MX2023010210A - Propulsor con control del área de escape del borde posterior del ala. - Google Patents

Propulsor con control del área de escape del borde posterior del ala.

Info

Publication number
MX2023010210A
MX2023010210A MX2023010210A MX2023010210A MX2023010210A MX 2023010210 A MX2023010210 A MX 2023010210A MX 2023010210 A MX2023010210 A MX 2023010210A MX 2023010210 A MX2023010210 A MX 2023010210A MX 2023010210 A MX2023010210 A MX 2023010210A
Authority
MX
Mexico
Prior art keywords
propulsor
area control
exhaust area
trailing edge
wing trailing
Prior art date
Application number
MX2023010210A
Other languages
English (en)
Spanish (es)
Inventor
Mark Douglass Moore
Ian Andreas Villa
Devon Jedamski
Original Assignee
Whisper Aero 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 Whisper Aero Inc filed Critical Whisper Aero Inc
Publication of MX2023010210A publication Critical patent/MX2023010210A/es

Links

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
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • F02K1/1207—Varying effective area of jet pipe or nozzle by means of pivoted flaps of one series of flaps hinged at their upstream ends on a fixed structure
    • 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
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/08—Varying effective area of jet pipe or nozzle by axially moving or transversely deforming an internal member, e.g. the exhaust cone
    • 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
    • B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/04—Arrangement 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
    • 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
    • F05D2250/10—Two-dimensional
    • F05D2250/12—Two-dimensional rectangular
    • 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
    • F05D2250/10—Two-dimensional
    • F05D2250/14—Two-dimensional elliptical
    • F05D2250/141—Two-dimensional elliptical circular
    • 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
    • F05D2260/50—Kinematic linkage, i.e. transmission of position
    • F05D2260/57—Kinematic linkage, i.e. transmission of position using servos, independent actuators, etc.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Exhaust Silencers (AREA)
  • Inorganic Insulating Materials (AREA)
  • Control Of The Air-Fuel Ratio Of Carburetors (AREA)
  • Catching Or Destruction (AREA)
MX2023010210A 2021-03-03 2022-02-24 Propulsor con control del área de escape del borde posterior del ala. MX2023010210A (es)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
US202163156067P 2021-03-03 2021-03-03
US202163156063P 2021-03-03 2021-03-03
US202163156073P 2021-03-03 2021-03-03
US202163156076P 2021-03-03 2021-03-03
PCT/IB2022/051659 WO2022185165A1 (en) 2021-03-03 2022-02-24 Propulsor wing trailing edge exhaust area control

Publications (1)

Publication Number Publication Date
MX2023010210A true MX2023010210A (es) 2023-11-09

Family

ID=83154910

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2023010210A MX2023010210A (es) 2021-03-03 2022-02-24 Propulsor con control del área de escape del borde posterior del ala.

Country Status (9)

Country Link
US (2) US12006891B2 (https=)
EP (1) EP4301971A4 (https=)
JP (2) JP7744433B2 (https=)
KR (1) KR20230161993A (https=)
AU (1) AU2022231432A1 (https=)
CA (1) CA3212144A1 (https=)
IL (1) IL305640A (https=)
MX (1) MX2023010210A (https=)
WO (1) WO2022185165A1 (https=)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US12420936B2 (en) 2023-05-11 2025-09-23 Cosmic Aerospace, Inc. Aerodynamic lifting structures having embedded engines, and associated systems and methods
WO2025251000A1 (en) 2024-05-31 2025-12-04 Whisper Aero Inc. Aircraft with ducted wing and/or ducted tail

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FR2679599A1 (fr) 1991-07-24 1993-01-29 Snecma Perfectionnement aux roues a aubes de turbomachines.
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WO2005085620A1 (ja) 2004-03-02 2005-09-15 Isamu Nemoto 亜音速機推進用可変サイクルエンジン
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GB201215908D0 (en) 2012-09-06 2012-10-24 Rolls Royce Plc Fan blade
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EP2813696B1 (de) * 2013-06-12 2015-12-02 MTU Aero Engines GmbH Schubumlenkvorrichtung sowie Flugtriebwerk
FR3018094B1 (fr) 2014-02-28 2021-12-03 Snecma Rotor de soufflante pour une turbomachine telle qu'un turboreacteur multiflux entraine par reducteur
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Also Published As

Publication number Publication date
WO2022185165A1 (en) 2022-09-09
US20240295198A1 (en) 2024-09-05
KR20230161993A (ko) 2023-11-28
US12006891B2 (en) 2024-06-11
EP4301971A4 (en) 2025-03-26
BR112023017764A2 (pt) 2023-11-21
TW202248090A (zh) 2022-12-16
JP2025178279A (ja) 2025-12-05
AU2022231432A1 (en) 2023-10-12
JP7744433B2 (ja) 2025-09-25
JP2024508933A (ja) 2024-02-28
EP4301971A1 (en) 2024-01-10
US20220349361A1 (en) 2022-11-03
IL305640A (en) 2023-11-01
CA3212144A1 (en) 2022-09-09

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