CN113320677A - 框架组装体以及框架组装体的制造方法 - Google Patents

框架组装体以及框架组装体的制造方法 Download PDF

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Publication number
CN113320677A
CN113320677A CN202110219585.6A CN202110219585A CN113320677A CN 113320677 A CN113320677 A CN 113320677A CN 202110219585 A CN202110219585 A CN 202110219585A CN 113320677 A CN113320677 A CN 113320677A
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CN
China
Prior art keywords
frame
members
frame assembly
frame member
fixing
Prior art date
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Pending
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CN202110219585.6A
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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
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Aeronext Inc
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Publication date
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First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=75801820&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=CN113320677(A) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Aeronext Inc filed Critical Aeronext Inc
Publication of CN113320677A publication Critical patent/CN113320677A/zh
Pending legal-status Critical Current

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    • 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
    • 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
    • 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
    • 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
    • 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
    • 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

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Remote Sensing (AREA)
  • Transportation (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Materials Engineering (AREA)
  • Connection Of Plates (AREA)
  • Body Structure For Vehicles (AREA)
  • Tents Or Canopies (AREA)
  • Toys (AREA)
CN202110219585.6A 2020-02-29 2021-02-26 框架组装体以及框架组装体的制造方法 Pending CN113320677A (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
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
JPPCT/JP2020/008560 2020-02-29

Publications (1)

Publication Number Publication Date
CN113320677A true CN113320677A (zh) 2021-08-31

Family

ID=75801820

Family Applications (2)

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
CN202120426834.4U Active CN222408555U (zh) 2020-02-29 2021-02-26 框架组装体

Family Applications After (1)

Application Number Title Priority Date Filing Date
CN202120426834.4U Active CN222408555U (zh) 2020-02-29 2021-02-26 框架组装体

Country Status (5)

Country Link
US (1) US12195180B2 (cg-RX-API-DMAC7.html)
EP (1) EP4112456A4 (cg-RX-API-DMAC7.html)
JP (3) JP6868317B1 (cg-RX-API-DMAC7.html)
CN (2) CN113320677A (cg-RX-API-DMAC7.html)
WO (1) WO2021171633A1 (cg-RX-API-DMAC7.html)

Cited By (1)

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CN115230935A (zh) * 2021-04-23 2022-10-25 盐城辉空科技有限公司 框架组装体以及框架组装体的制造方法

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* 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
EP4228966A4 (en) * 2021-12-31 2023-11-01 Istanbul Gelisim Üniversitesi Coaxial aluminum sigma drone chassis
AU2023225209A1 (en) * 2022-02-24 2024-09-05 Chairman, Defence Research And Development Organization A variable orthogrid stiffened shell

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FR2912804A1 (fr) * 2007-02-21 2008-08-22 Segeclair Sa Dispositif de montage d'equipements non dimensionnants sur une ossature structurelle d'un vehicule, vehicule equipe d'un tel dispositif et procede de montage.
JP2008214963A (ja) * 2007-03-05 2008-09-18 Shin Nikkei Co Ltd フレーム
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CN105059526A (zh) * 2015-07-29 2015-11-18 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
US20170291677A1 (en) * 2016-04-06 2017-10-12 Benjamin Harris Folding heavy-lift unmanned aerial vehicle frame
CN110691733A (zh) * 2017-06-04 2020-01-14 株式会社爱隆未来 飞行体
CN110697021A (zh) * 2019-10-24 2020-01-17 中国人民解放军军事科学院国防工程研究院 一种轻量化折叠无人机
CN210618446U (zh) * 2019-09-10 2020-05-26 苏州创飞智能科技有限公司 一种轻量化无人机

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DE102004063205B3 (de) 2004-12-23 2006-05-04 Julian Kuntz Fluggerät mit verbesserter Beweglichkeit am Boden
EP2121439B1 (en) * 2007-02-16 2012-11-14 Donald Orval Shaw Modular flying vehicle
US8079549B2 (en) * 2008-06-30 2011-12-20 EMBRAER—Empresa Brasileira de Aeronautica S.A. Monolithic integrated structural panels especially useful for aircraft structures
EP2530010B1 (en) * 2011-06-02 2013-09-18 Bell Helicopter Textron Inc. Integrally stiffened panel
WO2015094059A1 (en) * 2013-12-20 2015-06-25 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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US9657489B2 (en) * 2015-06-15 2017-05-23 The Boeing Company Fractal stiffening
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WO2017183551A1 (ja) * 2016-04-19 2017-10-26 株式会社プロドローン 無人航空機
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JP6606648B1 (ja) * 2018-07-17 2019-11-20 株式会社プロドローン 無人航空機
JP2019191585A (ja) 2019-04-26 2019-10-31 エスゼット ディージェイアイ オスモ テクノロジー カンパニー リミテッドＳＺ ＤＪＩ Ｏｓｍｏ Ｔｅｃｈｎｏｌｏｇｙ Ｃｏ．， Ｌｔｄ． 安定化と振動低減のための装置および方法

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2912804A1 (fr) * 2007-02-21 2008-08-22 Segeclair Sa Dispositif de montage d'equipements non dimensionnants sur une ossature structurelle d'un vehicule, vehicule equipe d'un tel dispositif et procede de montage.
JP2008214963A (ja) * 2007-03-05 2008-09-18 Shin Nikkei Co Ltd フレーム
CN102196963A (zh) * 2008-09-23 2011-09-21 空中客车运营公司 组合固定隔离垫和设备用的机身结构、具有这种结构的航空器
CN105059526A (zh) * 2015-07-29 2015-11-18 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
US20170291677A1 (en) * 2016-04-06 2017-10-12 Benjamin Harris Folding heavy-lift unmanned aerial vehicle frame
CN110691733A (zh) * 2017-06-04 2020-01-14 株式会社爱隆未来 飞行体
CN210618446U (zh) * 2019-09-10 2020-05-26 苏州创飞智能科技有限公司 一种轻量化无人机
CN110697021A (zh) * 2019-10-24 2020-01-17 中国人民解放军军事科学院国防工程研究院 一种轻量化折叠无人机

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115230935A (zh) * 2021-04-23 2022-10-25 盐城辉空科技有限公司 框架组装体以及框架组装体的制造方法
US12473071B2 (en) 2021-04-23 2025-11-18 Aeronext Inc. Frame assembly and method for manufacturing frame assembly

Also Published As

Publication number Publication date
CN222408555U (zh) 2025-01-28
JP6905779B1 (ja) 2021-07-21
EP4112456A1 (en) 2023-01-04
US20230083990A1 (en) 2023-03-16
JP7610261B2 (ja) 2025-01-08
JPWO2021171633A1 (cg-RX-API-DMAC7.html) 2021-09-02
EP4112456A4 (en) 2023-10-18
WO2021171633A1 (ja) 2021-09-02
JP2021138364A (ja) 2021-09-16
US12195180B2 (en) 2025-01-14
JP2021155042A (ja) 2021-10-07
JP6868317B1 (ja) 2021-05-12

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PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
TA01 Transfer of patent application right
TA01 Transfer of patent application right

Effective date of registration: 20220228

Address after: Room 2006, second floor, Ruihang mutual appreciation innovation center, Dongtai high tech Development Zone, Yancheng City, Jiangsu Province

Applicant after: Yancheng huikong Technology Co.,Ltd.

Applicant after: AERONEXT Inc.

Address before: No. 3-5, erdingmu, Shibuya District, Tokyo, Japan

Applicant before: AERONEXT Inc.

WD01 Invention patent application deemed withdrawn after publication
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20210831