WO2020003657A1 - Aéronef - Google Patents

Aéronef Download PDF

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Publication number
WO2020003657A1
WO2020003657A1 PCT/JP2019/012330 JP2019012330W WO2020003657A1 WO 2020003657 A1 WO2020003657 A1 WO 2020003657A1 JP 2019012330 W JP2019012330 W JP 2019012330W WO 2020003657 A1 WO2020003657 A1 WO 2020003657A1
Authority
WO
WIPO (PCT)
Prior art keywords
rotor
aircraft
center
wing
swept
Prior art date
Application number
PCT/JP2019/012330
Other languages
English (en)
Japanese (ja)
Inventor
雄介 大西
空野 宮内
哲弥 宮腰
悟 服部
認 柴田
Original Assignee
新明和工業株式会社
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 新明和工業株式会社 filed Critical 新明和工業株式会社
Publication of WO2020003657A1 publication Critical patent/WO2020003657A1/fr

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/25—Fixed-wing aircraft
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/10—Shape of wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00—Means for producing lift; Empennages; Arrangements thereof
    • B64U30/10—Wings
    • B64U30/12—Variable or detachable wings, e.g. wings with adjustable sweep
    • B64U30/16—Variable or detachable wings, e.g. wings with adjustable sweep movable along 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
    • B64U30/29—Constructional aspects of rotors or rotor supports; Arrangements thereof
    • B64U30/294—Rotors arranged in 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
    • B64U30/29—Constructional aspects of rotors or rotor supports; Arrangements thereof
    • B64U30/295—Rotors arranged in the wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U40/00—On-board mechanical arrangements for adjusting control surfaces or rotors; On-board mechanical arrangements for in-flight adjustment of the base configuration
    • B64U40/20—On-board mechanical arrangements for adjusting control surfaces or rotors; On-board mechanical arrangements for in-flight adjustment of the base configuration for in-flight adjustment of the base configuration
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
    • B64C27/26—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft characterised by provision of fixed wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/19—Propulsion using electrically powered motors

Abstract

La présente invention a pour objet de mettre en œuvre un aéronef qui comprend une paire de rotors côté gauche et côté droit, un rotor disposé sur la ligne centrale de la cellule, et une aile fixe et qui présente une excellente stabilité de cellule au cours du décollage et de l'atterrissage à la verticale. Cet aéronef (1) comprend : un fuselage (10) ; une aile fixe (20) qui est une aile en flèche positive ; une hélice (40) qui génère une poussée vers l'avant ; un rotor côté gauche (31) qui est disposé sur le côté gauche de la ligne centrale de la cellule (CL) ; un rotor côté droit (32) qui est disposé sur le côté droit de la ligne centrale de la cellule (CL) ; et un rotor central (33) qui est disposé sur la ligne centrale de la cellule (CL). Le centre de gravité (CG) de la cellule est situé à l'intérieur d'un triangle (50) qui est formé en reliant la ligne centrale de rotation (31c) du rotor côté gauche (31), la ligne centrale de rotation (32c) du rotor côté droit (32), et la ligne centrale de rotation (33c) du rotor central (33).
PCT/JP2019/012330 2018-06-27 2019-03-25 Aéronef WO2020003657A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP2018-121641 2018-06-27
JP2018121641A JP7149116B2 (ja) 2018-06-27 2018-06-27 航空機

Publications (1)

Publication Number Publication Date
WO2020003657A1 true WO2020003657A1 (fr) 2020-01-02

Family

ID=68986955

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/JP2019/012330 WO2020003657A1 (fr) 2018-06-27 2019-03-25 Aéronef

Country Status (2)

Country Link
JP (1) JP7149116B2 (fr)
WO (1) WO2020003657A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113443135A (zh) * 2020-03-25 2021-09-28 三菱重工业株式会社 翼及航空器

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20070057113A1 (en) * 2004-12-22 2007-03-15 Robert Parks System and method for utilizing stored electrical energy for VTOL aircraft thrust enhancement and attitude control
FR3020039A1 (fr) * 2014-04-16 2015-10-23 Michel Desbats Aerodyne
FR3020622A1 (fr) * 2014-04-30 2015-11-06 Heliceo Aerodyne sans pilote embarque
WO2016059040A1 (fr) * 2014-10-14 2016-04-21 Twingtec Ag Appareil volant
KR101828924B1 (ko) * 2016-08-22 2018-02-14 박춘배 내연 엔진과 전기 모터를 구비한 항공기

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20070057113A1 (en) * 2004-12-22 2007-03-15 Robert Parks System and method for utilizing stored electrical energy for VTOL aircraft thrust enhancement and attitude control
FR3020039A1 (fr) * 2014-04-16 2015-10-23 Michel Desbats Aerodyne
FR3020622A1 (fr) * 2014-04-30 2015-11-06 Heliceo Aerodyne sans pilote embarque
WO2016059040A1 (fr) * 2014-10-14 2016-04-21 Twingtec Ag Appareil volant
KR101828924B1 (ko) * 2016-08-22 2018-02-14 박춘배 내연 엔진과 전기 모터를 구비한 항공기

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113443135A (zh) * 2020-03-25 2021-09-28 三菱重工业株式会社 翼及航空器

Also Published As

Publication number Publication date
JP2020001509A (ja) 2020-01-09
JP7149116B2 (ja) 2022-10-06

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