Patent US4751979A successfully refreshed from Google Patents.
← Back to Patent Explorer
US4751979A Expired / Lapsed US ⏱️ 0.0 years remaining

Engine noise suppression kit for the nacelles of a jet aircraft

Assignee: Airborne Express Inc
•
Filing: 1985-05-16
•
Granted: 1988-06-21
•
Expires: 2005-05-16
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

Abstract An engine noise suppression kit for use on the inside surfaces of the cowlings or doors of conventional jet aircraft nacelles surrounding the jet aircraft engines. Each nacelle cowling or door comprises a skin mounted on a framework made up of longitudinal stringers and transversely extending ribs or formers. The formers divide the inside surface of the nacelle cowlings or doors into bays surrounding the jet engine located within the nacelle. The kit comprises a plurality of sound attenuating modules adapted to be affixed to an adjacent pair of cowling or door formers and to span the bay defined thereby such that at least those bays surrounding the combuster chamber/turbine area of the jet engine are covered by said modules. Each module constitutes a sealed metallic basket comprising a pair of perforated metallic panels spaced from each other by a surrounding metallic framework. The facing surfaces of said metallic panels being covered by silicon rubber-coated glass cloth. Acoustic material fills the remaining space between said panels. The surrounding metallic framework of each module has laterally extending flanges by which the module is attached to those formers defining its respective bay. The modules are arranged end to end in their respective bays.

Inventors

  • 👤 Albert D. Wiseman

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-07 06:03
CPC Classifications
F; F02; F02C; F02C7/00; F02C7/24

Claims Analysis

Total Claims: 20
Claim 1
Independent Claim 161 words
An engine noise suppression kit for use in association with a jet aircraft engine nacelle surrounding a jet engine of the type having a chamber/turbine area, said nacelle being of the type having openable doors, said kit comprising at least one sound attenuation module for each door shaped to conform to the inside surface of at least that portion of its respective door adjacent said combuster chamber/turbine area of said engine, means to mount said at least one module in spaced relationship to the inside surface of said door portion, each of said modules constituting a sealed basket, said basket comprising a pair of perforated panels spaced from each other by and fixed to a surrounding frame work, a layer of acoustical material located between said perforated panels, a protective sheet-like layer located between said acoustical material and each perforated panel to protect said acoustical material from water, fuel, oil and hydraulic fluid, said mounting means being affixed to said framework.
Claim 2
Dependent Claim 161 words
An engine noise suppression kit for use in association with a jet aircraft engine nacelle surrounding a jet engine of the type having a chamber/turbine area, said nacelle being of the type having openable doors, said kit comprising at least one sound attenuation module for each door shaped to conform to the inside surface of at least that portion of its respective door adjacent said combuster chamber/turbine area of said engine, means to mount said at least one module in spaced relationship to the inside surface of said door portion, each of said modules constituting a sealed basket, said basket comprising a pair of perforated panels spaced from each other by and fixed to a surrounding frame work, a layer of acoustical material located between said perforated panels, a protective sheet-like layer located between said acoustical material and each perforated panel to protect said acoustical material from water, fuel, oil and hydraulic fluid, said mounting means being affixed to said framework.
Claim 3
Dependent Claim 141 words
The noise suppression kit claimed in claim 1 wherein each of said doors is of the type comprising a skin affixed to a framework, said framework comprising at least a pair of stringers extending longitudinally of said door adjacent the longitudinal edges thereof and a plurality of formers extending transversely of said door and joining said stringers, said formers dividing the inside surface of said door into transverse bays, said kit comprising a plurality of said sound attenuating modules adapted to be located in at least those bays adjacent said combuster chamber/turbine area of said engine, each of said modules being so shaped so as to be affixed to and extend between an adjacent pair of said formers defining its respective bay, said modules being arranged end-to-end within their respective bays essentially covering said bays, and being spaced from said skin.
Claim 4
Dependent Claim 33 words
The engine noise suppression kit claimed in claim 3 wherein said acoustical material comprises a fibrous mat having sound absorption characteristics within the range of from about 4000 Hz to about 6000 Hz.
Claim 5
Dependent Claim 20 words
The engine suppression kit claimed in claim 1 wherein said perforated panels and said surrounding framework are made of aluminum.
Claim 6
Dependent Claim 23 words
The engine noise suppression kit claimed in claim 1 wherein said protective layers comprise glass cloth coated on one side with silicon rubber.
Claim 7
Dependent Claim 25 words
The engine noise suppression kit claimed in claim 1 wherein all joints and inside edges of said basket are sealed with a silicon adhesive sealant.
Claim 8
Dependent Claim 29 words
The engine noise suppression kit claimed in claim 1 wherein said perforated panels and said framework are contoured to substantially correspond to the adjacent portion of said nacelle skin.
Claim 9
Dependent Claim 128 words
The engine noise suppression kit claimed in claim 2 wherein said panels and said framework of each of said modules are contoured to substantially conform to the adjacent portion of said nacelle skin and the adjacent formers defining the bay for said module, said module framework comprising a pair of end members and a pair of longitudinal side members of Z-shaped cross section having a central web terminating at its longitudinal edges in inner and outer oppositely directed flanges, one of said perforated panels being mounted on said outer flanges, the other of said perforated panels being mounted on said inner flanges, said outer flanges overlying said formers defining said bay for said module, said outer flanges being affixed to said formers and comprising said module mounting means.
Claim 10
Dependent Claim 33 words
The engine noise suppression kit claimed in claim 8 wherein said acoustical material comprises a fibrous mat having sound absorption characteristics within, the range of from about 4000 Hz to about 6000 Hz.
Claim 11
Dependent Claim 20 words
The engine suppression kit claimed in claim 8 wherein said perforated panels and said surrounding framework are made of aluminum.
Claim 12
Dependent Claim 23 words
The engine noise suppression kit claimed in claim 8 wherein said protective layers comprise glass cloth, coated on one side with silicon rubber.
Claim 13
Dependent Claim 25 words
The engine noise suppression kit claimed in claim 2 wherein all joints and inside edges of said basket are sealed with a silicon adhesive sealant.
Claim 14
Dependent Claim 17 words
The engine noise suppression kit claimed in claim 4 wherein said perforated panels are about 37% open.
Claim 15
Dependent Claim 24 words
The engine noise suppression kit claimed in claim 5 wherein each protective layer has its silicon rubber-coated side bonded to the adjacent perforated panel.
Claim 16
Dependent Claim 21 words
The engine noise suppression kit claimed in claim 8 wherein said longitudinal Z-shaped side members each comprises an integral, one-piece element.
Claim 17
Dependent Claim 25 words
The engine noise suppression kit claimed in claim 8 wherein each of said Z-shaped longitudinal side members comprises a planar web portion and separate inner
Claim 18
Dependent Claim 20 words
The engine suppression kit claimed in claim 11 wherein said perforated panels and said surrounding framework are made of aluminum.
Claim 19
Dependent Claim 23 words
The engine noise suppression kit claimed in claim 17 wherein said protective layers comprise glass cloth coated on one side with silicon rubber.
Claim 20
Dependent Claim 25 words
The engine noise suppression kit claimed in claim 18 wherein all joints and inside edges of said basket are sealed with a silicon adhesive sealant.

References Cited (Backward Citations)

US3542152A Cited
US4235303A Cited
US4384634A Cited
US4449607A Cited
US4416349A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1991-06-21 1991-12-21 1992-06-21 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1995-06-21 1995-12-21 1996-06-21 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1999-06-21 1999-12-21 2000-06-21 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag