US4174020A
(en)
*
|
1975-07-01 |
1979-11-13 |
Challis Louis A |
Acoustic treatment for fans
|
US4064961A
(en)
*
|
1976-04-05 |
1977-12-27 |
Rohr Industries, Incorporated |
Slanted cavity resonator
|
US4100993A
(en)
*
|
1976-04-15 |
1978-07-18 |
United Technologies Corporation |
Acoustic liner
|
US4106587A
(en)
*
|
1976-07-02 |
1978-08-15 |
The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration |
Sound-suppressing structure with thermal relief
|
US4135603A
(en)
*
|
1976-08-19 |
1979-01-23 |
United Technologies Corporation |
Sound suppressor liners
|
US4189027A
(en)
*
|
1976-08-19 |
1980-02-19 |
United Technologies Corporation |
Sound suppressor liners
|
US4137992A
(en)
*
|
1976-12-30 |
1979-02-06 |
The Boeing Company |
Turbojet engine nozzle for attenuating core and turbine noise
|
FR2376994A1
(en)
*
|
1977-01-11 |
1978-08-04 |
Snecma |
IMPROVEMENTS TO RESONANT CAVITY DEVICES FOR THE REDUCTION OF NOISE IN A DUCT IN THE PRESENCE OF A GAS FLOW
|
JPS5447020A
(en)
*
|
1977-09-22 |
1979-04-13 |
Nissan Motor Co Ltd |
Sound insulating wall for internal combustion engine
|
DK142710B
(en)
*
|
1977-11-10 |
1980-12-29 |
Elektronikcentralen |
Sound absorbing structure.
|
DE2853613C2
(en)
*
|
1977-12-22 |
1984-08-16 |
Rolls-Royce Ltd., London |
Soundproofing device for a ship's gas turbine system
|
GB2038410B
(en)
*
|
1978-12-27 |
1982-11-17 |
Rolls Royce |
Acoustic lining utilising resonance
|
US4294329A
(en)
*
|
1979-12-17 |
1981-10-13 |
Rohr Industries, Inc. |
Double layer attenuation panel with two layers of linear type material
|
US4318453A
(en)
*
|
1979-09-17 |
1982-03-09 |
Rohr Industries, Inc. |
Double layer attenuation panel
|
US4291080A
(en)
*
|
1980-03-31 |
1981-09-22 |
Vought Corporation |
Sound attenuating structural panel
|
JPS6318799Y2
(en)
*
|
1980-12-02 |
1988-05-26 |
|
|
GB2090334B
(en)
*
|
1980-12-29 |
1983-11-16 |
Rolls Royce |
Damping flutter of ducted fans
|
US4421455A
(en)
*
|
1981-12-22 |
1983-12-20 |
The Garrett Corporation |
Duct lining
|
JPS6443297A
(en)
*
|
1987-08-10 |
1989-02-15 |
Yasutaka Hoshino |
Method for making needle hole freely openable and closable
|
JPH0320975U
(en)
*
|
1989-07-10 |
1991-02-28 |
|
|
US5014431A
(en)
*
|
1989-07-24 |
1991-05-14 |
Arnim B. Jebe |
Tool for handling disposable food containing bags
|
GB2236804A
(en)
*
|
1989-07-26 |
1991-04-17 |
Anthony Reginald Robins |
Compound nozzle
|
GB2237323A
(en)
*
|
1989-10-06 |
1991-05-01 |
Coal Ind |
Fan silencer apparatus
|
US5127602B1
(en)
*
|
1989-11-21 |
1995-05-02 |
Federal Express Corp |
Noise reduction kit for jet turbine engines.
|
KR920007624B1
(en)
*
|
1990-10-22 |
1992-09-09 |
대우캐리어 주식회사 |
Muffler for hermetic rotary compressor
|
US5758488A
(en)
*
|
1993-05-11 |
1998-06-02 |
Roderick Thomson |
Core flow expansion chamber device system for reduction of jet turbine engine noise
|
US5644918A
(en)
*
|
1994-11-14 |
1997-07-08 |
General Electric Company |
Dynamics free low emissions gas turbine combustor
|
US5777947A
(en)
*
|
1995-03-27 |
1998-07-07 |
Georgia Tech Research Corporation |
Apparatuses and methods for sound absorption using hollow beads loosely contained in an enclosure
|
US5592813A
(en)
*
|
1995-07-06 |
1997-01-14 |
Avaero |
Hush kit for jet engine
|
EP1342953A1
(en)
*
|
2002-03-07 |
2003-09-10 |
Siemens Aktiengesellschaft |
Gas turbine
|
EP1342952A1
(en)
*
|
2002-03-07 |
2003-09-10 |
Siemens Aktiengesellschaft |
Burner, process for operating a burner and gas turbine
|
GB0206136D0
(en)
*
|
2002-03-15 |
2002-04-24 |
Rolls Royce Plc |
Improvements in or relating to cellular materials
|
DE102004012929B3
(en)
*
|
2004-03-17 |
2005-04-21 |
Dornier Gmbh |
Noise reduction system for gas turbine engine for aircraft has surface cladding for hot gas channel downstream of turbine, with circular perforated plates covering large ends of frustoconical spaces
|
US7033137B2
(en)
|
2004-03-19 |
2006-04-25 |
Ametek, Inc. |
Vortex blower having helmholtz resonators and a baffle assembly
|
US7337875B2
(en)
*
|
2004-06-28 |
2008-03-04 |
United Technologies Corporation |
High admittance acoustic liner
|
US7311175B2
(en)
*
|
2005-08-10 |
