PL423418A1 - Jednostka napędowa pojazdu latającego - Google Patents
Jednostka napędowa pojazdu latającegoInfo
- 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
Links
- 238000010276 construction Methods 0.000 abstract 1
- 230000029305 taxis Effects 0.000 abstract 1
Classifications
-
- 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
- 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
- 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
- B64C29/0025—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 the propellers being fixed relative to the fuselage
-
- 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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/20—Vertical take-off and landing [VTOL] aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/30—Lift-producing means using radial airflow
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/80—Arrangement of on-board electronics, e.g. avionics systems or wiring
- B64U20/83—Electronic components structurally integrated with aircraft elements, e.g. circuit boards carrying loads
-
- 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
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).
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)
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)
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)
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 |
-
2017
- 2017-11-12 PL PL423418A patent/PL423418A1/pl unknown
-
2018
- 2018-11-05 EP EP18826116.8A patent/EP3707073A1/en active Pending
- 2018-11-05 CN CN201880054852.5A patent/CN111094129A/zh active Pending
- 2018-11-05 WO PCT/PL2018/000106 patent/WO2019093913A1/en active Application Filing
-
2020
- 2020-05-11 US US16/872,323 patent/US11753158B2/en active Active
Patent Citations (5)
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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