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MX2018002328A - Una unidad de produccion de empuje con al menos dos ensambles de rotor y una carcasa. - Google Patents

Una unidad de produccion de empuje con al menos dos ensambles de rotor y una carcasa.

Info

Publication number
MX2018002328A
MX2018002328A MX2018002328A MX2018002328A MX2018002328A MX 2018002328 A MX2018002328 A MX 2018002328A MX 2018002328 A MX2018002328 A MX 2018002328A MX 2018002328 A MX2018002328 A MX 2018002328A MX 2018002328 A MX2018002328 A MX 2018002328A
Authority
MX
Mexico
Prior art keywords
rotor assemblies
housing
production unit
push production
shrouding
Prior art date
Application number
MX2018002328A
Other languages
English (en)
Other versions
MX386532B (es
Inventor
Kiesewetter Uwe
Mores Sebastian
Bebesel Marius
Pfaller Rupert
Original Assignee
Airbus Helicopters Deutschland GmbH
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 Airbus Helicopters Deutschland GmbH filed Critical Airbus Helicopters Deutschland GmbH
Publication of MX2018002328A publication Critical patent/MX2018002328A/es
Publication of MX386532B publication Critical patent/MX386532B/es

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/001—Shrouded propellers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/46—Arrangements of, or constructional features peculiar to, multiple propellers
    • B64C11/48—Units of two or more coaxial propellers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U20/00—Constructional aspects of UAVs
    • B64U20/70—Constructional aspects of the UAV body
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00—Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20—Rotors; Rotor supports
    • B64U30/26—Ducted or shrouded rotors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/13—Propulsion using external fans or propellers
    • B64U50/14—Propulsion using external fans or propellers ducted or shrouded
    • 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
    • B64D2241/00—NACA type air intakes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U20/00—Constructional aspects of UAVs
    • B64U20/20—Constructional aspects of UAVs for noise reduction
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00—UAVs specially adapted for particular uses or applications
    • B64U2101/60—UAVs specially adapted for particular uses or applications for transporting passengers; for transporting goods other than weapons
    • B64U2101/61—UAVs specially adapted for particular uses or applications for transporting passengers; for transporting goods other than weapons for transporting passengers

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Motor Or Generator Cooling System (AREA)
  • Coiling Of Filamentary Materials In General (AREA)
  • Automatic Assembly (AREA)
  • Storage Of Web-Like Or Filamentary Materials (AREA)
  • Toys (AREA)
  • Wind Motors (AREA)
  • Moulding By Coating Moulds (AREA)
  • Switches With Compound Operations (AREA)

Abstract

La invención se refiere a una unidad de producción de empuje 3d para producir empuje en una dirección predeterminada, que comprende al menos dos ensambles de rotor 7d, 8d y una carcasa 6d que acomoda como mucho uno de dichos al menos dos ensambles de rotor 7d, 8d, en donde la carcasa 6d define un ducto de aire cilíndrico 20 que está delimitado axialmente por una región de entrada de aire 20e y una región de salida de aire 20f, y en donde la región de entrada de aire 20e exhibe en dirección circunferencial del ducto de aire cilíndrico 20 una geometría ondulada.
MX2018002328A 2017-02-27 2018-02-23 Una unidad de producción de empuje con al menos dos ensambles de rotor y una carcasa. MX386532B (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP17400008.3A EP3366586B1 (en) 2017-02-27 2017-02-27 A thrust producing unit with at least two rotor assemblies and a shrouding

Publications (2)

Publication Number Publication Date
MX2018002328A true MX2018002328A (es) 2018-11-09
MX386532B MX386532B (es) 2025-03-18

Family

ID=58410234

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2018002328A MX386532B (es) 2017-02-27 2018-02-23 Una unidad de producción de empuje con al menos dos ensambles de rotor y una carcasa.

Country Status (8)

Country Link
US (1) US11220325B2 (es)
EP (1) EP3366586B1 (es)
JP (1) JP6516888B2 (es)
KR (1) KR102049969B1 (es)
CN (1) CN108502151B (es)
BR (1) BR102018003220B1 (es)
MX (1) MX386532B (es)
SG (1) SG10201800731PA (es)

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Also Published As

Publication number Publication date
EP3366586B1 (en) 2020-08-19
JP6516888B2 (ja) 2019-05-22
KR20180099522A (ko) 2018-09-05
US20180244367A1 (en) 2018-08-30
KR102049969B1 (ko) 2019-11-28
BR102018003220A2 (pt) 2018-10-30
BR102018003220B1 (pt) 2022-05-17
EP3366586A1 (en) 2018-08-29
CN108502151A (zh) 2018-09-07
US11220325B2 (en) 2022-01-11
JP2018140772A (ja) 2018-09-13
MX386532B (es) 2025-03-18
CN108502151B (zh) 2021-06-08
SG10201800731PA (en) 2018-09-27

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