PL423418A1 - Jednostka napędowa pojazdu latającego - Google Patents

Jednostka napędowa pojazdu latającego

Info

Publication number
PL423418A1
PL423418A1 PL423418A PL42341817A PL423418A1 PL 423418 A1 PL423418 A1 PL 423418A1 PL 423418 A PL423418 A PL 423418A PL 42341817 A PL42341817 A PL 42341817A PL 423418 A1 PL423418 A1 PL 423418A1
Authority
PL
Poland
Prior art keywords
flying
flying vehicle
driving unit
fixed
fans
Prior art date
Application number
PL423418A
Other languages
English (en)
Inventor
Grzegorz BRYZIK
Original Assignee
Bryzik Grzegorz
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 Bryzik Grzegorz filed Critical Bryzik Grzegorz
Priority to PL423418A priority Critical patent/PL423418A1/pl
Priority to CN201880054852.5A priority patent/CN111094129A/zh
Priority to PCT/PL2018/000106 priority patent/WO2019093913A1/en
Priority to EP18826116.8A priority patent/EP3707073A1/en
Publication of PL423418A1 publication Critical patent/PL423418A1/pl
Priority to US16/872,323 priority patent/US11753158B2/en

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00Propulsion; Power supply
    • B64U50/10Propulsion
    • B64U50/13Propulsion using external fans or propellers
    • B64U50/14Propulsion using external fans or propellers ducted or shrouded
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/001Shrouded propellers
    • 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
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02Aircraft characterised by the type or position of power plants
    • B64D27/24Aircraft characterised by the type or position of power plants using steam or spring force
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00Type of UAV
    • B64U10/20Vertical take-off and landing [VTOL] aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00Means for producing lift; Empennages; Arrangements thereof
    • B64U30/30Lift-producing means using radial airflow
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U20/00Constructional aspects of UAVs
    • B64U20/80Arrangement of on-board electronics, e.g. avionics systems or wiring
    • B64U20/83Electronic components structurally integrated with aircraft elements, e.g. circuit boards carrying loads
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00Means for producing lift; Empennages; Arrangements thereof
    • B64U30/10Wings
    • B64U30/12Variable or detachable wings, e.g. wings with adjustable sweep

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Remote Sensing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Toys (AREA)

Abstract

Rozwiązaniem jest jednostka napędowa pojazdu latającego umożliwiająca budowanie pojazdów latających pionowego startu i lądowania do stosowania na przykład w produkcji taksówek latających, w branży modelarskiej oraz w branży zabawkarskiej. Jednostkę napędową tworzy kanał powietrzny (1) w postaci prostego odcinka rury o przekroju kołowym, który na obu końcach ma zamocowane nieruchomo wentylatory (2 i 2') z silnikami (3 i 3'). Pomiędzy zamocowanymi wentylatorami (2 i 2') napędu umieszczony jest otwór dyszy wylotowo-wlotowej ciągu pionowego (5).
PL423418A 2017-11-12 2017-11-12 Jednostka napędowa pojazdu latającego PL423418A1 (pl)

Priority Applications (5)

Application Number Priority Date Filing Date Title
PL423418A PL423418A1 (pl) 2017-11-12 2017-11-12 Jednostka napędowa pojazdu latającego
CN201880054852.5A CN111094129A (zh) 2017-11-12 2018-11-05 飞行器驱动单元
PCT/PL2018/000106 WO2019093913A1 (en) 2017-11-12 2018-11-05 Flying vehicle's drive unit
EP18826116.8A EP3707073A1 (en) 2017-11-12 2018-11-05 Flying vehicle's drive unit
US16/872,323 US11753158B2 (en) 2017-11-12 2020-05-11 Air vehicle's drive unit

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PL423418A PL423418A1 (pl) 2017-11-12 2017-11-12 Jednostka napędowa pojazdu latającego

Publications (1)

Publication Number Publication Date
PL423418A1 true PL423418A1 (pl) 2019-05-20

Family

ID=64870537

Family Applications (1)

Application Number Title Priority Date Filing Date
PL423418A PL423418A1 (pl) 2017-11-12 2017-11-12 Jednostka napędowa pojazdu latającego

Country Status (5)

