03
Dang, Khanh
Acoustics
Sound-modifying means
Muffler, fluid conducting type
181214, 181292, F02K 100
Patent
active
055810543
ABSTRACT:
An acoustic liner jet engine inlet barrel is formed from a perforated permeable skin, a honeycomb core, and a solid facesheet, each of which is formed in a one-piece configuration such that at most only a narrow single fore-to-aft splice, or no splice at all, is present in the finished product. The acoustic modal content remains unaffected, thus preserving a high degree of liner effectiveness, increasing the total active acoustic area of the barrel while decreasing its weight, and increasing its durability.
REFERENCES:
patent: 4023644 (1977-05-01), Cowan et al.
patent: 4122672 (1978-10-01), Lowrie
patent: 4235303 (1980-11-01), Dhoore
patent: 4421201 (1983-12-01), Nelsen et al.
patent: 4600619 (1986-07-01), Chee et al.
patent: 4759513 (1988-07-01), Birbragher
patent: 4817756 (1989-04-01), Carr et al.
patent: 4826106 (1989-05-01), Anderson
patent: 4850093 (1989-07-01), Parente
patent: 4969535 (1990-11-01), Arcas et al.
patent: 5014815 (1991-05-01), Arcas et al.
patent: 5025888 (1991-06-01), Arcas et al.
patent: 5175401 (1992-12-01), Arcas et al.
Anderson Robert E.
Parente Charles A.
Anderson Terry J.
Dang Khanh
Grumman Aerospace Corporation
Hoch Jr. Karl J.
LandOfFree
One-piece engine inlet acoustic barrel does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with One-piece engine inlet acoustic barrel, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and One-piece engine inlet acoustic barrel will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-787127