CN222408555U - 框架组装体 - Google Patents

框架组装体 Download PDF

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Publication number
CN222408555U
CN222408555U CN202120426834.4U CN202120426834U CN222408555U CN 222408555 U CN222408555 U CN 222408555U CN 202120426834 U CN202120426834 U CN 202120426834U CN 222408555 U CN222408555 U CN 222408555U
Authority
CN
China
Prior art keywords
frame
members
frame assembly
frame member
fixing
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.)
Active
Application number
CN202120426834.4U
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English (en)
Chinese (zh)
Inventor
铃木阳一
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.)
Yancheng Huikong Technology Co ltd
Aeronext Inc
Original Assignee
Yancheng Huikong Technology Co ltd
Aeronext 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 Yancheng Huikong Technology Co ltd, Aeronext Inc filed Critical Yancheng Huikong Technology Co ltd
Application granted granted Critical
Publication of CN222408555U publication Critical patent/CN222408555U/zh
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U20/00—Constructional aspects of UAVs
    • B64U20/70—Constructional aspects of the UAV body
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/08—Geodetic or other open-frame structures
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/02—Aircraft not otherwise provided for characterised by special use
    • B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U20/00—Constructional aspects of UAVs
    • B64U20/60—UAVs characterised by the material
    • B64U20/65—Composite materials
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
    • F16B5/04—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of riveting
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/10—Rotorcrafts
    • B64U10/13—Flying platforms
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Remote Sensing (AREA)
  • Transportation (AREA)
  • General Engineering & Computer Science (AREA)
  • Composite Materials (AREA)
  • Materials Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Connection Of Plates (AREA)
  • Body Structure For Vehicles (AREA)
  • Toys (AREA)
  • Tents Or Canopies (AREA)
CN202120426834.4U 2020-02-29 2021-02-26 框架组装体 Active CN222408555U (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JPPCT/JP2020/008560 2020-02-29
PCT/JP2020/008560 WO2021171633A1 (ja) 2020-02-29 2020-02-29 フレーム組立体及びフレーム組立体の製造方法

Publications (1)

Publication Number Publication Date
CN222408555U true CN222408555U (zh) 2025-01-28

Family

ID=75801820

Family Applications (2)

Application Number Title Priority Date Filing Date
CN202120426834.4U Active CN222408555U (zh) 2020-02-29 2021-02-26 框架组装体
CN202110219585.6A Pending CN113320677A (zh) 2020-02-29 2021-02-26 框架组装体以及框架组装体的制造方法

Family Applications After (1)

Application Number Title Priority Date Filing Date
CN202110219585.6A Pending CN113320677A (zh) 2020-02-29 2021-02-26 框架组装体以及框架组装体的制造方法

Country Status (5)

Country Link
US (1) US12195180B2 (enExample)
EP (1) EP4112456A4 (enExample)
JP (3) JP6868317B1 (enExample)
CN (2) CN222408555U (enExample)
WO (1) WO2021171633A1 (enExample)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
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US11613340B2 (en) * 2020-05-21 2023-03-28 North West Heli-Structures Incorporated Panel systems and methods for helicopters
JPWO2022224630A1 (enExample) 2021-04-23 2022-10-27
EP4228966A4 (en) * 2021-12-31 2023-11-01 Istanbul Gelisim Üniversitesi Coaxial aluminum sigma drone chassis

