T桁条相关的专利数据

序号	专利名	申请号	申请日	公开（公告）号	公开（公告）日	发明人
161	METHOD AND TOOL FOR PRODUCING A T-STRINGER	PCT/EP2008057608	2008-06-17	WO2009010357A3	2009-03-12	LENGSFELD HAUKE; LUEBBERING CHRISTIAN
The invention relates to a method and to a tool (1, 48) for producing a T-stringer, in particular in air travel and space travel. The method is characterised in that two intermediate strips (3, 4) are superimposed, sections (5, 6) of said intermediate strips (3, 4) being associated with a stringer base (60) that is to be formed, are separated from each other by means of separation films (7, 8) and the sections (14, 15) of the intermediate strips (14, 15) associated with a stringer rod (61) are brought into direct contact, in particular in a material fit. In a further method step, the sections (5, 6) of the intermediate strips (3, 4) associated with the stringer rod (61) that is to be formed are clamped in a clamping device (1). In another method step, the sections (5, 6) that are associated with the stinger base (60) that is to be formed, are folded in the counter direction (28, 29) by means of an unfolding pin (25) and pressed counter to the corresponding pressure surfaces (23, 24) of the clamping device (1) by means of a pressing cylinder (37), such that the sections (5, 6) are aligned exactly. Subsequently, only the folded intermediate strips (3, 4) are hardened in order to form the T-stringer that is to be produced. The invention method has an advantage over known methods for producing T-stringers in that a smaller number of steps are required in order to produce the T-stringer, and said steps could easy be automated.
162	用於製造格子桁的方法及裝置 METHOD AND DEVICE FOR PRODUCING A LATTICE GIRDER	TW094103148	2005-02-02	TWI304001B	2008-12-11	克勞斯利特爾 RITTER, KLAUS
本發明係關於用於製造格子桁(G, G')之方法,此格子桁係由至少一條上弦、至少一條下弦(U, U')及來回延伸在上弦與下弦間之至少一支柱線(Z, Z')所組成,以鋸齒狀予以彎曲具有彎曲頂點在上弦端和下弦端,並將每一者焊接至上弦和下弦上,其中選擇格子桁以內支柱線的鄰近彎曲頂點(S, S')的間距(T, T')是可變,其中可將下弦進給入各種進給平面(X-X, X-X')中及其中,將格子桁在預定之切割位置上自連續產生之材料股線上切斷。
163	Joint for composite wings	US13675809	2012-11-13	US09272769B2	2016-03-01	Chun-Liang Lin; Ryan M Mahn; Karl B Lee
A wing joint including a T-chord and a splice plate for connecting an inboard wing panel assembly and an outboard wing panel assembly. The wing panel assemblies include a stringer co-bonded or co-cured with a wing skin. The webbing and cap of the stringer may be trimmed to expose a noodle and base flange. The noodle and base flange interface with the bottom of the T-chord and the wing skin interfaces with the splice plate. The exposed noodle may be non-flush with the base flange of the trimmed stringer. The bottom of the T-chord may include a groove to accommodate a non-flush noodle so that a gap does not exist between the T-chord and the base flange. Alternatively, shims may be used to compensate for a non-flush noodle or the base flange and web may include sacrificial plies permitting the base flange and web to be trimmed flush with the noodle.
164	JOINT FOR COMPOSITE WINGS	US13675809	2012-11-13	US20140131518A1	2014-05-15	Chun-Liang Lin; Ryan M. Mahn; Karl B. Lee
A wing joint including a T-chord and a splice plate for connecting an inboard wing panel assembly and an outboard wing panel assembly. The wing panel assemblies include a stringer co-bonded or co-cured with a wing skin. The webbing and cap of the stringer may be trimmed to expose a noodle and base flange. The noodle and base flange interface with the bottom of the T-chord and the wing skin interfaces with the splice plate. The exposed noodle may be non-flush with the base flange of the trimmed stringer. The bottom of the T-chord may include a groove to accommodate a non-flush noodle so that a gap does not exist between the T-chord and the base flange. Alternatively, shims may be used to compensate for a non-flush noodle or the base flange and web may include sacrificial plies permitting the base flange and web to be trimmed flush with the noodle.
165	복합재 날개용 조인트	KR1020130128067	2013-10-25	KR1020140061237A	2014-05-21	린,천-리앙; 만,라이언엠.; 리,카알비.
A wing joint includes a T-chord and a splice plate for connecting an inboard wing panel assembly and an outboard wing panel assembly. The wing panel assemblies include a stringer co-bonded or co-cured with a wing skin. The web and cap of the stringer may be trimmed to expose a noodle and a base flange. The noodle and the base flange interface with the bottom of the T-chord and the wing skin interfaces with the splice plate. The exposed noodle may be non-flush with the base flange of the trimmed stringer. The bottom of the T-chord may include a groove to accommodate a non-flush noodle so that a gap does not exist between the T-chord and the base flange. Alternatively, shims may be used to compensate for a non-flush noodle or the base flange and web may include sacrificial plies permitting the base flange and web to be trimmed flush with the noodle.
