WO2022228734A3 - Effiziente schubkrafterzeugung - Google Patents

Effiziente schubkrafterzeugung Download PDF

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Publication number
WO2022228734A3
WO2022228734A3 PCT/EP2022/025188 EP2022025188W WO2022228734A3 WO 2022228734 A3 WO2022228734 A3 WO 2022228734A3 EP 2022025188 W EP2022025188 W EP 2022025188W WO 2022228734 A3 WO2022228734 A3 WO 2022228734A3
Authority
WO
WIPO (PCT)
Prior art keywords
fluid
blade
bladed rotor
thrust
generation
Prior art date
Application number
PCT/EP2022/025188
Other languages
English (en)
French (fr)
Other versions
WO2022228734A2 (de
Inventor
Malte Schwarze
Original Assignee
Malte Schwarze
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
Priority claimed from EP21020484.8A external-priority patent/EP4155506A1/de
Application filed by Malte Schwarze filed Critical Malte Schwarze
Publication of WO2022228734A2 publication Critical patent/WO2022228734A2/de
Publication of WO2022228734A3 publication Critical patent/WO2022228734A3/de
Priority to DE102023110824.7A priority Critical patent/DE102023110824A1/de
Priority to DE102023110825.5A priority patent/DE102023110825A1/de
Priority to DE102023110821.2A priority patent/DE102023110821A1/de
Priority to DE102023110822.0A priority patent/DE102023110822A1/de
Priority to DE102023110823.9A priority patent/DE102023110823A1/de

Links

Classifications

    • 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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/16—Control of working fluid flow
    • F02C9/20—Control of working fluid flow by throttling; by adjusting vanes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63H—MARINE PROPULSION OR STEERING
    • B63H25/00—Steering; Slowing-down otherwise than by use of propulsive elements; Dynamic anchoring, i.e. positioning vessels by means of main or auxiliary propulsive elements
    • B63H25/06—Steering by rudders
    • B63H25/38—Rudders
    • B63H25/40—Rudders using Magnus effect
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/162—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/02—De-icing means for engines having icing phenomena
    • 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
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/64—Reversing fan flow
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K5/00—Plants including an engine, other than a gas turbine, driving a compressor or a ducted fan
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63H—MARINE PROPULSION OR STEERING
    • B63H1/00—Propulsive elements directly acting on water
    • B63H2001/005—Propulsive elements directly acting on water using Magnus effect
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/82—Rotorcraft; 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
    • B64C2027/8263—Rotorcraft; 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
    • B64C2027/8272—Rotorcraft; 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 fins, or movable rudders
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/82—Rotorcraft; 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
    • B64C2027/8263—Rotorcraft; 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
    • B64C2027/8281—Rotorcraft; 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
    • 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
    • B64D2027/005—Aircraft with an unducted turbofan comprising contra-rotating rotors, e.g. contra-rotating open rotors [CROR]
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
    • F01D25/162—Bearing supports
    • 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
    • F05D2220/30—Application in turbines
    • F05D2220/36—Application in turbines specially adapted for the fan of turbofan engines

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Ocean & Marine Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Other Liquid Machine Or Engine Such As Wave Power Use (AREA)

Abstract

Das technische Gebiet liegt auf dem Gebiet der Schuberzeugung durch Rückstoß eines Fluids. Aufgabe ist es unter anderem die Schuberzeugung effizient zu machen. Dies gelingt durch ein Triebwerksanordnung mit mindestens einem beschaufelten Rotor, auf welchen mindestens eine Antriebsleistung aufgekoppelt werden kann, mit der Folge, dass zumindest eine Druckänderung in einem Teil des Fluides hervorgerufen werden kann, mit der Folge, dass sich mindestens ein Fluidmassenstrom bewegen kann, wobei in mindestens einem der bewegten Fluidmassenströme mindestens eine Statoreinrichtung angeordnet ist, wobei diese Statoranordnung mindestens ein Blatt umfasst, welches im Einstellwinkel veränderbar ist, so, dass mindestens dieses in Bezug zur fluiddynamischen Strömung des mindestens einen beschaufelten Rotors so angeströmt werden kann, dass das Blatt eine resultierende Strömungskraft erzeugen kann, die eine Kraftkomponente in Richtung der resultierenden Saugkraft oder in Richtung der Drehachse des beschaufelten Rotors hat.
PCT/EP2022/025188 2021-04-26 2022-04-26 Effiziente schubkrafterzeugung WO2022228734A2 (de)

Priority Applications (5)

