CN110816807B - 细长结构、具有细长结构的结构组装件以及支撑结构载荷的方法 - Google Patents
细长结构、具有细长结构的结构组装件以及支撑结构载荷的方法 Download PDFInfo
- Publication number
- CN110816807B CN110816807B CN201910462335.8A CN201910462335A CN110816807B CN 110816807 B CN110816807 B CN 110816807B CN 201910462335 A CN201910462335 A CN 201910462335A CN 110816807 B CN110816807 B CN 110816807B
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- China
- Prior art keywords
- elongated structure
- web
- elongated
- height
- length
- 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.)
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Links
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- 230000000712 assembly Effects 0.000 description 24
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- 238000000110 selective laser sintering Methods 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 238000004026 adhesive bonding Methods 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 238000000149 argon plasma sintering Methods 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
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- 238000011960 computer-aided design Methods 0.000 description 1
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Classifications
-
- 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
- B64C1/061—Frames
-
- 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
- B64C1/064—Stringers; Longerons
-
- 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
- B64C1/068—Fuselage sections
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Moulding By Coating Moulds (AREA)
- Rod-Shaped Construction Members (AREA)
- Supports For Pipes And Cables (AREA)
- Laminated Bodies (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US16/058,230 US11312468B2 (en) | 2018-08-08 | 2018-08-08 | Elongate structures, structural assemblies with elongate structures, and methods for supporting a structural load |
| US16/058,230 | 2018-08-08 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN110816807A CN110816807A (zh) | 2020-02-21 |
| CN110816807B true CN110816807B (zh) | 2024-03-29 |
Family
ID=66589302
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910462335.8A Active CN110816807B (zh) | 2018-08-08 | 2019-05-30 | 细长结构、具有细长结构的结构组装件以及支撑结构载荷的方法 |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US11312468B2 (enExample) |
| EP (1) | EP3608218B1 (enExample) |
| JP (1) | JP7401221B2 (enExample) |
| CN (1) | CN110816807B (enExample) |
| CA (1) | CA3042655C (enExample) |
Families Citing this family (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US11447228B2 (en) * | 2020-04-23 | 2022-09-20 | The Boeing Company | Methods of manufacture for aircraft substructure |
| CN112548569B (zh) * | 2020-12-02 | 2023-07-07 | 南京航空航天大学 | 一种飞行器蒙皮-桁条结构复合增材减材制造系统与方法 |
| CN112765695B (zh) * | 2021-01-21 | 2023-12-05 | 深圳市创想三维科技股份有限公司 | 支撑体生成方法、3d打印机、计算机装置及存储介质 |
| US11981460B2 (en) * | 2022-05-13 | 2024-05-14 | Firestorm Labs, Inc. | Mission-adaptable aerial vehicle and methods for in-field assembly and use |
| CA3160533A1 (en) * | 2022-05-26 | 2023-11-26 | Airbus Canada Limited Partnership | Stiffener integration in an isogrid structure |
| US12479644B1 (en) * | 2023-01-26 | 2025-11-25 | United States Of America, Department Of The Navy | Sealed ortho-grid laser and imaging director with an ortho/iso-grid pressure vessel |
| WO2025193944A1 (en) | 2024-03-13 | 2025-09-18 | Firestorm Labs, Inc. | Additive manufactured integral fastening system for mission adaptable unmanned aerial vehicles |
| EP4656512A1 (en) * | 2024-05-29 | 2025-12-03 | AIRBUS Operations GmbH | Aircraft fuselage and aircraft or spacecraft |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB0712552D0 (en) * | 2007-06-29 | 2007-08-08 | Airbus Uk Ltd | Elongate composite structural members and improvements therein |
| DE102008057247B3 (de) * | 2008-11-13 | 2010-01-28 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Paneel in einer Semimonocoque-Bauweise und Herstellungsverfahren dafür |
| CN101795937A (zh) * | 2007-06-29 | 2010-08-04 | 空中客车英国有限公司 | 细长复合结构件的改进 |
| CN103561940A (zh) * | 2011-05-19 | 2014-02-05 | 波音公司 | 高容量拉脱的飞机结构 |
