FR2953093B1 - COMPOSITE STRUCTURAL ELEMENT WITH ELECTRICAL TRANSMISSION OF INTEGRATED POWER - Google Patents
COMPOSITE STRUCTURAL ELEMENT WITH ELECTRICAL TRANSMISSION OF INTEGRATED POWERInfo
- Publication number
- FR2953093B1 FR2953093B1 FR0958371A FR0958371A FR2953093B1 FR 2953093 B1 FR2953093 B1 FR 2953093B1 FR 0958371 A FR0958371 A FR 0958371A FR 0958371 A FR0958371 A FR 0958371A FR 2953093 B1 FR2953093 B1 FR 2953093B1
- Authority
- FR
- France
- Prior art keywords
- structural element
- integrated power
- electrical transmission
- composite structural
- composite
- 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
Links
- 230000005540 biological transmission Effects 0.000 title 1
- 239000002131 composite material Substances 0.000 title 1
Classifications
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02G—INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES
- H02G3/00—Installations of electric cables or lines or protective tubing therefor in or on buildings, equivalent structures or vehicles
- H02G3/36—Installations of cables or lines in walls, floors or ceilings
-
- 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
- B64C1/18—Floors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02G—INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES
- H02G3/00—Installations of electric cables or lines or protective tubing therefor in or on buildings, equivalent structures or vehicles
- H02G3/36—Installations of cables or lines in walls, floors or ceilings
- H02G3/38—Installations of cables or lines in walls, floors or ceilings the cables or lines being installed in preestablished conduits or ducts
- H02G3/386—Installations of cables or lines in walls, floors or ceilings the cables or lines being installed in preestablished conduits or ducts in walls
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0958371A FR2953093B1 (en) | 2009-11-25 | 2009-11-25 | COMPOSITE STRUCTURAL ELEMENT WITH ELECTRICAL TRANSMISSION OF INTEGRATED POWER |
PCT/EP2010/068145 WO2011064263A2 (en) | 2009-11-25 | 2010-11-24 | Composite structural element having a built-in electrical power transmission |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0958371A FR2953093B1 (en) | 2009-11-25 | 2009-11-25 | COMPOSITE STRUCTURAL ELEMENT WITH ELECTRICAL TRANSMISSION OF INTEGRATED POWER |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2953093A1 FR2953093A1 (en) | 2011-05-27 |
FR2953093B1 true FR2953093B1 (en) | 2012-11-09 |
Family
ID=42270489
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0958371A Active FR2953093B1 (en) | 2009-11-25 | 2009-11-25 | COMPOSITE STRUCTURAL ELEMENT WITH ELECTRICAL TRANSMISSION OF INTEGRATED POWER |
Country Status (2)
Country | Link |
---|---|
FR (1) | FR2953093B1 (en) |
WO (1) | WO2011064263A2 (en) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2977733B1 (en) * | 2011-07-05 | 2018-07-27 | European Aeronautic Defence And Space Company Eads France | ASSEMBLED STRUCTURE WITH ELECTRIC CONTINUITY |
FR2977861B1 (en) * | 2011-07-13 | 2015-01-16 | Eads Europ Aeronautic Defence | SUPPORT STRAP FOR A STRUCTURE OF AN AIRCRAFT AND ASSOCIATED AIRCRAFT |
RU2014138578A (en) | 2012-02-24 | 2016-04-10 | Сигмент Десигн Металс Лтд. | Combined structural element |
FR2995464B1 (en) * | 2012-09-08 | 2021-05-14 | Cqfd Composites | BEAM CONTAINING ELECTRICAL CONDUCTORS AND ELECTRIFICATION SYSTEM USING SUCH BEAMS |
DE102015213271A1 (en) * | 2015-07-15 | 2017-01-19 | Siemens Aktiengesellschaft | Aircraft with a support structure for transmitting electrical energy between a power source and an energy consumer |
US10053203B2 (en) * | 2015-10-13 | 2018-08-21 | The Boeing Company | Composite stiffener with integral conductive element |
US11014337B2 (en) | 2016-12-14 | 2021-05-25 | The Boeing Company | Laminate structures comprising fiber-reinforced thermoplastic prepreg plies |
US11077644B2 (en) | 2016-12-14 | 2021-08-03 | The Boeing Company | Material systems and methods of manufacturing material systems |
US11273622B2 (en) | 2016-12-14 | 2022-03-15 | The Boeing Company | Stiffening elements that comprise integral current flowpaths |
FR3068952B1 (en) * | 2017-07-11 | 2019-07-26 | Airbus Sas | FUSELAGE AND AIRCRAFT COMPRISING A MULTIFUNCTIONAL AIR DISTRIBUTION SUB-STRUCTURE AND METHOD OF ASSEMBLY |
DE102019109149A1 (en) * | 2019-04-08 | 2020-10-08 | Airbus Operations Gmbh | Rail for fastening equipment elements in aircraft, in particular seats, and method of manufacture |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3531028A1 (en) * | 1985-08-30 | 1987-03-05 | Velden Alexander Jacobus Maria | Reinforced structure |
US7661229B2 (en) * | 2005-05-12 | 2010-02-16 | Worthington Armstrong Venture | Electrical conductivity in a suspended ceiling system |
DE102006050534B4 (en) * | 2006-10-26 | 2013-12-12 | Airbus Operations Gmbh | Conduit system for an aircraft, in particular an aircraft |
-
2009
- 2009-11-25 FR FR0958371A patent/FR2953093B1/en active Active
-
2010
- 2010-11-24 WO PCT/EP2010/068145 patent/WO2011064263A2/en active Application Filing
Also Published As
Publication number | Publication date |
---|---|
WO2011064263A3 (en) | 2012-05-31 |
FR2953093A1 (en) | 2011-05-27 |
WO2011064263A2 (en) | 2011-06-03 |
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Legal Events
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PLFP | Fee payment |
Year of fee payment: 7 |
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Year of fee payment: 14 |
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PLFP | Fee payment |
Year of fee payment: 15 |