2007-12-25 |
United Technologies Corporation |
Acoustic liner with bypass cooling
|
US7401682B2
(en)
*
|
2005-08-10 |
2008-07-22 |
United Technologies Corporation |
Architecture for an acoustic liner
|
US7461719B2
(en)
*
|
2005-11-10 |
2008-12-09 |
Siemens Energy, Inc. |
Resonator performance by local reduction of component thickness
|
DE202006012949U1
(en)
*
|
2006-08-23 |
2007-12-27 |
Mann + Hummel Gmbh |
Silencer for an internal combustion engine
|
US20090025393A1
(en)
*
|
2006-10-31 |
2009-01-29 |
Karl Edward Sheldon |
Auxiliary power unit assembly
|
GB0907578D0
(en)
*
|
2009-05-05 |
2009-06-10 |
Rolls Royce Plc |
A damping assembly
|
US8413443B2
(en)
*
|
2009-12-15 |
2013-04-09 |
Siemens Energy, Inc. |
Flow control through a resonator system of gas turbine combustor
|
JP5804808B2
(en)
*
|
2011-07-07 |
2015-11-04 |
三菱日立パワーシステムズ株式会社 |
Gas turbine combustor and its combustion vibration damping method
|
US8469141B2
(en)
*
|
2011-08-10 |
2013-06-25 |
General Electric Company |
Acoustic damping device for use in gas turbine engine
|
WO2014133770A1
(en)
*
|
2013-03-01 |
2014-09-04 |
United Technologies Corporation |
Gas turbine engine noise reducing nose cone
|
WO2016057186A1
(en)
|
2014-10-08 |
2016-04-14 |
Dresser-Rand Company |
Concentric resonators for machines
|
FR3028886B1
(en)
*
|
2014-11-24 |
2019-09-13 |
Safran Aircraft Engines |
TURBOREACTOR BLOWER NOISE REDUCTION BODY
|
DE102015214709A1
(en)
*
|
2015-07-31 |
2017-02-02 |
Mahle International Gmbh |
Flow channel and ventilation, heating or air conditioning
|
US9472179B1
(en)
*
|
2015-09-05 |
2016-10-18 |
Xiaobing Cai |
Sound absorber
|
US10174675B2
(en)
*
|
2015-12-30 |
2019-01-08 |
General Electric Company |
Acoustic liner for gas turbine engine components
|
US20180281559A1
(en)
*
|
2017-03-29 |
2018-10-04 |
Ford Global Technologies, Llc |
Acoustic air duct and air extraction system with nesting expansion chambers
|
US10532631B2
(en)
|
2017-03-29 |
2020-01-14 |
Ford Global Technologies, Llc |
Acoustic air duct and air extraction system including a plurality of channels having an expansion chamber
|
US10720136B2
(en)
*
|
2017-12-04 |
2020-07-21 |
Zin Technologies, Inc. |
Layered chamber acoustic attenuation
|
SE544189C2
(en)
*
|
2018-02-13 |
2022-02-22 |
Faurecia Creo Ab |
Acoustic damper for a gas duct system
|
US11059559B2
(en)
|
2018-03-05 |
2021-07-13 |
General Electric Company |
Acoustic liners with oblique cellular structures
|
WO2019195189A1
(en)
*
|
2018-04-02 |
2019-10-10 |
Itt Manufacturing Enterprises Llc |
Multi-frequency helmholtz resonator system
|
US11047304B2
(en)
|
2018-08-08 |
2021-06-29 |
General Electric Company |
Acoustic cores with sound-attenuating protuberances
|
US10823059B2
(en)
|
2018-10-03 |
2020-11-03 |
General Electric Company |
Acoustic core assemblies with mechanically joined acoustic core segments, and methods of mechanically joining acoustic core segments
|
JP7172457B2
(en)
*
|
2018-11-05 |
2022-11-16 |
ヤマハ株式会社 |
Sound-absorbing units and sound-absorbing structures
|
JP7310120B2
(en)
|
2018-11-05 |
2023-07-19 |
ヤマハ株式会社 |
sound absorbing structure
|
US11434819B2
(en)
|
2019-03-29 |
2022-09-06 |
General Electric Company |
Acoustic liners with enhanced acoustic absorption and reduced drag characteristics
|
US11008112B2
(en)
*
|
2019-06-07 |
2021-05-18 |
Bryan B. Solstin |
Laminar inducing apparatus
|
US11339720B2
(en)
*
|
2020-02-21 |
2022-05-24 |
Raytheon Technologies Corporation |
Acoustic liner with non-uniform volumetric distribution
|
US11566564B2
(en)
*
|
2020-07-08 |
2023-01-31 |
Raytheon Technologies Corporation |
Acoustically treated panels
|
US11668236B2
(en)
|
2020-07-24 |
2023-06-06 |
General Electric Company |
Acoustic liners with low-frequency sound wave attenuating features
|
US11970992B2
(en)
|
2021-06-03 |
2024-04-30 |
General Electric Company |
Acoustic cores and tools and methods for forming the same
|
US11739698B2
(en)
*
|
2022-01-19 |
2023-08-29 |
General Electric Company |
Aero-acoustically dampened bleed valve
|
US11965425B2
(en)
|
2022-05-31 |
2024-04-23 |
General Electric Company |
Airfoil for a turbofan engine
|