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* Cited by examiner, † Cited by third party
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US4761930A (en) * 1981-12-14 1988-08-09 Fibergrate Corporation Grating system
DE102004063205B3 (de) 2004-12-23 2006-05-04 Julian Kuntz Fluggerät mit verbesserter Beweglichkeit am Boden
US8453962B2 (en) * 2007-02-16 2013-06-04 Donald Orval Shaw Modular flying vehicle
FR2912804B1 (fr) * 2007-02-21 2010-10-01 Sogeclair Dispositif de montage d'equipements non dimensionnants sur une ossature structurelle d'un vehicule, vehicule equipe d'un tel dispositif et procede de montage.
JP4793998B2 (ja) * 2007-03-05 2011-10-12 株式会社Ｌｉｘｉｌ フレーム
US8079549B2 (en) * 2008-06-30 2011-12-20 EMBRAER—Empresa Brasileira de Aeronautica S.A. Monolithic integrated structural panels especially useful for aircraft structures
FR2936219B1 (fr) * 2008-09-23 2010-09-17 Airbus France Structure de fuselage pour fixation combinee de matelas d'isolation et d'equipements, aeronef incorporant une telle structure.
EP2530010B1 (en) * 2011-06-02 2013-09-18 Bell Helicopter Textron Inc. Integrally stiffened panel
EP3083395B1 (en) * 2013-12-20 2021-09-08 Saab Ab Stiffening element and reinforced structure
EP2889212B1 (en) * 2013-12-30 2016-01-06 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Subfloor structure with an integral hull for a rotary wing aircraft
EP2942269B1 (en) * 2014-05-06 2018-09-26 Airbus Operations GmbH Method for manufacturing a load bearing structure and such a load bearing structure
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JP6383878B2 (ja) * 2014-11-11 2018-08-29 アマゾン テクノロジーズ インコーポレイテッド 長期飛行のための無人航空機構成
CN112722239B (zh) * 2015-06-01 2023-02-28 深圳市大疆创新科技有限公司 无人飞行器
US9657489B2 (en) * 2015-06-15 2017-05-23 The Boeing Company Fractal stiffening
KR101692315B1 (ko) 2015-06-17 2017-01-03 이상현 멀티 로터 비행체
CN105059526B (zh) 2015-07-29 2018-02-09 北京中科遥数信息技术有限公司 一种滑竿式的轻型四旋翼无人机
CN105775151A (zh) 2016-01-29 2016-07-20 上海云舞网络科技有限公司 360°全景航拍摄影摄像无人机及机架框
US10266245B2 (en) * 2016-04-06 2019-04-23 Harris Aerial Llc Folding heavy-lift unmanned aerial vehicle frame
WO2017183551A1 (ja) * 2016-04-19 2017-10-26 株式会社プロドローン 無人航空機
US11142311B2 (en) * 2016-07-01 2021-10-12 Textron Innovations Inc. VTOL aircraft for external load operations
US10183746B2 (en) * 2016-07-01 2019-01-22 Bell Helicopter Textron Inc. Aircraft with independently controllable propulsion assemblies
CN106043679B (zh) 2016-07-28 2018-09-07 易瓦特科技股份公司 多轴动力源无人飞行设备
EP3281861B1 (en) * 2016-08-11 2019-10-02 AIRBUS HELICOPTERS DEUTSCHLAND GmbH A rotary wing aircraft with a fuselage that comprises at least one structural stiffened panel
US10183747B1 (en) * 2016-08-26 2019-01-22 Kitty Hawk Corporation Multicopter with boom-mounted rotors
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WO2018225112A1 (ja) * 2017-06-04 2018-12-13 株式会社エアロネクスト 飛行体
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KR101883346B1 (ko) 2017-11-03 2018-07-30 이상현 비행체
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Also Published As

Publication number Publication date
EP4112456A1 (en) 2023-01-04
JPWO2021171633A1 (enExample) 2021-09-02
JP7610261B2 (ja) 2025-01-08
JP6905779B1 (ja) 2021-07-21
US12195180B2 (en) 2025-01-14
EP4112456A4 (en) 2023-10-18
JP2021155042A (ja) 2021-10-07
WO2021171633A1 (ja) 2021-09-02
US20230083990A1 (en) 2023-03-16
JP2021138364A (ja) 2021-09-16
CN113320677A (zh) 2021-08-31
JP6868317B1 (ja) 2021-05-12

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