FR3108890A1 - Aéronef - Google Patents

Aéronef Download PDF

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Publication number
FR3108890A1
FR3108890A1 FR2103060A FR2103060A FR3108890A1 FR 3108890 A1 FR3108890 A1 FR 3108890A1 FR 2103060 A FR2103060 A FR 2103060A FR 2103060 A FR2103060 A FR 2103060A FR 3108890 A1 FR3108890 A1 FR 3108890A1
Authority
FR
France
Prior art keywords
aircraft
cabin
abstract
published
recess
Prior art date
Legal status (The legal status 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 status listed.)
Pending
Application number
FR2103060A
Other languages
English (en)
Inventor
Martin Hoffmeister
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Dr Ing HCF Porsche AG
Original Assignee
Dr Ing HCF Porsche AG
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 Dr Ing HCF Porsche AG filed Critical Dr Ing HCF Porsche AG
Publication of FR3108890A1 publication Critical patent/FR3108890A1/fr
Pending legal-status Critical Current

Links

Classifications

    • 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
    • B64D27/40Arrangements for mounting power plants in aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/32Wings specially adapted for mounting power plant
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • 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
    • 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
    • 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
    • B64D27/40Arrangements for mounting power plants in aircraft
    • B64D27/402Arrangements for mounting power plants in aircraft comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant
    • 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
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/50On board measures aiming to increase energy efficiency
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Toys (AREA)
  • Bridges Or Land Bridges (AREA)
  • Sliding-Contact Bearings (AREA)
  • Tires In General (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Wind Motors (AREA)

Abstract

Aéronef La présente invention concerne un aéronef (10) avec les caractéristiques suivantes : l’aéronef (10) comprend une carlingue avec un portant (11) supportant un rotor sustentateur (14) et comportant un renfoncement. Figure à publier avec l’abrégé : Fig. 1
FR2103060A 2020-04-03 2021-03-26 Aéronef Pending FR3108890A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102020109331.4 2020-04-03
DE102020109331.4A DE102020109331B3 (de) 2020-04-03 2020-04-03 Luftfahrzeug

Publications (1)

Publication Number Publication Date
FR3108890A1 true FR3108890A1 (fr) 2021-10-08

Family

ID=76432483

Family Applications (1)

Application Number Title Priority Date Filing Date
FR2103060A Pending FR3108890A1 (fr) 2020-04-03 2021-03-26 Aéronef

Country Status (4)

Country Link
US (1) US20210371117A1 (fr)
CN (1) CN113492965B (fr)
DE (1) DE102020109331B3 (fr)
FR (1) FR3108890A1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102021132911A1 (de) 2021-12-14 2023-06-15 Dr. Ing. H.C. F. Porsche Aktiengesellschaft Hubeinheit für ein Luftfahrzeug und Luftfahrzeug mit einer solchen Hubeinheit

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5374011A (en) 1991-11-13 1994-12-20 Massachusetts Institute Of Technology Multivariable adaptive surface control
DE102008025298B4 (de) * 2008-05-27 2010-12-16 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verfahren und Vorrichtung zur aktiven Dämpfung von Vertikalschwingungen bei einem Hubschrauber mit angehängter Außenlast
FR2935350B1 (fr) * 2008-08-27 2011-05-20 Snecma Methode de reduction des niveaux vibratoires d'une helice de turbomoteur.
DE202013012547U1 (de) * 2012-11-15 2017-07-03 SZ DJI Technology Co., Ltd. Unbemanntes Luftfahrzeug mit mehreren Rotoren
US20160244160A1 (en) * 2013-08-09 2016-08-25 FourthWing Sensors, LLC Convertible unmanned aerial vehicle
DE102013109392A1 (de) * 2013-08-29 2015-03-05 Airbus Defence and Space GmbH Schnellfliegendes, senkrechtstartfähiges Fluggerät
WO2016003530A2 (fr) 2014-05-08 2016-01-07 Northrop Grumman Systems Corporation Véhicule aérien sans pilote (uav) de type à décollage et atterrissage verticaux (adav)
CN205186541U (zh) 2015-11-24 2016-04-27 零度智控(北京)智能科技有限公司 无人机机体支架
AT518116B1 (de) * 2015-12-30 2019-05-15 Cyclotech Gmbh Fluggerät
EP3971084A1 (fr) 2016-02-22 2022-03-23 SZ DJI Technology Co., Ltd. Foldable multi-rotor aerial vehicle
EP3445650A4 (fr) * 2016-04-19 2019-11-13 Advanced Aircraft Company Véhicule aérien sans pilote
CN106379530A (zh) * 2016-11-01 2017-02-08 赖奕璋 一种结构简单且运行平稳的垂直起降飞行器
US10577091B2 (en) * 2017-04-24 2020-03-03 Bcg Digital Ventures Gmbh Vertical take-off and landing aircraft
US11124286B1 (en) * 2017-05-25 2021-09-21 Amazon Technologies, Inc. Adjustable shrouds for propeller safety
WO2019140640A1 (fr) * 2018-01-19 2019-07-25 深圳市大疆创新科技有限公司 Ensemble bras et véhicule aérien sans pilote
EP3581490B1 (fr) * 2018-06-13 2021-01-13 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Aéronef multirotor avec une unité de production de poussée comprenant un bandage à aérodynamisme optimisé
US20220073205A1 (en) * 2018-12-28 2022-03-10 Harrison Francis Hertzberg Unmanned aerial vehicle (uav) pest abatement device
CN113682476B (zh) * 2019-01-23 2024-03-26 杭州零零科技有限公司 无人驾驶飞行系统和用于无人驾驶飞行系统的控制系统

Also Published As

Publication number Publication date
US20210371117A1 (en) 2021-12-02
DE102020109331B3 (de) 2021-07-08
CN113492965B (zh) 2024-04-02
CN113492965A (zh) 2021-10-12

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