GB201204586D0 - Seamless acoustic liner - Google Patents
Seamless acoustic linerInfo
- Publication number
- GB201204586D0 GB201204586D0 GBGB1204586.0A GB201204586A GB201204586D0 GB 201204586 D0 GB201204586 D0 GB 201204586D0 GB 201204586 A GB201204586 A GB 201204586A GB 201204586 D0 GB201204586 D0 GB 201204586D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- layer
- face
- composite material
- acoustic panel
- acoustic liner
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 239000002131 composite material Substances 0.000 abstract 3
- 238000005553 drilling Methods 0.000 abstract 1
- 239000006262 metallic foam Substances 0.000 abstract 1
- 238000000034 method Methods 0.000 abstract 1
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/60—Assembly methods
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/20—Three-dimensional
- F05D2250/28—Three-dimensional patterned
- F05D2250/283—Three-dimensional patterned honeycomb
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/96—Preventing, counteracting or reducing vibration or noise
- F05D2260/963—Preventing, counteracting or reducing vibration or noise by Helmholtz resonators
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/612—Foam
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Composite Materials (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Multimedia (AREA)
- Laminated Bodies (AREA)
- Soundproofing, Sound Blocking, And Sound Damping (AREA)
Abstract
A composite acoustic panel employed in an inlet passage of a gas turbine engine or turbofan engine of the type fitted to commercial aircraft and comprises a permeable face-layer 8 made of a composite material, an impermeable backing sheet 9 made of a composite material and a sound absorbing layer 10 which may be a metallic foam or metallic honeycomb structure. It is manufactured by a double polymerisation process for the face- layer and the remainder of the acoustic panel and finally a perforation step, such as by drilling spindles or laser to perforate the face-layer according to a pre-determined perforation distribution
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1204586.0A GB2486120B (en) | 2010-03-02 | 2010-03-02 | Seamless acoustic liner |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1204586.0A GB2486120B (en) | 2010-03-02 | 2010-03-02 | Seamless acoustic liner |
Publications (3)
Publication Number | Publication Date |
---|---|
GB201204586D0 true GB201204586D0 (en) | 2012-05-02 |
GB2486120A GB2486120A (en) | 2012-06-06 |
GB2486120B GB2486120B (en) | 2012-10-31 |
Family
ID=46049571
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1204586.0A Active GB2486120B (en) | 2010-03-02 | 2010-03-02 | Seamless acoustic liner |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2486120B (en) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SE536860C2 (en) | 2012-02-23 | 2014-10-07 | Noisetech Hb | A sound absorber |
NL2012692B1 (en) | 2014-04-25 | 2016-07-18 | Fokker Aerostructures Bv | Panel from laminates, as well as method for manufacturing them. |
DE102015113685B4 (en) | 2014-11-27 | 2020-08-06 | East-4D Carbon Technology Gmbh | Air control and noise protection device in a two-stream jet engine and method for its assembly |
US9447576B2 (en) * | 2015-01-09 | 2016-09-20 | Rohr, Inc. | Post bond perforation of a septum in an acoustic panel |
GB201521075D0 (en) * | 2015-11-30 | 2016-01-13 | Short Brothers Plc | Methods, precursors and abrasive blasting masks for manufacturing noise attenuating devices |
WO2018034949A1 (en) * | 2016-08-19 | 2018-02-22 | 3M Innovative Properties Company | Sound-absorbing panels comprising a core consisting of connected cells, wherein some of the cell walls have openings |
US11027372B2 (en) * | 2018-01-10 | 2021-06-08 | Rohr, Inc. | Controlling perforating of an acoustic panel based on sensed optical emissions |
US20200291645A1 (en) * | 2019-03-11 | 2020-09-17 | Rohr, Inc. | Acoustic panel |
FR3095369B1 (en) * | 2019-04-29 | 2023-04-07 | Airbus Operations Sas | Method for manufacturing a sound-absorbing structure using at least one conforming plate, sound-absorbing structure obtained from said process and aircraft comprising said sound-absorbing structure |
US11260641B2 (en) | 2019-05-10 | 2022-03-01 | American Honda Motor Co., Inc. | Apparatus for reticulation of adhesive and methods of use thereof |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2256611B (en) * | 1991-06-13 | 1995-05-31 | British Aerospace | Manufacture of perforated composite structures |
FR2927271B1 (en) * | 2008-02-08 | 2010-07-30 | Aircelle Sa | METHOD FOR DRILLING AN ACOUSTIC PIECE OF A NACELLE OF AN AIRCRAFT |
-
2010
- 2010-03-02 GB GB1204586.0A patent/GB2486120B/en active Active
Also Published As
Publication number | Publication date |
---|---|
GB2486120B (en) | 2012-10-31 |
GB2486120A (en) | 2012-06-06 |
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