PL3793898T3 - Połączony układ wyrzutnika sprężonego płynu i śrubowego układu napędowego - Google Patents

Połączony układ wyrzutnika sprężonego płynu i śrubowego układu napędowego

Info

Publication number
PL3793898T3
PL3793898T3 PL19804546.0T PL19804546T PL3793898T3 PL 3793898 T3 PL3793898 T3 PL 3793898T3 PL 19804546 T PL19804546 T PL 19804546T PL 3793898 T3 PL3793898 T3 PL 3793898T3
Authority
PL
Poland
Prior art keywords
propulsion system
fluid ejector
propeller propulsion
combination compressed
compressed
Prior art date
Application number
PL19804546.0T
Other languages
English (en)
Inventor
Andrei Evulet
Original Assignee
Jetoptera, Inc.
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 Jetoptera, Inc. filed Critical Jetoptera, Inc.
Publication of PL3793898T3 publication Critical patent/PL3793898T3/pl

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
    • 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
    • B64C29/0033—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 tiltable relative to the fuselage
    • 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
    • B64C29/04—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 characterised by jet-reaction propulsion
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/20—Adaptations of gas-turbine plants for driving vehicles
    • F02C6/206—Adaptations of gas-turbine plants for driving vehicles the vehicles being airscrew driven
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
    • F02K1/006—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector within one plane only
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2230/00—Boundary layer controls
    • B64C2230/06—Boundary layer controls by explicitly adjusting fluid flow, e.g. by using valves, variable aperture or slot areas, variable pump action or variable fluid pressure
    • 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
    • B64U50/12—Propulsion using turbine engines, e.g. turbojets or turbofans
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/90—Application in vehicles adapted for vertical or short take off and landing (v/stol vehicles)

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Control Of Turbines (AREA)
  • Jet Pumps And Other Pumps (AREA)
PL19804546.0T 2018-05-17 2019-05-17 Połączony układ wyrzutnika sprężonego płynu i śrubowego układu napędowego PL3793898T3 (pl)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201862673094P 2018-05-17 2018-05-17
PCT/US2019/032988 WO2019222702A1 (en) 2018-05-17 2019-05-17 Combination compressed-fluid ejector and propeller propulsion system

Publications (1)

Publication Number Publication Date
PL3793898T3 true PL3793898T3 (pl) 2026-03-23

Family

ID=68541055

Family Applications (1)

Application Number Title Priority Date Filing Date
PL19804546.0T PL3793898T3 (pl) 2018-05-17 2019-05-17 Połączony układ wyrzutnika sprężonego płynu i śrubowego układu napędowego

Country Status (11)

Country Link
US (2) US20210206484A1 (pl)
EP (2) EP4650588A3 (pl)
JP (2) JP7547213B2 (pl)
KR (2) KR20250162934A (pl)
CN (1) CN112533826A (pl)
AU (2) AU2019270239A1 (pl)
BR (1) BR112020023319A2 (pl)
CA (1) CA3100545A1 (pl)
ES (1) ES3053807T3 (pl)
PL (1) PL3793898T3 (pl)
WO (1) WO2019222702A1 (pl)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN117858832A (zh) * 2021-05-19 2024-04-09 杰托普特拉股份有限公司 自适应流体推进系统

Family Cites Families (29)

