PL3635235T3 - Osłona wlotu powietrza - Google Patents

Osłona wlotu powietrza

Info

Publication number
PL3635235T3
PL3635235T3 PL18729486T PL18729486T PL3635235T3 PL 3635235 T3 PL3635235 T3 PL 3635235T3 PL 18729486 T PL18729486 T PL 18729486T PL 18729486 T PL18729486 T PL 18729486T PL 3635235 T3 PL3635235 T3 PL 3635235T3
Authority
PL
Poland
Prior art keywords
air intake
intake cover
cover
air
intake
Prior art date
Application number
PL18729486T
Other languages
English (en)
Inventor
Anthony James Howarth
Original Assignee
Mbda Uk Limited
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
Priority claimed from GB1708985.5A external-priority patent/GB2563230B/en
Priority claimed from EP17275080.4A external-priority patent/EP3412903A1/en
Application filed by Mbda Uk Limited filed Critical Mbda Uk Limited
Publication of PL3635235T3 publication Critical patent/PL3635235T3/pl

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/05—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for obviating the penetration of damaging objects or particles
    • F02C7/055—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for obviating the penetration of damaging objects or particles with intake grids, screens or guards
    • 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
    • B64D7/00—Arrangements of military equipment, e.g. armaments, armament accessories, or military shielding, in aircraft; Adaptations of armament mountings for aircraft
    • B64D7/08—Arrangements of rocket launchers or releasing means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/05—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for obviating the penetration of damaging objects or particles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/74—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant
    • F02K9/78—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant with an air-breathing jet-propulsion plant

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
PL18729486T 2017-06-06 2018-06-04 Osłona wlotu powietrza PL3635235T3 (pl)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
GB1708985.5A GB2563230B (en) 2017-06-06 2017-06-06 Air intake cover
EP17275080.4A EP3412903A1 (en) 2017-06-06 2017-06-06 Air intake cover
EP18729486.3A EP3635235B1 (en) 2017-06-06 2018-06-04 Air intake cover
PCT/GB2018/051518 WO2018224809A1 (en) 2017-06-06 2018-06-04 Air intake cover

Publications (1)

Publication Number Publication Date
PL3635235T3 true PL3635235T3 (pl) 2021-12-20

Family

ID=62530262

Family Applications (1)

Application Number Title Priority Date Filing Date
PL18729486T PL3635235T3 (pl) 2017-06-06 2018-06-04 Osłona wlotu powietrza

Country Status (5)

Country Link
US (1) US11506123B2 (pl)
EP (1) EP3635235B1 (pl)
ES (1) ES2887056T3 (pl)
PL (1) PL3635235T3 (pl)
WO (1) WO2018224809A1 (pl)

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2418743A1 (fr) * 1978-03-01 1979-09-28 Alkan R & Cie Dispositif a pinces effacables pour le transport et l'ejection de charges sans anneau emportees sous avion
US4874145A (en) * 1986-10-27 1989-10-17 Rockwell International Corporation Missile air inlet cover retractor system
US5172873A (en) * 1991-05-14 1992-12-22 Grumman Aerospace Corporation Anti-roll system for a missile launcher
US5660357A (en) * 1995-07-24 1997-08-26 Northrop Grumman Corporation Airstream ejected missile engine inlet cover
US8262344B2 (en) * 2008-04-02 2012-09-11 Hamilton Sundstrand Corporation Thermal management system for a gas turbine engine
US8777154B2 (en) * 2012-07-09 2014-07-15 United Technologies Corporation Apparatus and method for preventing gas turbine engine freezing
US10852112B2 (en) * 2014-11-07 2020-12-01 Kongsberg Defence & Aerospace As Method and system for protecting folding wings on a missile while in their stowed state
US20180179990A1 (en) * 2016-12-27 2018-06-28 Orbital Atk, Inc. Hybrid metal composite structures, rocket motors and multi-stage rocket motor assemblies including hybrid metal composite structures, and related methods

Also Published As

Publication number Publication date
EP3635235B1 (en) 2021-08-18
ES2887056T3 (es) 2021-12-21
EP3635235A1 (en) 2020-04-15
US11506123B2 (en) 2022-11-22
WO2018224809A1 (en) 2018-12-13
US20200141318A1 (en) 2020-05-07

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