Application Number Priority Date Filing Date Title
DE102023110824.7A DE102023110824A1 (de) 2022-04-26 2023-04-26 Sensorbasierte effiziente Schuberzeugung
DE102023110825.5A DE102023110825A1 (de) 2022-04-26 2023-04-26 Selektiv bodengebundene flexible Schubkrafterzeugung
DE102023110821.2A DE102023110821A1 (de) 2022-04-26 2023-04-26 Effiziente und fortschrittliche Schuberzeugung
DE102023110822.0A DE102023110822A1 (de) 2022-04-26 2023-04-26 Luftfahrzeug mit effizienter und sicherer Schubkrafterzeugung
DE102023110823.9A DE102023110823A1 (de) 2022-04-26 2023-04-26 Luftfahrzeug mit effizienter Schuberzeugung und Triebwerksanbindung

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
DE102021110655.9 2021-04-26
DE102021110655 2021-04-26
EP21020484.8 2021-09-26
EP21020484.8A EP4155506A1 (de) 2021-09-26 2021-09-26 Effiziente schubkrafterzeugung

Publications (2)

Publication Number Publication Date
WO2022228734A2 WO2022228734A2 (de) 2022-11-03
WO2022228734A3 true WO2022228734A3 (de) 2023-03-23

Family

ID=83848873

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2022/025188 WO2022228734A2 (de) 2021-04-26 2022-04-26 Effiziente schubkrafterzeugung

Country Status (1)

Country Link
WO (1) WO2022228734A2 (de)

Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2506500A1 (de) * 1974-02-25 1975-08-28 Gen Electric Turbofantriebwerk mit variablem bypass-verhaeltnis
DE3927463A1 (de) * 1988-11-28 1990-05-31 Gen Electric Hilfskraftquelle in einem mantellosen geblaese-gasturbinen-triebwerk
US5315821A (en) * 1993-02-05 1994-05-31 General Electric Company Aircraft bypass turbofan engine thrust reverser
GB2403778A (en) * 2003-07-11 2005-01-12 Rolls Royce Plc Inlet guide vane with electrical heater
US20100014977A1 (en) * 2008-07-15 2010-01-21 Shattuck Colman D Variable pitch aft propeller vane system
US20170175628A1 (en) * 2015-12-16 2017-06-22 General Electric Company Method and system for inlet guide vane heating
US20180066536A1 (en) * 2015-03-26 2018-03-08 Safran Aircraft Engines Compressor stage
EP3620389A1 (de) * 2018-09-10 2020-03-11 General Electric Company Luftfahrzeug mit einem heckmotor
WO2020074839A1 (fr) * 2018-10-10 2020-04-16 Safran Aircraft Engines Module de soufflante a pales a calage variable
WO2021191553A1 (fr) * 2020-03-25 2021-09-30 Safran Aircraft Engines Turbomachine d'aeronef equipee d'une machine electrique
EP3960994A1 (de) * 2020-08-31 2022-03-02 General Electric Company Hybrider elektrischer luftfahrzeugmotor

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2506500A1 (de) * 1974-02-25 1975-08-28 Gen Electric Turbofantriebwerk mit variablem bypass-verhaeltnis
DE3927463A1 (de) * 1988-11-28 1990-05-31 Gen Electric Hilfskraftquelle in einem mantellosen geblaese-gasturbinen-triebwerk
US5315821A (en) * 1993-02-05 1994-05-31 General Electric Company Aircraft bypass turbofan engine thrust reverser
GB2403778A (en) * 2003-07-11 2005-01-12 Rolls Royce Plc Inlet guide vane with electrical heater
US20100014977A1 (en) * 2008-07-15 2010-01-21 Shattuck Colman D Variable pitch aft propeller vane system
US20180066536A1 (en) * 2015-03-26 2018-03-08 Safran Aircraft Engines Compressor stage
US20170175628A1 (en) * 2015-12-16 2017-06-22 General Electric Company Method and system for inlet guide vane heating
EP3620389A1 (de) * 2018-09-10 2020-03-11 General Electric Company Luftfahrzeug mit einem heckmotor
WO2020074839A1 (fr) * 2018-10-10 2020-04-16 Safran Aircraft Engines Module de soufflante a pales a calage variable
WO2021191553A1 (fr) * 2020-03-25 2021-09-30 Safran Aircraft Engines Turbomachine d'aeronef equipee d'une machine electrique
EP3960994A1 (de) * 2020-08-31 2022-03-02 General Electric Company Hybrider elektrischer luftfahrzeugmotor

Also Published As

Publication number Publication date
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