GB202202234D0 - Exhaust nozzle - Google Patents

Exhaust nozzle

Info

Publication number
GB202202234D0
GB202202234D0 GBGB2202234.7A GB202202234A GB202202234D0 GB 202202234 D0 GB202202234 D0 GB 202202234D0 GB 202202234 A GB202202234 A GB 202202234A GB 202202234 D0 GB202202234 D0 GB 202202234D0
Authority
GB
United Kingdom
Prior art keywords
exhaust nozzle
exhaust
nozzle
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.)
Pending
Application number
GBGB2202234.7A
Other versions
GB2615794A (en
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.)
BAE Systems PLC
Original Assignee
BAE Systems PLC
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 BAE Systems PLC filed Critical BAE Systems PLC
Priority to GB2202234.7A priority Critical patent/GB2615794A/en
Publication of GB202202234D0 publication Critical patent/GB202202234D0/en
Priority to PCT/GB2023/050273 priority patent/WO2023156760A1/en
Publication of GB2615794A publication Critical patent/GB2615794A/en
Pending legal-status Critical Current

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
    • F02K1/28—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow
    • 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
    • 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
    • F02K1/28—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow
    • F02K1/30—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow for varying effective area of jet pipe or nozzle
    • 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
    • F02K1/44—Nozzles having means, e.g. a shield, reducing sound radiation in a specified direction
    • 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
    • F05D2250/11—Two-dimensional triangular
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
GB2202234.7A 2022-02-18 2022-02-18 Exhaust nozzle Pending GB2615794A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB2202234.7A GB2615794A (en) 2022-02-18 2022-02-18 Exhaust nozzle
PCT/GB2023/050273 WO2023156760A1 (en) 2022-02-18 2023-02-08 Exhaust nozzle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2202234.7A GB2615794A (en) 2022-02-18 2022-02-18 Exhaust nozzle

Publications (2)

Publication Number Publication Date
GB202202234D0 true GB202202234D0 (en) 2022-04-06
GB2615794A GB2615794A (en) 2023-08-23

Family

ID=80934438

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2202234.7A Pending GB2615794A (en) 2022-02-18 2022-02-18 Exhaust nozzle

Country Status (1)

Country Link
GB (1) GB2615794A (en)

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2004061286A1 (en) * 2002-12-18 2004-07-22 Lockheed Martin Corporation Apparatus and method for controlling primary fluid flow using secondary fluid flow injection
SE527829C2 (en) * 2004-11-05 2006-06-13 Volvo Aero Corp Outlet nozzle for a jet engine and method for controlling a gas flow from the jet engine
FR2884560B1 (en) * 2005-04-14 2007-05-25 Snecma Moteurs Sa EJECTION TUBE OF A FLYING ENGINE ENGINE
FR2900389B1 (en) * 2006-04-28 2009-01-16 Snecma Sa PROPULSION GAS EXHAUST ASSEMBLY IN A CORRELATED AIRCRAFT AIRCRAFT
CN101787937B (en) * 2010-02-08 2013-04-17 北京航空航天大学 Porous wall expanding type dual throat nozzle
CN111577480A (en) * 2020-05-26 2020-08-25 中国航发沈阳发动机研究所 Low detectable integration spray tube suitable for self-adaptation engine

Also Published As

Publication number Publication date
GB2615794A (en) 2023-08-23

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