Country Link
US (1) US11753158B2 (pl)
EP (1) EP3707073A1 (pl)
CN (1) CN111094129A (pl)
PL (1) PL423418A1 (pl)
WO (1) WO2019093913A1 (pl)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20210237709A1 (en) * 2018-05-09 2021-08-05 Autonomous Control Systems Laboratory Ltd. Moving Object and Method for Using Same

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2569233A1 (fr) * 1977-12-03 1986-02-21 Rolls Royce Turboreacteur pour aeronef a decollage vertical
GB2313580A (en) * 1996-05-31 1997-12-03 Astovl Limited Power plant for producing variable direction efflux
FR2894630A1 (fr) * 1989-02-17 2007-06-15 Rolls Royce Plc Plc Tuyere d'ejection pour turboreacteur d'aeronef.
US20120275905A1 (en) * 2011-04-26 2012-11-01 Lockheed Martin Corporation Lift fan spherical thrust vectoring nozzle
US20160207624A1 (en) * 2015-01-19 2016-07-21 Hi-Lite Aircraft Vertical take-off and landing (vtol) fixed wing aircraft

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1457024A (en) * 1920-06-29 1923-05-29 Henry M Franzen Control for aircraft and the like
US1728404A (en) * 1928-04-30 1929-09-17 Thomas M Finley Flying machine
FR1280103A (fr) * 1960-11-18 1961-12-29 Snecma Moteur à réaction composite pour aérodynes à grand écart de vitesse
US3316717A (en) * 1965-09-15 1967-05-02 Gen Motors Corp Dual fan engine
US5666803A (en) * 1995-08-14 1997-09-16 Windisch; D. Anthony Vectored thrust compressor for remote controlled aircraft
DE29916203U1 (de) * 1999-09-15 2000-10-26 Striebel Christhard Senkrechtstart- und landefähiges Fluggerät
GB2365392B (en) * 2000-03-22 2002-07-10 David Bernard Cassidy Aircraft
US6568630B2 (en) * 2001-08-21 2003-05-27 Urban Aeronautics Ltd. Ducted vehicles particularly useful as VTOL aircraft
CA2490886A1 (en) * 2002-06-28 2004-01-08 Ashley Christopher Bryant Ducted air power plant
ITTO20020667A1 (it) * 2002-07-26 2004-01-26 Fiat Ricerche Microvelivolo vtol
US7932580B2 (en) * 2006-12-21 2011-04-26 Sanyo Electric Co., Ltd. Semiconductor device and method of manufacturing the same
CN101850845A (zh) * 2009-04-02 2010-10-06 余志刚 垂直起降飞机的垂直起降升力系统
US20110001014A1 (en) * 2009-07-06 2011-01-06 William Dwight Gramling Twin vortex vtol aircraft
PL221132B1 (pl) * 2012-03-19 2016-02-29 Radosław Pełka Napęd pojazdu latającego pionowego startu i lądowania
GB2528489A (en) * 2014-07-23 2016-01-27 Cassidian Ltd Improvements in and relating to unmanned aerial vehicles
US10579074B2 (en) * 2016-09-30 2020-03-03 Youngsub Ahn Propeller-enclosed airlifting air tube apparatus
US11519434B2 (en) * 2017-08-10 2022-12-06 Paul NEISER Apparatus and method for fluid manipulation
US11613371B1 (en) * 2021-11-19 2023-03-28 John Daniel Romo Electric vacuum jet engine

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2569233A1 (fr) * 1977-12-03 1986-02-21 Rolls Royce Turboreacteur pour aeronef a decollage vertical
FR2894630A1 (fr) * 1989-02-17 2007-06-15 Rolls Royce Plc Plc Tuyere d'ejection pour turboreacteur d'aeronef.
GB2313580A (en) * 1996-05-31 1997-12-03 Astovl Limited Power plant for producing variable direction efflux
US20120275905A1 (en) * 2011-04-26 2012-11-01 Lockheed Martin Corporation Lift fan spherical thrust vectoring nozzle
US20160207624A1 (en) * 2015-01-19 2016-07-21 Hi-Lite Aircraft Vertical take-off and landing (vtol) fixed wing aircraft

Also Published As

Publication number Publication date
EP3707073A1 (en) 2020-09-16
WO2019093913A1 (en) 2019-05-16
CN111094129A (zh) 2020-05-01
US20200277050A1 (en) 2020-09-03
US11753158B2 (en) 2023-09-12

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