* Cited by examiner, † Cited by third party
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CH334205A (fr) * 1955-01-12 1958-11-15 Wibault Michel Henri Marie Jos Aérodyne
US2939649A (en) * 1957-04-22 1960-06-07 Ronald A Shaw Aircraft having wings with ducted fans therein
GB928475A (en) * 1961-12-27 1963-06-12 Rolls Royce Improvements in or relating to by-pass gas turbine engines
US3388878A (en) * 1965-06-01 1968-06-18 Ryan Aeronautical Co Vtol aircraft with balanced power, retractible lift fan system
DE1901707A1 (de) * 1969-01-15 1970-08-20 Hamburger Flugzeugbau Gmbh Luftfahrzeug mit ortsfest angeordneten Schub- und Hubgeblaesen
US3747874A (en) 1971-08-25 1973-07-24 Rohr Corp Ejector nozzle having primary nozzles communicating with exhaust gases in plenum chamber
GB2169968A (en) * 1985-01-22 1986-07-23 Rolls Royce Turbo-propeller aircraft gas turbine engines
US5246188A (en) * 1989-09-14 1993-09-21 Koutsoupidis Theodore K Wing turbines in conjuction with propulsion systems for aircraft and helicopters
WO1991009776A1 (en) * 1989-12-29 1991-07-11 Venturi Applications, Inc. Venturi-enhanced airfoil
US5209428A (en) * 1990-05-07 1993-05-11 Lockheed Corporation Propulsion system for a vertical and short takeoff and landing aircraft
US5275356A (en) * 1992-07-15 1994-01-04 Lockheed Corporation Propulsion system for a V/STOL aircraft
US6250066B1 (en) * 1996-11-26 2001-06-26 Honeywell International Inc. Combustor with dilution bypass system and venturi jet deflector
GB2365392B (en) * 2000-03-22 2002-07-10 David Bernard Cassidy Aircraft
JP2003206746A (ja) 2002-01-16 2003-07-25 National Aerospace Laboratory Of Japan 多ファン式コアエンジン分離型ターボファンエンジン
US6808140B2 (en) * 2002-02-08 2004-10-26 Moller Paul S Vertical take-off and landing vehicles
US7155898B2 (en) * 2004-04-13 2007-01-02 Aerojet-General Corporation Thrust vector control system for a plug nozzle rocket engine
US7150432B2 (en) * 2004-06-18 2006-12-19 The Boeing Company Horizontal augmented thrust system and method for creating augmented thrust
WO2006113877A2 (en) 2005-04-20 2006-10-26 Lugg Richard H Hybrid jet/electric vtol aircraft
ITTO20070468A1 (it) * 2007-06-29 2008-12-30 Alenia Aeronautica Spa Metodo per incrementare la portanza di superfici aerodinamiche e per ridurre la resistenza all'avanzamento
US8511058B2 (en) * 2007-11-29 2013-08-20 United Technologies Corporation Convertible gas turbine propulsion system
JP2010185363A (ja) 2009-02-12 2010-08-26 Toyota Motor Corp ターボファンエンジン
DE102009010524A1 (de) * 2009-02-25 2010-09-02 Rolls-Royce Deutschland Ltd & Co Kg Turbopropantrieb mit Druckpropeller
US8382030B2 (en) 2010-09-02 2013-02-26 Patrick A. Kosheleff Variable cycle VTOL powerplant
EP4306789A3 (en) * 2015-09-02 2024-06-12 Jetoptera, Inc. Fluidic propulsive system
US10464668B2 (en) 2015-09-02 2019-11-05 Jetoptera, Inc. Configuration for vertical take-off and landing system for aerial vehicles
US20170283080A1 (en) * 2015-09-02 2017-10-05 Jetoptera, Inc. Winglet ejector configurations
CA3006361A1 (en) 2015-12-04 2017-07-06 Jetoptera, Inc. Micro-turbine gas generator and propulsive system
CA3017263A1 (en) 2016-03-11 2017-12-07 Jetoptera, Inc. Configuration for vertical take-off and landing system for aerial vehicles
US11077951B1 (en) * 2020-03-28 2021-08-03 Textron Innovations Inc. Propulsion systems for low observable aircraft

Also Published As

Publication number Publication date
EP3793898A4 (en) 2022-01-26
KR20250162934A (ko) 2025-11-19
KR20210037615A (ko) 2021-04-06
US20210206484A1 (en) 2021-07-08
JP2021523855A (ja) 2021-09-09
EP4650588A3 (en) 2025-12-10
EP4650588A2 (en) 2025-11-19
EP3793898A1 (en) 2021-03-24
WO2019222702A1 (en) 2019-11-21
US20240217654A1 (en) 2024-07-04
EP3793898B1 (en) 2025-11-05
JP7547213B2 (ja) 2024-09-09
CN112533826A (zh) 2021-03-19
AU2025202280A1 (en) 2025-04-17
ES3053807T3 (en) 2026-01-26
AU2019270239A1 (en) 2020-12-03
JP2024178185A (ja) 2024-12-24
BR112020023319A2 (pt) 2021-02-02
KR102882577B1 (ko) 2025-11-06
CA3100545A1 (en) 2019-11-21

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