MY202190A - A vtol-capable airplane having angled propulsors - Google Patents

A vtol-capable airplane having angled propulsors

Info

Publication number
MY202190A
MY202190A MYPI2020001612A MYPI2020001612A MY202190A MY 202190 A MY202190 A MY 202190A MY PI2020001612 A MYPI2020001612 A MY PI2020001612A MY PI2020001612 A MYPI2020001612 A MY PI2020001612A MY 202190 A MY202190 A MY 202190A
Authority
MY
Malaysia
Prior art keywords
propulsors
vtol
airplane
angled
vertical
Prior art date
Application number
MYPI2020001612A
Inventor
Chung How Poh
Chung Kiak Poh
Original Assignee
Chung How Poh
Chung Kiak Poh
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 Chung How Poh, Chung Kiak Poh filed Critical Chung How Poh
Priority to MYPI2020001612A priority Critical patent/MY202190A/en
Priority to AU2020100605A priority patent/AU2020100605B4/en
Priority to GBGB2104177.7A priority patent/GB202104177D0/en
Priority to CN202110331847.8A priority patent/CN113443138A/en
Publication of MY202190A publication Critical patent/MY202190A/en

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
    • 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
    • B64C27/28—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft with forward-propulsion propellers pivotable to act as lifting rotors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/32—Rotors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Traffic Control Systems (AREA)
  • Navigation (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
  • Toys (AREA)

Abstract

The present invention relates to an airplane capable of hyper-short / vertical takeoff and landing (hyper-STOL / VTOL) and having a positive tilt angle applied to the horizontal propulsors (104A, 104B). A positive tilt angle may also be applied to the vertical propulsors (106A, 106B, 106A1, 106A2, 106B1, 106B2). This invention attempts to reduce pitch angle during hovering and vertical flight. (Most Illustrative Diagram: FIG. 3)
MYPI2020001612A 2020-03-26 2020-03-26 A vtol-capable airplane having angled propulsors MY202190A (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
MYPI2020001612A MY202190A (en) 2020-03-26 2020-03-26 A vtol-capable airplane having angled propulsors
AU2020100605A AU2020100605B4 (en) 2020-03-26 2020-04-20 A vtol-capable airplane having angled propulsors
GBGB2104177.7A GB202104177D0 (en) 2020-03-26 2021-03-25 A vtol-capable airplane having angled propulsors
CN202110331847.8A CN113443138A (en) 2020-03-26 2021-03-26 Vertical take-off and landing capability aircraft with inclined propellers

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
MYPI2020001612A MY202190A (en) 2020-03-26 2020-03-26 A vtol-capable airplane having angled propulsors

Publications (1)

Publication Number Publication Date
MY202190A true MY202190A (en) 2024-04-16

Family

ID=70776151

Family Applications (1)

Application Number Title Priority Date Filing Date
MYPI2020001612A MY202190A (en) 2020-03-26 2020-03-26 A vtol-capable airplane having angled propulsors

Country Status (4)

Country Link
CN (1) CN113443138A (en)
AU (1) AU2020100605B4 (en)
GB (1) GB202104177D0 (en)
MY (1) MY202190A (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US12084176B2 (en) 2022-10-11 2024-09-10 The Boeing Company Aircraft, a control system for the aircraft and a method of controlling the aircraft

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3563496A (en) * 1967-06-12 1971-02-16 Daniel R Zuck Compound helicopter
US7874512B2 (en) * 2006-07-12 2011-01-25 Junfeng Xu System and method for a flyable and roadable vehicle
KR20090054027A (en) * 2007-11-26 2009-05-29 임채호 Vertical takeoff and landing gear with variable rotorcraft
CA2714497C (en) * 2008-02-13 2016-06-28 Bell Helicopter Textron Inc. Rotorcraft with variable incident wing
US20140158815A1 (en) * 2012-12-10 2014-06-12 Joseph Raymond RENTERIA Zero Transition Vertical Take-Off and Landing Aircraft
KR20190039888A (en) * 2016-05-18 2019-04-16 에이캐럿큐브드 바이 에어버스 엘엘씨 Vertical takeoff and landing aircraft with tilting wing configuration
US10301016B1 (en) * 2016-08-09 2019-05-28 Vimana, Inc. Stabilized VTOL flying apparatus and aircraft
US10384776B2 (en) * 2017-02-22 2019-08-20 Bell Helicopter Textron Inc. Tiltrotor aircraft having vertical lift and hover augmentation
RU183293U1 (en) * 2017-08-28 2018-09-17 Федеральное государственное унитарное предприятие "Сибирский научно-исследовательский институт авиации им. С.А. Чаплыгина" Biplane

Also Published As

Publication number Publication date
AU2020100605B4 (en) 2020-12-24
AU2020100605A4 (en) 2020-05-28
GB202104177D0 (en) 2021-05-12
CN113443138A (en) 2021-09-28

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