-
1.Method of configuring composite core in a core stiffened structure and a structure incorporating the same 有权
Title translation: 一种用于在结构和结构顺序的复合材料芯的配置方法kernversteiften公开(公告)号:EP2832533B1
公开(公告)日:2016-03-23
申请号:EP13195029.7
申请日:2013-11-29
Applicant: Bell Helicopter Textron Inc.
Inventor: KENDRICK, Phillip A. , CARLSON, David G. , OLDROYD, Paul K.
CPC classification number: B32B37/146 , B29C65/483 , B29C65/4835 , B29C65/486 , B29C65/5042 , B29C65/5057 , B29C65/7838 , B29C66/0042 , B29C66/1122 , B29C66/1142 , B29C66/5227 , B29C66/54 , B29C66/612 , B29C66/71 , B29C66/7212 , B29C66/72141 , B29C66/72143 , B29C66/7254 , B29C66/7392 , B29C66/7394 , B29C66/8122 , B29C66/81261 , B29C66/81467 , B29C66/8185 , B29C66/8284 , B29C66/83415 , B29D99/0021 , B29L2031/3076 , B29L2031/3088 , B29L2031/608 , B32B3/04 , B32B3/12 , B32B5/12 , B32B5/142 , B32B7/12 , B32B2038/0076 , B32B2260/023 , B32B2260/046 , B32B2307/302 , B32B2605/00 , B32B2605/18 , B64C1/18 , B64C3/20 , Y10T156/1093 , Y10T428/24149 , Y10T428/24165 , B29K2827/18 , B29K2307/04 , B29K2077/00 , B29K2309/08 , B29K2277/10 , B29K2071/00 , B29K2067/00 , B29K2061/00 , B29K2081/04 , B29K2063/00 , B29K2079/08 , B29K2031/00 , B29K2061/04
-
2.Method of configuring composite core in a core stiffened structure and a structure incorporating the same 有权
Title translation: Verfahren zur Konfiguration eines Verbundkerns in einer kernversteiften Struktur und Struktur damit公开(公告)号:EP2832533A1
公开(公告)日:2015-02-04
申请号:EP13195029.7
申请日:2013-11-29
Applicant: Bell Helicopter Textron Inc.
Inventor: KENDRICK, Phillip A. , CARLSON, David G. , OLDROYD, Paul K.
CPC classification number: B32B37/146 , B29C65/483 , B29C65/4835 , B29C65/486 , B29C65/5042 , B29C65/5057 , B29C65/7838 , B29C66/0042 , B29C66/1122 , B29C66/1142 , B29C66/5227 , B29C66/54 , B29C66/612 , B29C66/71 , B29C66/7212 , B29C66/72141 , B29C66/72143 , B29C66/7254 , B29C66/7392 , B29C66/7394 , B29C66/8122 , B29C66/81261 , B29C66/81467 , B29C66/8185 , B29C66/8284 , B29C66/83415 , B29D99/0021 , B29L2031/3076 , B29L2031/3088 , B29L2031/608 , B32B3/04 , B32B3/12 , B32B5/12 , B32B5/142 , B32B7/12 , B32B2038/0076 , B32B2260/023 , B32B2260/046 , B32B2307/302 , B32B2605/00 , B32B2605/18 , B64C1/18 , B64C3/20 , Y10T156/1093 , Y10T428/24149 , Y10T428/24165 , B29K2827/18 , B29K2307/04 , B29K2077/00 , B29K2309/08 , B29K2277/10 , B29K2071/00 , B29K2067/00 , B29K2061/00 , B29K2081/04 , B29K2063/00 , B29K2079/08 , B29K2031/00 , B29K2061/04
Abstract: A method of manufacturing a core stiffened structure includes orienting the plurality of core wafers (2401) in a non-uniform pattern onto a first face sheet (2805), the non-uniform pattern producing non-uniform spacing (2809) between adjacent core wafers; assembling a second face sheet (2803) onto the plurality of wafers (2401); and curing an adhesive to create a bond between the plurality of wafers (2401), the first face sheet (2805), and the second face sheet (2803).
Abstract translation: 一种制造芯加强结构的方法包括将多个芯晶片(2401)以不均匀图案定向到第一面板(2805)上,所述不均匀图案在相邻芯片之间产生不均匀间隔(2809) ; 将第二面板(2803)组装到所述多个晶片(2401)上; 以及固化粘合剂以在所述多个晶片(2401),所述第一面板(2805)和所述第二面板(2803)之间形成结合。
-