USD926135S1 - Nozzle - Google Patents

Nozzle Download PDF

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Publication number
USD926135S1
USD926135S1 US29/676,779 US201929676779F USD926135S US D926135 S1 USD926135 S1 US D926135S1 US 201929676779 F US201929676779 F US 201929676779F US D926135 S USD926135 S US D926135S
Authority
US
United States
Prior art keywords
nozzle
view
ornamental design
design
broken lines
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.)
Active
Application number
US29/676,779
Inventor
Andrei Evulet
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Jetoptera Inc
Original Assignee
Jetoptera Inc
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Jetoptera Inc filed Critical Jetoptera Inc
Priority to US29/676,779 priority Critical patent/USD926135S1/en
Assigned to Jetoptera, Inc. reassignment Jetoptera, Inc. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: EVULET, ANDREI
Application granted granted Critical
Publication of USD926135S1 publication Critical patent/USD926135S1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
    • F02K1/004—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector by using one or more swivable nozzles rotating about their own axis
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C15/00—Attitude, flight direction, or altitude control by jet reaction
    • B64C15/02—Attitude, flight direction, or altitude control by jet reaction the jets being propulsion jets
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine type 
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/04—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/78—Other construction of jet pipes
    • F02K1/82—Jet pipe walls, e.g. liners
    • 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
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/323—Application in turbines in gas turbines for aircraft propulsion, e.g. jet engines
    • 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
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F05D2240/12—Fluid guiding means, e.g. vanes
    • F05D2240/128—Nozzles
    • 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
    • F05D2250/40—Movement of components
    • F05D2250/43—Movement of components with three degrees of freedom
    • 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
    • F05D2250/60—Structure; Surface texture
    • F05D2250/61—Structure; Surface texture corrugated
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Description

FIG. 1 is a front perspective view of a nozzle showing my new design;
FIG. 2 is a side view of the nozzle in FIG. 1; and,
FIG. 3 is a front view of the nozzle in FIG. 1.
The broken lines shown in the drawings are included for the purpose of illustrating environmental structure and form no part of the claimed design.

Claims (1)

    CLAIM
  1. The ornamental design for a nozzle, as shown and described.
US29/676,779 2017-07-12 2019-01-14 Nozzle Active USD926135S1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US29/676,779 USD926135S1 (en) 2017-07-12 2019-01-14 Nozzle

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US201762531817P 2017-07-12 2017-07-12
US16/033,197 US20190017468A1 (en) 2017-07-12 2018-07-12 Gimballed Augmentation Shroud
US29/676,779 USD926135S1 (en) 2017-07-12 2019-01-14 Nozzle

Related Parent Applications (1)

Application Number Title Priority Date Filing Date
US16/033,197 Continuation US20190017468A1 (en) 2017-07-12 2018-07-12 Gimballed Augmentation Shroud

Publications (1)

Publication Number Publication Date
USD926135S1 true USD926135S1 (en) 2021-07-27

Family

ID=64998794

Family Applications (2)

Application Number Title Priority Date Filing Date
US16/033,197 Abandoned US20190017468A1 (en) 2017-07-12 2018-07-12 Gimballed Augmentation Shroud
US29/676,779 Active USD926135S1 (en) 2017-07-12 2019-01-14 Nozzle

Family Applications Before (1)

Application Number Title Priority Date Filing Date
US16/033,197 Abandoned US20190017468A1 (en) 2017-07-12 2018-07-12 Gimballed Augmentation Shroud

Country Status (2)

Country Link
US (2) US20190017468A1 (en)
WO (1) WO2019014386A1 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR102492920B1 (en) * 2020-10-05 2023-01-31 연세대학교 산학협력단 Airfoil-Shaped Aircraft
US11772809B2 (en) * 2021-11-27 2023-10-03 Airbus Defence and Space GmbH Fuselage for an aircraft with fuselage-integrated tailplane
CN117846807A (en) * 2024-03-07 2024-04-09 中国空气动力研究与发展中心高速空气动力研究所 Combined supersonic jet noise reduction spray pipe

Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7037026B2 (en) * 2001-11-16 2006-05-02 Ab Skf Method for mounting a sleeve on a shaft and a sleeve device for such mounting
US7216476B2 (en) * 2003-12-09 2007-05-15 The Boeing Company Two-axis thrust vectoring nozzle
USD543495S1 (en) * 2006-08-01 2007-05-29 Williams Herbert L Open center turbine
USD659103S1 (en) * 2011-01-10 2012-05-08 John Mezzalingua Associates, Inc. Sealing boot
USD678923S1 (en) * 2010-08-27 2013-03-26 Komet Group Gmbh Connector
US20140260283A1 (en) * 2013-03-12 2014-09-18 Pratt & Whitney Canada Corp. Gas turbine engine exhaust mixer with aerodynamic struts
US20160010489A1 (en) * 2013-05-15 2016-01-14 Ihi Corporation Variable nozzle for aeronautic gas turbine engine
US9758254B2 (en) * 2014-11-11 2017-09-12 The Boeing Company Jet noise suppressor
USD801286S1 (en) * 2015-08-26 2017-10-31 Roxtec Ab Seal
US20180135556A1 (en) * 2016-11-16 2018-05-17 Rolls-Royce Deutschland Ltd & Co Kg Mixer for an engine manufactured from at least one composite material, manufacturing method and manufacturing device
US20180347550A1 (en) * 2017-06-05 2018-12-06 Henry Lewis LaMuth Device providing non-inertial propulsion while conserving propellant mass and method therefor

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB600397A (en) * 1946-08-27 1948-04-07 Fairey Aviat Co Ltd Improvements in or relating to controlling means for high speed aircraft
US2706886A (en) * 1950-06-14 1955-04-26 Honeywell Regulator Co Coordinated hydraulic control apparatus
US2846844A (en) * 1956-01-24 1958-08-12 Ryan Aeronautical Co Variable area thrust deflectoraugmenter for jet engines
US3443775A (en) * 1965-06-23 1969-05-13 Williams Res Corp Flight belt
GB1291586A (en) * 1969-10-23 1972-10-04 Rolls Royce Propulsive jet nozzle assembly
FR2789123B1 (en) * 1999-01-29 2001-04-27 Snecma ELASTIC RING-ORIENTED NOZZLE ACTIVATION SYSTEM FOR A REACTION PROPELLER
FR2841939B1 (en) * 2002-07-04 2006-09-22 Snecma Propulsion Solide MOBILE DIVERGENT ORIENTABLE TUYERE ON CARDAN FOR FUSEE ENGINE
FR2884874B1 (en) * 2005-04-26 2007-06-15 Snecma Moteurs Sa DIRECTIONABLE EJECTION TUYERE OF AN AIRCRAFT ENGINE
FR2960028B1 (en) * 2010-05-12 2016-07-15 Snecma DEVICE FOR ATTENUATING THE NOISE EMITTED BY THE JET OF A PROPULSION ENGINE OF AN AIRCRAFT.
FR3002289B1 (en) * 2013-02-15 2016-06-17 Herakles MOBILE DIVERGENT TUYERE WITH THERMAL PROTECTION SYSTEM

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7037026B2 (en) * 2001-11-16 2006-05-02 Ab Skf Method for mounting a sleeve on a shaft and a sleeve device for such mounting
US7216476B2 (en) * 2003-12-09 2007-05-15 The Boeing Company Two-axis thrust vectoring nozzle
USD543495S1 (en) * 2006-08-01 2007-05-29 Williams Herbert L Open center turbine
USD678923S1 (en) * 2010-08-27 2013-03-26 Komet Group Gmbh Connector
USD659103S1 (en) * 2011-01-10 2012-05-08 John Mezzalingua Associates, Inc. Sealing boot
US20140260283A1 (en) * 2013-03-12 2014-09-18 Pratt & Whitney Canada Corp. Gas turbine engine exhaust mixer with aerodynamic struts
US20160010489A1 (en) * 2013-05-15 2016-01-14 Ihi Corporation Variable nozzle for aeronautic gas turbine engine
US9758254B2 (en) * 2014-11-11 2017-09-12 The Boeing Company Jet noise suppressor
USD801286S1 (en) * 2015-08-26 2017-10-31 Roxtec Ab Seal
US20180135556A1 (en) * 2016-11-16 2018-05-17 Rolls-Royce Deutschland Ltd & Co Kg Mixer for an engine manufactured from at least one composite material, manufacturing method and manufacturing device
US20180347550A1 (en) * 2017-06-05 2018-12-06 Henry Lewis LaMuth Device providing non-inertial propulsion while conserving propellant mass and method therefor

Also Published As

Publication number Publication date
US20190017468A1 (en) 2019-01-17
WO2019014386A1 (en) 2019-01-17

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