# US 6,718,752 B2 · Deployable segmented exhaust nozzle for a jet engine > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 6,718,752 B2 - Document ID: US6718752B2 - Status: Granted - Kind: B2 - Application number: 10/157,681 - Filed: 2002-05-29 - Published: 2003-12-04 - Granted: 2004-04-13 - Earliest claimed: 2002-05-29 - Assignees: The Boeing Company - Inventors: Eric H. Nesbitt; George W. Butler; David H. Reed - Web page: https://patentgrep.com/patent/US6718752B2 ## CPC - F02K 1/48: Corrugated nozzles - F02K 1/46: Nozzles having means for adding air to the jet or for augmenting the mixing region between the jet and the ambient air, e.g. for silencing (F02K1/28, F02K1/36, F02K1/38 take precedence) - F05D 2300/505: Shape memory behaviour - Y02T 50/60: Efficient propulsion technologies, e.g. for aircraft - F02K: JET-PROPULSION PLANTS (features of jet-propulsion plants common to gas-turbine plants, air intakes or fuel supply control of air-breathing jet-propulsion plants F02C7/00, F02C9/00) - F05D: INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS - Y02T: CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION ## Abstract An exhaust flow nozzle for a jet engine having a plurality of flow altering components extending from a lip portion of a secondary exhaust nozzle that are movable between first and second positions. In the first position the flow altering components are disposed substantially parallel to an exhaust gas flow path and thereby do not produce drag or a reduction of thrust from the engine. In the second position the flow altering components bend or are deformed to project into the exhaust gas flow path exiting from the secondary exhaust nozzle. The flow altering components are comprised of a shape-memory alloy material which deforms in response to heat. One or more additional layers of material are bonded or otherwise coupled to the shape-memory alloy layer of each flow altering component to assist in returning the shape-memory alloy layer to its unheated shape. ## Claims ### Claim 1 A system for reducing noise from an exhaust nozzle associated with a jet engine, comprising: a plurality of exhaust flow altering components spaced apart from one another and extending from a lip of said exhaust nozzle adjacent a flow path of an exhaust flow emitted from said exhaust nozzle; and each of said exhaust flow altering components being deformable from a first position adjacent to said flow path to a second position extending into said flow path of said exhaust flow in response to a control signal applied thereto, to thereby promote at least one of mixing of said exhaust flow with an adjacent airflow and attenuation of noise generated by said jet engine. ### Claim 2 (depends on 1) The system of claim 1, wherein said control signal comprises said exhaust flow; and wherein each of said flow altering components includes a heat sensitive layer of prestressed, shape-memory material. ### Claim 3 (depends on 2) The system of claim 2, wherein said heat sensitive layer of prestressed, shape-memory material comprises an alloy of nickel and titanium. ### Claim 4 (depends on 3) The system of claim 3, wherein said flow altering component further comprises a layer of metal secured to said alloy of nickel and titanium. ### Claim 5 (depends on 2) The system of claim 2, wherein said flow altering component further comprises a layer of a composite secured to said alloy of nickel and titanium. ### Claim 6 (depends on 2) The system of claim 2, wherein said nickel-titanium alloy comprises NITINOL® shape-memory nickel-titanium alloy. ### Claim 7 (depends on 6) The exhaust nozzle of claim 6, wherein said nickel-titanium alloy layer is bonded to said metal layer. ### Claim 8 (depends on 1) The system of claim 1, wherein each of said flow altering components comprise a triangular shape. ### Claim 9 (depends on 1) The system of claim 1, wherein said flow altering component comprises a super elastic layer of nickel-titanium alloy secured to said shape memory alloy. ### Claim 10 (depends on 1) The system of claim 1, wherein said flow altering component includes a conductor for supplying electrical current to said flow altering component to heat said flow altering component. ### Claim 11 An exhaust nozzle for a jet engine for reducing noise emitted from said jet engine, said exhaust nozzle comprising: a circumferential lip portion; a plurality of deformable flow altering components extending from said lip portion and spaced apart from one another circumferentially about said lip portion; and each of said flow altering components being movable relative to said lip portion from a first position extending generally parallel to an exhaust flow path of an exhaust gas flow generated by said jet engine, to a second position protruding into said exhaust flow path in response to experiencing a control signal, to thereby promote mixing of said exhaust gas flow with a separate flow stream and attenuation of noise created by said exhaust gas flow. ### Claim 12 (depends on 11) The exhaust flow nozzle of claim 11, wherein said control signal comprises heat generated from said exhaust gas flow; and wherein said flow altering components each comprise a layer of nickel-titanium alloy operable to change a shape of said flow altering components in response to experiencing said heat from said exhaust gas flow. ### Claim 13 (depends on 11) The exhaust nozzle of claim 11, wherein said flow altering components each comprise a triangular shape. ### Claim 14 (depends on 11) The exhaust nozzle of claim 11, wherein said flow altering components each comprise a nickel-titanium alloy layer secured to a metal layer. ### Claim 15 (depends on 14) The exhaust nozzle of claim 14, wherein said metal layer comprises aluminum. ### Claim 16 (depends on 11) The exhaust nozzle of claim 11, wherein said flow altering components each comprise a nickel-titanium alloy layer secured to a super elastic layer of nickel-titanium. ### Claim 17 (depends on 11) The exhaust nozzle of claim 11, wherein said flow altering components each comprise a layer of NITINOL® shape-memory nickel-titanium alloy. ### Claim 18 (depends on 11) The exhaust nozzle of claim 11, wherein said flow altering components each comprise a conductor for enabling said flow altering components to be heated via an electrical current. ### Claim 19 A method for attenuating noise from a jet engine, comprising: disposing an exhaust nozzle adjacent said jet engine; coupling a plurality of tab-like flow altering components to a portion of said exhaust nozzle such that said tab-like flow altering components extend generally adjacent an exhaust gas flow generated by said jet engine; and controllably deforming said flow altering components such that said components project into said exhaust gas flow to thereby promote mixing of said exhaust gas flow with an adjacent airflow to thus reduce noise generated by said jet engine.