-
公开(公告)号：CA2753761A1
公开(公告)日：2010-09-02
申请号：CA2753761
申请日：2010-02-25
Applicant: BAE SYSTEMS PLC
Inventor： DUNLEAVY MICHAEL , HAQ SAJAD , HUCKER MARTYN JOHN
Abstract: A method for electroless metal deposition on a surface in a finely dimensioned space (e.g. the bore of a hollow fibre) comprises introducing into said space an electroless plating solution that has a nil or relatively low plating rate at normal room temperature, and there after heating said structure to an elevated temperature for a period sufficient to cause metal to plate on the wall surface. The steps of introducing and heating may be repeated as necessary to build up a required thickness.
-
公开(公告)号：ES2341883T3
公开(公告)日：2010-06-29
申请号：ES06744278
申请日：2006-06-22
Applicant: BAE SYSTEMS PLC
Inventor： DUNLEAVY MICHAEL , HAQ SAJAD
IPC: B29C73/22 , B29C70/10 , B29K101/10 , B29K309/08 , B29L31/30
Abstract: Una estructura que comprende una pluralidad de fibras huecas que están ensambladas para formar un cuerpo de material compuesto, estando dispuestas las fibras en pares, conteniendo una fibra de cada par un material resinoso sin curar como componente de una composición resinosa curable de dos componentes y comprendiendo la otra un agente de curado de la composición resinosa de dos componentes, siendo dicha una fibra de cada par conectable a un primer depósito de dicho material resinoso sin curar, pudiéndose suministrar desde dicho primer depósito dicho material resinoso sin curar a dicha una fibra de cada par bajo presión, y siendo dicha otra fibra de cada par conectable a un segundo depósito de dicho agente de curado, pudiéndose suministrar desde dicho segundo depósito dicho agente de curado a dicha otra fibra de cada par bajo presión, por lo que, en caso de que se produzca una fractura en cualquiera de las fibras, se produce la combinación de los dos componentes en la región de la fractura para permitir el curado de la composición y el sellado de la fractura.
-
公开(公告)号：DE602006012982D1
公开(公告)日：2010-04-29
申请号：DE602006012982
申请日：2006-06-22
Applicant: BAE SYSTEMS PLC
Inventor： DUNLEAVY MICHAEL , HAQ SAJAD
IPC: B29C73/22 , B29C70/10 , B29K101/10 , B29K309/08 , B29L31/30
Abstract: This invention relates to a structure which comprises hollow and solid fibre material embedded in a resin matrix where a repair facility is provided for repairing fractures in the fibres and in the resin matrix by the use of curable two-part adhesive compositions in some of the fibres of the structure. Single fibres (58) can be deployed within the structure where each single fibre (58) carries one component of the composition and the fibre itself is coated along its exterior with the second component (60) so that in the event of fracture of any fibres, the component parts of the adhesive composition can combine and cure in situ to fill and 'heal' the fracture. The invention has particular but not exclusive application to in 'flight' repair of aircraft components which are formed by such structures, and can also be used in the manufacture of fabric materials.
-
公开(公告)号：AT461033T
公开(公告)日：2010-04-15
申请号：AT06744278
申请日：2006-06-22
Applicant: BAE SYSTEMS PLC
Inventor： DUNLEAVY MICHAEL , HAQ SAJAD
IPC: B29C73/22 , B29C70/10 , B29K101/10 , B29K309/08 , B29L31/30
Abstract: This invention relates to a structure which comprises hollow and solid fibre material embedded in a resin matrix where a repair facility is provided for repairing fractures in the fibres and in the resin matrix by the use of curable two-part adhesive compositions in some of the fibres of the structure. Single fibres (58) can be deployed within the structure where each single fibre (58) carries one component of the composition and the fibre itself is coated along its exterior with the second component (60) so that in the event of fracture of any fibres, the component parts of the adhesive composition can combine and cure in situ to fill and 'heal' the fracture. The invention has particular but not exclusive application to in 'flight' repair of aircraft components which are formed by such structures, and can also be used in the manufacture of fabric materials.
-
公开(公告)号：AU2009269832A1
公开(公告)日：2010-01-14
申请号：AU2009269832
申请日：2009-06-25
Applicant: BAE SYSTEMS PLC
Inventor： HUCKER MARTYN JOHN , WEBBERELY PHILIP LAWRENCE , DYKE AMY ELIZABETH , DUNLEAVY MICHEAL , HAQ SAJAD
Abstract: An electrical power source including at least one hollow fiber incorporated in a material structure, wherein the at least one hollow fiber forms part of an electric circuit capable of storing or generating electrical power. In this way power sources may be provided as an integral part of a fiber composite structure or fabric.