| EP2960150A1 (en) * | 2014-06-26 | 2015-12-30 | The Boeing Company | Elongated structures and related assemblies |
Family Cites Families (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2617179A (en) * | 1950-05-10 | 1952-11-11 | Mcdonnell Aircraft Corp | Method of manufacturing tapered beams |
| US6648273B2 (en) * | 2001-10-30 | 2003-11-18 | The Boeing Company | Light weight and high strength fuselage |
| US7818945B2 (en) * | 2005-03-31 | 2010-10-26 | The Boeing Company | Composite structural member having an undulating web and method for forming same |
| FR2906008B1 (fr) * | 2006-09-15 | 2008-11-07 | Airbus France Sa | Eclisse de lisses et dispositif de jonction orbitale |
| DE102007044389A1 (de) * | 2007-09-18 | 2009-04-02 | Airbus Deutschland Gmbh | Strukturbauteil und Rumpf eines Luft- oder Raumfahrzeugs |
| DE102007054053A1 (de) * | 2007-11-13 | 2009-05-20 | Airbus Deutschland Gmbh | Kupplungselement zur Verbindung von zwei Längsversteifungselementen |
| US8993097B2 (en) | 2011-10-10 | 2015-03-31 | The Boeing Company | Tapered height curved composite stringers and corresponding panels |
| FR2984844B1 (fr) * | 2011-12-21 | 2014-02-28 | Airbus Operations Sas | Element de structure de fuselage d'aeronef anti deversement |
| US8703269B2 (en) * | 2012-02-14 | 2014-04-22 | Gulfstream Aerospace Corporation | Reinforced composite structures for aircrafts and methods for making the same |
| US9096324B2 (en) * | 2013-03-19 | 2015-08-04 | The Boeing Company | Joint assembly to form a sealed flow conduit |
| EP2781450B1 (en) * | 2013-03-19 | 2018-05-02 | Airbus Operations GmbH | System and method for interconnecting composite structures |
| ES2819076T3 (es) * | 2013-04-30 | 2021-04-14 | Airbus Operations Sl | Estructura compuesta para una aeronave y procedimiento de fabricación de la misma |
| GB2517954B (en) * | 2013-09-05 | 2018-07-04 | Airbus Operations Ltd | Repair of a damaged composite aircraft wing |
| US10086922B2 (en) | 2013-11-15 | 2018-10-02 | The Boeing Company | Low stress stiffener runout in Pi bonded structure |
| EP3083395B1 (en) * | 2013-12-20 | 2021-09-08 | Saab Ab | Stiffening element and reinforced structure |
| CL2014000880A1 (es) | 2014-04-08 | 2014-10-03 | Guillermo Moyano | Fondo de contenedor para productos hortofruticolas que optimiza el uso del material para distribuir los esfuerzos a los cuales es sometido, dicho fondo conformado por un marco de fondo unido a una base de fondo porque dicha base de fondo comprende nervios de altura variable; contenedor para productos hortofruticolas y procedimiento de fabricacion. |
-
2018
- 2018-08-08 US US16/058,230 patent/US11312468B2/en active Active
-
2019
- 2019-05-08 CA CA3042655A patent/CA3042655C/en active Active
- 2019-05-16 EP EP19174854.0A patent/EP3608218B1/en active Active
- 2019-05-30 CN CN201910462335.8A patent/CN110816807B/zh active Active
- 2019-08-08 JP JP2019145894A patent/JP7401221B2/ja active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB0712552D0 (en) * | 2007-06-29 | 2007-08-08 | Airbus Uk Ltd | Elongate composite structural members and improvements therein |
| CN101772452A (zh) * | 2007-06-29 | 2010-07-07 | 空中客车英国有限公司 | 细长复合结构件及其改进 |
| CN101795937A (zh) * | 2007-06-29 | 2010-08-04 | 空中客车英国有限公司 | 细长复合结构件的改进 |
| DE102008057247B3 (de) * | 2008-11-13 | 2010-01-28 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Paneel in einer Semimonocoque-Bauweise und Herstellungsverfahren dafür |
| CN103561940A (zh) * | 2011-05-19 | 2014-02-05 | 波音公司 | 高容量拉脱的飞机结构 |
| EP2960150A1 (en) * | 2014-06-26 | 2015-12-30 | The Boeing Company | Elongated structures and related assemblies |
Also Published As
| Publication number | Publication date |
|---|---|
| CA3042655C (en) | 2023-08-15 |
| EP3608218A1 (en) | 2020-02-12 |
| US11312468B2 (en) | 2022-04-26 |
| JP7401221B2 (ja) | 2023-12-19 |
| CA3042655A1 (en) | 2020-02-08 |
| CN110816807A (zh) | 2020-02-21 |
| JP2020050332A (ja) | 2020-04-02 |
| EP3608218B1 (en) | 2022-08-17 |
| US20200047867A1 (en) | 2020-02-13 |
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| GR01 | Patent grant | ||
| GR01 | Patent grant |