SG11202001253VA - Airborne aerodynamic arrangement - Google Patents

Airborne aerodynamic arrangement

Info

Publication number
SG11202001253VA
SG11202001253VA SG11202001253VA SG11202001253VA SG11202001253VA SG 11202001253V A SG11202001253V A SG 11202001253VA SG 11202001253V A SG11202001253V A SG 11202001253VA SG 11202001253V A SG11202001253V A SG 11202001253VA SG 11202001253V A SG11202001253V A SG 11202001253VA
Authority
SG
Singapore
Prior art keywords
aerodynamic arrangement
airborne
airborne aerodynamic
arrangement
aerodynamic
Prior art date
Application number
SG11202001253VA
Inventor
Alexander Nagel
Alexander Barladian
Original Assignee
Israel Aerospace Ind Ltd
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 Israel Aerospace Ind Ltd filed Critical Israel Aerospace Ind Ltd
Publication of SG11202001253VA publication Critical patent/SG11202001253VA/en

Links

Classifications

    • 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
    • B64D33/08—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of power plant cooling systems
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/005—Influencing air flow over aircraft surfaces, not otherwise provided for by other means not covered by groups B64C23/02 - B64C23/08, e.g. by electric charges, magnetic panels, piezoelectric elements, static charges or ultrasounds
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64B—LIGHTER-THAN AIR AIRCRAFT
    • B64B1/00—Lighter-than-air aircraft
    • B64B1/06—Rigid airships; Semi-rigid airships
    • B64B1/24—Arrangement of propulsion plant
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
    • B64C21/02—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like
    • B64C21/025—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like for simultaneous blowing and sucking
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C7/00—Structures or fairings not otherwise provided for
    • B64C7/02—Nacelles
    • 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
    • B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
    • B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
    • B64D2013/0603—Environmental Control Systems
    • B64D2013/0614—Environmental Control Systems with subsystems for cooling avionics

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
SG11202001253VA 2017-10-03 2018-09-03 Airborne aerodynamic arrangement SG11202001253VA (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
IL254871A IL254871B (en) 2017-10-03 2017-10-03 Airborne aerodynamic arrangement
PCT/IL2018/050974 WO2019069302A1 (en) 2017-10-03 2018-09-03 Airborne aerodynamic arrangement

Publications (1)

Publication Number Publication Date
SG11202001253VA true SG11202001253VA (en) 2020-03-30

Family

ID=61198624

Family Applications (1)

Application Number Title Priority Date Filing Date
SG11202001253VA SG11202001253VA (en) 2017-10-03 2018-09-03 Airborne aerodynamic arrangement

Country Status (4)

Country Link
US (1) US11884415B2 (en)
IL (1) IL254871B (en)
SG (1) SG11202001253VA (en)
WO (1) WO2019069302A1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP7330848B2 (en) * 2019-10-16 2023-08-22 三菱重工業株式会社 Airflow control system and aircraft
CN113998126B (en) * 2021-12-03 2023-10-20 江西洪都航空工业集团有限责任公司 Piston engine air cooling device for folding unmanned aerial vehicle

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1874278A (en) * 1929-08-28 1932-08-30 Edmund P Gaines Aerofoil
US3247676A (en) 1965-01-14 1966-04-26 Rosemount Eng Co Ltd Aerodynamic cooling
US4174083A (en) * 1977-04-29 1979-11-13 The Boeing Company Flow deflector for fluid inlet
US4674704A (en) 1985-12-03 1987-06-23 The United States Of America As Represented By The Secretary Of The Air Force Direct air cooling system for airborne electronics
US5203163A (en) * 1990-08-01 1993-04-20 General Electric Company Heat exchange arrangement in a gas turbine engine fan duct for cooling hot bleed air
US6575402B1 (en) 2002-04-17 2003-06-10 Sikorsky Aircraft Corporation Cooling system for a hybrid aircraft
GB2437295B (en) * 2006-04-20 2008-06-25 Rolls Royce Plc Aeroengine ventilation system
EP2074318B1 (en) * 2006-10-12 2016-03-09 United Technologies Corporation Turbofan engine and method of changing an effective nozzle exit area of the same
DE602006019008D1 (en) * 2006-10-12 2011-01-27 United Technologies Corp MODULATION FLOW THROUGH TURBO MOTOR COOLING SYSTEM
BRPI0700765A (en) 2007-02-15 2007-12-04 Embraer Aeronautica Sa vortex generator to improve performance of recessed air intakes
US20120124964A1 (en) * 2007-07-27 2012-05-24 Hasel Karl L Gas turbine engine with improved fuel efficiency
US20090277993A1 (en) 2008-05-07 2009-11-12 Honeywell International Inc. Systems and methods for a passive, forced convection cooling system
US8979499B2 (en) * 2012-08-17 2015-03-17 United Technologies Corporation Gas turbine engine airfoil profile
DE102012217469A1 (en) 2012-09-26 2014-03-27 Siemens Aktiengesellschaft Cooling system for components in (air) vehicle structures
US9810147B2 (en) * 2013-10-31 2017-11-07 The Boeing Company Angled inlet system for a precooler

Also Published As

Publication number Publication date
IL254871B (en) 2020-09-30
US20200277074A1 (en) 2020-09-03
US11884415B2 (en) 2024-01-30
WO2019069302A1 (en) 2019-04-11
IL254871A (en) 2018-01-31

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