PL414124A1 - Vertical takeoff and landing aircraft - Google Patents
Vertical takeoff and landing aircraftInfo
- Publication number
- PL414124A1 PL414124A1 PL414124A PL41412415A PL414124A1 PL 414124 A1 PL414124 A1 PL 414124A1 PL 414124 A PL414124 A PL 414124A PL 41412415 A PL41412415 A PL 41412415A PL 414124 A1 PL414124 A1 PL 414124A1
- Authority
- PL
- Poland
- Prior art keywords
- aircraft
- control
- vertical
- counter
- center
- Prior art date
Links
- 230000001419 dependent effect Effects 0.000 abstract 1
- 230000005484 gravity Effects 0.000 abstract 1
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
- B64C29/02—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis vertical when grounded
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/12—Canard-type aircraft
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U70/00—Launching, take-off or landing arrangements
- B64U70/80—Vertical take-off or landing, e.g. using rockets
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Toys (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
Abstract
Przedmiotem zgłoszenia jest statek powietrzny pionowego startu i lądowania w wersji pilotowej lub bezpilotowej, napędzany przez jeden lub więcej silników elektrycznych obracających umieszczone z przodu dwa przeciwbieżne śmigła o stałym lub zmiennym skoku. Do sterowania w pionowych i poziomych stanach lotu statku powietrznego wykorzystuje się dodatkowe poziome i pionowe powierzchnie sterująco - wyważające (5 i 7), umieszczone w strumieniu zaśmigłowym przeciwbieżnych śmigieł (1) przed środkiem ciężkości statku powietrznego, zaś same powierzchnie sterująco - wyważające (5 i 7) są zawieszone względem statku powietrznego na osiach (6 i 8), które są usytuowane przed środkiem sił aerodynamicznych przez nie wytwarzanych, dzięki czemu powierzchnie aerodynamiczne ustawiają się zgodnie z kierunkiem przepływającego powietrza sterującego statku powietrznego, zaś siła nośna przez nie wytwarzana jest bezpośrednio zależna od momentów przykładanych do ich osi obrotów (6 i 8), a wytwarzanym przy pomocy liniowych lub kątowych dźwigników magneto - dynamicznych (10) lub w sposób aerodynamiczny przez dodatkowe klapki sterujące (12) zabudowane na powierzchniach sterująco - wyważających (5 i 7).The subject of the notification is an aircraft of vertical take-off and landing in a pilot or unmanned version, driven by one or more electric motors rotating placed in front two counter-rotating propellers with fixed or variable pitch. To control in vertical and horizontal flight conditions of an aircraft, additional horizontal and vertical control and balancing surfaces (5 and 7) are used, placed in the propeller stream of counter-rotating propellers (1) in front of the aircraft's center of gravity, and the control and balancing surfaces themselves (5 and 7) are suspended relative to the aircraft on axles (6 and 8), which are located in front of the center of the aerodynamic forces generated by them, thanks to which the aerodynamic surfaces position themselves in the direction of the flowing control air of the aircraft, and the lift force generated by them is directly dependent from the moments applied to their axis of rotation (6 and 8), and produced by means of linear or angular magneto-dynamic jacks (10) or aerodynamically by additional control flaps (12) mounted on control and balancing surfaces (5 and 7).
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PL414124A PL414124A1 (en) | 2015-09-23 | 2015-09-23 | Vertical takeoff and landing aircraft |
| EP16788576.3A EP3365227A1 (en) | 2015-09-23 | 2016-09-21 | Vertical take-off and landing aircraft |
| PCT/PL2016/000107 WO2017052396A1 (en) | 2015-09-23 | 2016-09-21 | Vertical take-off and landing aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PL414124A PL414124A1 (en) | 2015-09-23 | 2015-09-23 | Vertical takeoff and landing aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| PL414124A1 true PL414124A1 (en) | 2017-03-27 |
Family
ID=57211554
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PL414124A PL414124A1 (en) | 2015-09-23 | 2015-09-23 | Vertical takeoff and landing aircraft |
Country Status (3)
| Country | Link |
|---|---|
| EP (1) | EP3365227A1 (en) |
| PL (1) | PL414124A1 (en) |
| WO (1) | WO2017052396A1 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| IT202200013030A1 (en) * | 2022-06-20 | 2023-12-20 | Hpg S R L | VERTICAL TAKE-OFF AND LANDING AIRCRAFT |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2578578A (en) * | 1946-03-04 | 1951-12-11 | Myers George Francis | Convertible aircraft landing gear |
| US5289994A (en) * | 1989-10-10 | 1994-03-01 | Juan Del Campo Aguilera | Equipment carrying remote controlled aircraft |
| US5114096A (en) * | 1990-07-27 | 1992-05-19 | Wernicke Kenneth G | Tail sitter airplane |
| JP4848382B2 (en) * | 2008-02-27 | 2011-12-28 | 三菱重工業株式会社 | Unmanned aircraft and unmanned aircraft systems |
| PL389502A1 (en) * | 2009-11-09 | 2011-05-23 | Edward Margański | Aircraft |
| US8505846B1 (en) * | 2010-05-11 | 2013-08-13 | II Stanley Gordon Sanders | Vertical takeoff and landing aircraft |
-
2015
- 2015-09-23 PL PL414124A patent/PL414124A1/en unknown
-
2016
- 2016-09-21 EP EP16788576.3A patent/EP3365227A1/en not_active Withdrawn
- 2016-09-21 WO PCT/PL2016/000107 patent/WO2017052396A1/en active Application Filing
Also Published As
| Publication number | Publication date |
|---|---|
| WO2017052396A1 (en) | 2017-03-30 |
| EP3365227A1 (en) | 2018-08-29 |
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