-
Patent Agency Ranking
公开(公告)号：DE602006005930D1
公开(公告)日：2009-05-07
申请号：DE602006005930
申请日：2006-06-22
Applicant: BAE SYSTEMS PLC
Inventor： HAQ SAJAD , DUNLEAVY MICHAEL
IPC: B29C70/22 , B29C70/10 , B29K101/10 , B29K309/08 , B29L31/30
Abstract: The invention relates to the use of fibre composites and specifically to the use of adhesive compositions within hollow fibres of the composites to provide a repair function within the composite in the event of damage to of the fibres. The invention relates to the manner in which one-part adhesive compositions can be delivered to a point of fracture. The invention is more specifically concerned with the use of pressure to deliver adhesive composition to the point of damage.
-
公开(公告)号：CA2378164C
公开(公告)日：2006-05-16
申请号：CA2378164
申请日：2000-06-29
Applicant: BAE SYSTEMS PLC
Inventor： HAQ SAJAD , HUDD JENNIFER , SOMERTON CHRISTOPHER , DUNLEAVY MICHAEL
Abstract: A filled hollow fibre composite material is made by laying up a plurality of prepreg plies (1) of hollow fibre composite material and non-stick film material (2) one on top of another with the non-stick film material (2) interleaving successive plies (1) at selected areas thereof. The laid up interleaved plies are treated to resin bond the ply areas (3) not interleave d with the non-stick film material and leave the interleaved areas (4) unbonde d. The so formed laminate is treated at edge regions to expose open unfilled hollow fibre ends (5, 6) and the plies in the unbonded interleaved areas (4) are separated at the non-stick film material (2) to provide access to the op en hollow fibre ends (7) in each ply for the introduction of a film material in to the hollow fibres through the open hollow fibre ends (7) in one or more of t he separated plies (1) to form a filled hollow fibre components material.
-
公开(公告)号：AU764873B2
公开(公告)日：2003-09-04
申请号：AU5693000
申请日：2000-06-29
Applicant: BAE SYSTEMS PLC
Inventor： DUNLEAVY MICHAEL , SOMERTON CHRISTOPHER , HUDD JENNIFER , HAQ SAJAD
Abstract: A filled hollow fibre composite material is made by laying up a plurality of prepreg plies (1) of hollow fibre composite material and non-stick film material (2) one on top of another with the non-stick film material (2) interleaving successive plies (1) at selected areas thereof. The laid up interleaved plies are treated to resin bond the ply areas (3) not interleaved with the non-stick film material and leave the interleaved areas (4) unbonded. The so formed laminate is treated at edge regions to expose open unfilled hollow fibre ends (5, 6) and the plies in the unbonded interleaved areas (4) are separated at the non-stick film material (2) to provide access to the open hollow fibre ends (7) in each ply for the introduction of a film material into the hollow fibres through the open hollow fibre ends (7) in one or more of the separated plies (1) to form a filled hollow fibre composite material.
-
公开(公告)号：ES2182808T3
公开(公告)日：2003-03-16
申请号：ES00942225
申请日：2000-06-29
Applicant: BAE SYSTEMS PLC
Inventor： DUNLEAVY MICHAEL , SOMERTON CHRISTOPHER , HUDD JENNIFER , HAQ SAJAD
Abstract: A filled hollow fibre composite material is made by laying up a plurality of prepreg plies (1) of hollow fibre composite material and non-stick film material (2) one on top of another with the non-stick film material (2) interleaving successive plies (1) at selected areas thereof. The laid up interleaved plies are treated to resin bond the ply areas (3) not interleaved with the non-stick film material and leave the interleaved areas (4) unbonded. The so formed laminate is treated at edge regions to expose open unfilled hollow fibre ends (5, 6) and the plies in the unbonded interleaved areas (4) are separated at the non-stick film material (2) to provide access to the open hollow fibre ends (7) in each ply for the introduction of a film material into the hollow fibres through the open hollow fibre ends (7) in one or more of the separated plies (1) to form a filled hollow fibre composite material.
-
公开(公告)号：DE69624188T2
公开(公告)日：2003-02-13
申请号：DE69624188
申请日：1996-08-14
Applicant: BAE SYSTEMS PLC FARNBOROUGH
Inventor： HAQ SAJAD
Abstract: Chiral composite material is made using an apertured plate (2) having apertures (3) therethrough corresponding to the desired location of Chiral elements (4) in the composite material. The plate (2) is located to overlie a substrate (1) with or without the intermission of spacer (10) which may be apertured in correspondence with the plate (2) or which may be ring like in form. The Chiral elements (4) are held in position by locating means such as a tab (5) which may be magnetic in, on or associated with the plate (2) and a first layer (8) of liquid host material is placed in the apertures (3) around the elemtns (4) against the substrate (1), allowed to set and the plate (2) removed. A second layer (9) of liquid host material is then applied to the set first layer (8) and allowed to set to produce the desired composite material.
-
-
-
-
-
-
-
-
-
Search Results
100
records
(took 0.03 seconds)
