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GB2592063B - VTOL Aircraft - Google Patents

VTOL Aircraft Download PDF

Info

Publication number
GB2592063B
GB2592063B GB2002091.3A GB202002091A GB2592063B GB 2592063 B GB2592063 B GB 2592063B GB 202002091 A GB202002091 A GB 202002091A GB 2592063 B GB2592063 B GB 2592063B
Authority
GB
United Kingdom
Prior art keywords
vtol aircraft
vtol
aircraft
Prior art date
Legal status (The legal status 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 status listed.)
Active
Application number
GB2002091.3A
Other versions
GB202002091D0 (en
GB2592063A (en
Inventor
Mohammad Mohseni Seyed
David Richard Wijker Norman
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Arc Aerosystems Ltd
Original Assignee
Samad Aerospace 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 Samad Aerospace Ltd filed Critical Samad Aerospace Ltd
Priority to GB2002091.3A priority Critical patent/GB2592063B/en
Publication of GB202002091D0 publication Critical patent/GB202002091D0/en
Publication of GB2592063A publication Critical patent/GB2592063A/en
Application granted granted Critical
Publication of GB2592063B publication Critical patent/GB2592063B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C29/00Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0016Aircraft 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C29/00Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0016Aircraft 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
    • B64C29/0025Aircraft 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 the propellers being fixed relative to the fuselage
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/46Arrangements of, or constructional features peculiar to, multiple propellers
    • B64C11/48Units of two or more coaxial propellers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/22Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
    • B64C27/26Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft characterised by provision of fixed wings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/82Rotorcraft; 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D35/00Transmitting power from power plants to propellers or rotors; Arrangements of transmissions
    • B64D35/04Transmitting power from power plants to propellers or rotors; Arrangements of transmissions characterised by the transmission driving a plurality of propellers or rotors
    • B64D35/06Transmitting power from power plants to propellers or rotors; Arrangements of transmissions characterised by the transmission driving a plurality of propellers or rotors the propellers or rotors being counter-rotating
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/82Rotorcraft; 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
    • B64C2027/8227Rotorcraft; 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 comprising more than one rotor
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/82Rotorcraft; 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
    • B64C2027/8254Shrouded tail rotors, e.g. "Fenestron" fans
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/82Rotorcraft; 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
    • B64C2027/8263Rotorcraft; 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 comprising in addition rudders, tails, fins, or the like
    • B64C2027/8281Rotorcraft; 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 comprising in addition rudders, tails, fins, or the like comprising horizontal tail planes

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
GB2002091.3A 2020-02-14 2020-02-14 VTOL Aircraft Active GB2592063B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2002091.3A GB2592063B (en) 2020-02-14 2020-02-14 VTOL Aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2002091.3A GB2592063B (en) 2020-02-14 2020-02-14 VTOL Aircraft

Publications (3)

Publication Number Publication Date
GB202002091D0 GB202002091D0 (en) 2020-04-01
GB2592063A GB2592063A (en) 2021-08-18
GB2592063B true GB2592063B (en) 2024-06-05

Family

ID=69956586

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2002091.3A Active GB2592063B (en) 2020-02-14 2020-02-14 VTOL Aircraft

Country Status (1)

Country Link
GB (1) GB2592063B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115626284A (en) * 2022-11-04 2023-01-20 孙林青 An amphibious aircraft that can automatically cope with stall and spin

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1988000556A1 (en) * 1986-07-16 1988-01-28 Kimberley Vere Sadleir A vtol aircraft and components
CN102120489A (en) * 2011-02-28 2011-07-13 南昌航空大学 Tilt ducted unmanned aerial vehicle
ES2378039A1 (en) * 2010-09-14 2012-04-04 Manuel Muñoz Saiz Success system and procedure, propulsor and stabilizer for vertical landing and tuning aircraft. (Machine-translation by Google Translate, not legally binding)
US20120280091A1 (en) * 2009-08-26 2012-11-08 Manuel Munoz Saiz Lift, propulsion and stabilising system for vertical take-off and landing aircraft
CN104401480A (en) * 2014-11-06 2015-03-11 南京航空航天大学 Ducted tilt aircraft
CN108100207A (en) * 2016-11-24 2018-06-01 中航贵州飞机有限责任公司 A kind of inflatable vertically taking off and landing flyer

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1988000556A1 (en) * 1986-07-16 1988-01-28 Kimberley Vere Sadleir A vtol aircraft and components
US20120280091A1 (en) * 2009-08-26 2012-11-08 Manuel Munoz Saiz Lift, propulsion and stabilising system for vertical take-off and landing aircraft
ES2378039A1 (en) * 2010-09-14 2012-04-04 Manuel Muñoz Saiz Success system and procedure, propulsor and stabilizer for vertical landing and tuning aircraft. (Machine-translation by Google Translate, not legally binding)
CN102120489A (en) * 2011-02-28 2011-07-13 南昌航空大学 Tilt ducted unmanned aerial vehicle
CN104401480A (en) * 2014-11-06 2015-03-11 南京航空航天大学 Ducted tilt aircraft
CN108100207A (en) * 2016-11-24 2018-06-01 中航贵州飞机有限责任公司 A kind of inflatable vertically taking off and landing flyer

Also Published As

Publication number Publication date
GB202002091D0 (en) 2020-04-01
GB2592063A (en) 2021-08-18

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