公开(公告)号：EP2909008B1

公开(公告)日：2018-04-11

申请号：EP12887148.0

申请日：2012-10-22

Applicant: SAAB AB

Inventor： RYDBOM, Anders

IPC: B29C70/08 ,  B64C1/00 ,  B64C3/20 ,  B29C65/50 ,  B29C70/14 ,  B32B5/28 ,  B64C3/26 ,  B29C70/24 ,  B29L31/30 ,  B29K105/12 ,  B32B5/02 ,  B29C65/48

CPC classification number: B29C70/08 ,  B29C65/483 ,  B29C65/488 ,  B29C65/5014 ,  B29C65/5057 ,  B29C66/1122 ,  B29C66/3034 ,  B29C66/30341 ,  B29C66/474 ,  B29C66/532 ,  B29C66/543 ,  B29C66/61 ,  B29C66/7212 ,  B29C66/72143 ,  B29C66/73751 ,  B29C66/73754 ,  B29C70/14 ,  B29C70/24 ,  B29D99/0014 ,  B29K2105/124 ,  B29L2031/085 ,  B29L2031/3055 ,  B29L2031/3064 ,  B29L2031/3076 ,  B29L2031/3085 ,  B32B5/024 ,  B32B5/26 ,  B32B2260/023 ,  B32B2260/046 ,  B32B2262/0269 ,  B32B2262/106 ,  B32B2307/54 ,  B32B2307/542 ,  B32B2605/18 ,  B64C3/187 ,  B64C3/20 ,  B64C3/26 ,  Y02P70/523 ,  Y02T50/43 ,  B29K2307/04

Abstract: The present invention relates to a torsion-box type airfoil structure. The structure (3) being formed by joined structural composite parts (5, 7, 9, 11) made of fiber reinforced plies (19) stacked onto each other. At least a first (11) and a second structural part (5) being joined by embedding a plurality of elongated reinforcement fiber-like elements (17, 17', 23, 23', 23'', 23''') in said first (11) and second (5) structural parts, wherein said fiber-like elements (17, 17', 23, 23', 23'', 23''') connect said parts to each other.

公开(公告)号：EP2909009A1

公开(公告)日：2015-08-26

申请号：EP12887291.8

申请日：2012-10-22

Applicant: SAAB AB

Inventor： NORDIN, Pontus ,  RYDBOM, Anders ,  VÅNGELL, Tomas

IPC: B29C70/08 ,  B29C70/14 ,  B29C70/30 ,  B32B5/28 ,  B64C23/06

CPC classification number: B29C70/14 ,  B29C70/081 ,  B29C70/30 ,  B29L2031/3085 ,  B32B5/024 ,  B32B5/12 ,  B32B5/26 ,  B32B7/12 ,  B32B2260/023 ,  B32B2260/046 ,  B32B2262/0269 ,  B32B2262/101 ,  B32B2262/106 ,  B32B2307/558 ,  B32B2605/18 ,  B64C23/069 ,  Y02T50/164

Abstract: The present invention regards a structurally integrated curved structure (13, 13', 13'') comprising a curved transition region (15) being defined between a tip section (42) and a root section (11, 21), an upper and lower composite skin (27, 29) comprising an inner surface (45) fixed to a substructure (31) of said transition region (15), the substructure (31) and skins (27, 29) are, during use of the structure (13, 13', 13''), subjected to a bending moment (M), each skin (27, 29) of said transition region (15) comprises elongated reinforcement fiber-like elements. The lower composite skin (29) comprises reinforcing fibersand/or nano tubes(41, 43), which are oriented transverse to the inner surface (45). The invention also regard sa method for producing the structurally integrated curved structure (13, 13', 13'').

公开(公告)号：EP2909008A1

公开(公告)日：2015-08-26

申请号：EP12887148.0

申请日：2012-10-22

Applicant: SAAB AB

Inventor： RYDBOM, Anders

IPC: B29C70/08 ,  B64C1/00 ,  B64C3/20 ,  B29C65/50 ,  B29C70/14 ,  B32B5/28 ,  B64C3/26

CPC classification number: B29C70/08 ,  B29C65/483 ,  B29C65/488 ,  B29C65/5014 ,  B29C65/5057 ,  B29C66/1122 ,  B29C66/3034 ,  B29C66/30341 ,  B29C66/474 ,  B29C66/532 ,  B29C66/543 ,  B29C66/61 ,  B29C66/7212 ,  B29C66/72143 ,  B29C66/73751 ,  B29C66/73754 ,  B29C70/14 ,  B29C70/24 ,  B29D99/0014 ,  B29K2105/124 ,  B29L2031/085 ,  B29L2031/3055 ,  B29L2031/3064 ,  B29L2031/3076 ,  B29L2031/3085 ,  B32B5/024 ,  B32B5/26 ,  B32B2260/023 ,  B32B2260/046 ,  B32B2262/0269 ,  B32B2262/106 ,  B32B2307/54 ,  B32B2307/542 ,  B32B2605/18 ,  B64C3/187 ,  B64C3/20 ,  B64C3/26 ,  Y02P70/523 ,  Y02T50/43 ,  B29K2307/04

Abstract: The present invention relates to a torsion-box type airfoil structure. The structure (3) being formed by joined structural composite parts (5, 7, 9, 11) made of fiber reinforced plies (19) stacked onto each other. At least a first (11) and a second structural part (5) being joined by embedding a plurality of elongated reinforcement fiber-like elements (17, 17', 23, 23', 23'', 23''') in said first (11) and second (5) structural parts, wherein said fiber-like elements (17, 17', 23, 23', 23'', 23''') connect said parts to each other.