RU96119509A - PANEL FROM COMPOSITE MATERIAL - Google Patents

PANEL FROM COMPOSITE MATERIAL

Info

Publication number
RU96119509A
RU96119509A RU96119509/28A RU96119509A RU96119509A RU 96119509 A RU96119509 A RU 96119509A RU 96119509/28 A RU96119509/28 A RU 96119509/28A RU 96119509 A RU96119509 A RU 96119509A RU 96119509 A RU96119509 A RU 96119509A
Authority
RU
Russia
Prior art keywords
casing
panel
composite material
stringers
legs
Prior art date
Application number
RU96119509/28A
Other languages
Russian (ru)
Other versions
RU2112698C1 (en
Inventor
Л.А. Климакова
Original Assignee
Обнинское научно-производственное предприятие "Технология"
Filing date
Publication date
Application filed by Обнинское научно-производственное предприятие "Технология" filed Critical Обнинское научно-производственное предприятие "Технология"
Priority to RU96119509A priority Critical patent/RU2112698C1/en
Priority claimed from RU96119509A external-priority patent/RU2112698C1/en
Application granted granted Critical
Publication of RU2112698C1 publication Critical patent/RU2112698C1/en
Publication of RU96119509A publication Critical patent/RU96119509A/en

Links

Claims (1)

Панель из композиционного материала, содержащая обшивку, продольные стрингеры и поперечные элементы подкрепления, изготовленные совместно с обшивкой, отличающаяся тем, что поперечные элементы подкрепления выполнены в виде силовых поясов (усилений), которые располагаются либо на обшивке, либо на лапках стрингеров, либо на обшивке и лапках стрингеров, либо на обшивке, лапках и стенках стрингеров.A panel of composite material containing a casing, longitudinal stringers and transverse reinforcement elements made together with the casing, characterized in that the transverse reinforcement elements are made in the form of power belts (reinforcements), which are located either on the casing, or on the legs of the stringers, or on the casing and the legs of the stringers, or on the casing, legs and walls of the stringers.
RU96119509A 1996-09-30 1996-09-30 Panel made from composite material RU2112698C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU96119509A RU2112698C1 (en) 1996-09-30 1996-09-30 Panel made from composite material

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU96119509A RU2112698C1 (en) 1996-09-30 1996-09-30 Panel made from composite material

Publications (2)

Publication Number Publication Date
RU2112698C1 RU2112698C1 (en) 1998-06-10
RU96119509A true RU96119509A (en) 1998-11-20

Family

ID=20186080

Family Applications (1)

Application Number Title Priority Date Filing Date
RU96119509A RU2112698C1 (en) 1996-09-30 1996-09-30 Panel made from composite material

Country Status (1)

Country Link
RU (1) RU2112698C1 (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0624208D0 (en) * 2006-12-04 2007-01-10 Airbus Uk Ltd Composite structure
GB0709118D0 (en) 2007-05-14 2007-06-20 Airbus Uk Ltd Reinforced panel
WO2010136741A2 (en) * 2009-05-28 2010-12-02 Societe Lorraine De Construction Aeronautique Composite structuring panel for the trailing edge of an aircraft element
GB201000878D0 (en) 2010-01-20 2010-03-10 Airbus Operations Ltd Sandwich panel
GB201016279D0 (en) * 2010-09-28 2010-11-10 Airbus Operations Ltd Stiffener run-out
GB201220937D0 (en) * 2012-11-21 2013-01-02 Airbus Uk Ltd Modular structural assembly
RU2542801C2 (en) * 2013-07-18 2015-02-27 Александр Николаевич Кирилин Light-weight integral panel of polymer composites for aircraft contouring components

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