166	Roof truss and roof structure	JP2005118697	2005-04-15	JP2006299534A	2006-11-02	KATO TOSHIKAZU
<P>PROBLEM TO BE SOLVED: To provide a roof truss and a roof structure formed by making use thereof capable of forming a required shape by the planned number of upper chord constituent members and, at the same time, finishing the surface of a roof with a smooth curved surface. <P>SOLUTION: The roof truss is so constituted that purlin engaged sections 12, 2 and 32 are provided to each outside surface of upper chord constituent members 1, 2 and 3 at predetermined intervals and that the purlin engaged sections have different depths due to a position wherein each purlin section has to be placed. The roof structure is so constituted that a plurality of roof truss T are lined up in the direction of the ridge of a building, a plurality of purlin 61, 62 and 63 are engaged with the purlin engaged sections provided to the upper chord constituent members of the roof truss to provide and that roof imported timber is extended to a curved surface through the outer surface of the purlin. <P>COPYRIGHT: (C)2007,JPO&INPIT
167	Joint for composite wings	JP2013225969	2013-10-30	JP2014097786A	2014-05-29	LIN CHUN-LIANG; MAHN RYAN M; LEE KARL B
PROBLEM TO BE SOLVED: To provide a wing joint including a T-chord and a splice plate for connecting an inboard wing panel assembly and an outboard wing panel assembly.SOLUTION: The wing panel assemblies comprise a stringer 60 co-bonded or co-cured with a wing skin 40, 50. A webbing 62 and a cap of the stringer may be trimmed to expose a noodle and a base flange. The noodle and the base flange interface with the bottom of a T-chord 10, and the wing skin interfaces with a splice plate 15. The exposed noodle may be non-flush with the base flange of the trimmed stringer. The bottom of the T-chord may include a groove to accommodate the noodle so that a gap does not exist between the T-chord and the base flange. Alternatively, shims may be used to compensate for the noodle, or the base flange and a web may include sacrificial plies permitting the base flange and the web to be trimmed to be flush with the noodle.
168	Structural framing system for buildings	US022068	1993-02-24	US5341611A	1994-08-30	Robert C. Lewis
A structural frame for a building including multiple truss members and multiple column members. The column members are comprised of multiple upstanding support members and are connected to the truss members by means of a mortise-and-tenon type connection. A plurality of T-purlins, having face boards and cross brace boards, interconnect the rafters of the truss members and the joists of the truss members. A face girt is secured to the lower ends of the rafters so that an external roof structure can be attached to the girts at the same slope and elevation from the rafters as compared to the face boards of the T-purlins.
169	Joint for composite wings	EP13192586.9	2013-11-12	EP2730498A2	2014-05-14	Lin, Chun-Liang; Mahn, Ryan M; Lee, Karl B
A wing joint (1) including a T-chord (10) and a splice plate (15) for connecting an inboard wing panel assembly (20) and an outboard wing panel assembly (30). The wing panel assemblies include a stringer (60) co-bonded or co-cured with a wing skin. The webbing and cap of the stringer may be trimmed to expose a noodle and base flange. The noodle and base flange interface with the bottom of the T-chord and the wing skin interfaces with the splice plate (16,17). The exposed noodle may be non-flush with the base flange of the trimmed stringer. The bottom of the T-chord may include a groove to accommodate a non-flush noodle so that a gap does not exist between the T-chord and the base flange. Alternatively, shims may be used to compensate for a non-flush noodle or the base flange and web may include sacrificial plies permitting the base flange and web to be trimmed flush with the noodle.
170	복합재 날개용 조인트	KR1020160055068	2016-05-04	KR1020160058732A	2016-05-25	린,천-리앙; 만,라이언엠.; 리,카알비.
날개조인트는내부날개패널조립체와외부날개패널조립체를연결하기위한 T-코드와스플라이스판을포함한다. 날개패널조립체들은날개표피와공동접합또는공동경화된스트링거를포함한다. 스트링거의웹과캡은누들과기저플랜지를노출하기위하여트리밍될수 있다. 누들과기저플랜지는 T-코드의바닥부와접속하고또 날개표피는스플라이스판과접속한다. 노출된누들은트리밍된스트링거의기저플랜지와동일한높이가아닐수 있다. T-코드의바닥부는 T-코드와기저플랜지사이에간극이존재하지않도록같은높이가아닌누들을수용하기위하여홈을포함할수 있다. 대신에, 동일한높이가아닌누들을보상하기위하여심이사용될수 있거나기저플랜지또는웹은기저플랜지및 웹이누들과동일한높이로트리밍되는것을허용하는희생플라이들을포함할수 있다.
171	SELF-CENTERING CEILING PANEL	US13082159	2011-04-07	US20110252736A1	2011-10-20	David Bailey; Ko Kuperus; Richard Mayer
A panel for a drop ceiling is made of a semi-rigid but resilient material such as spring steel and includes corner clips adapted to cooperate with the inverted T-shaped stringers of a drop ceiling support system so that the panel is self-centering between opposing stringers and is spring biased into a clamped relationship with horizontal flanges of the inverted T-shape stringers to prevent the panel from moving up and down. The corner clips are also designed to transfer any horizontal compressive shear force in the mounting system to vertical edges of the panel so as not to undesirably bow the flat base of the panel.
172	Positioning, handling and assembling system for manufacture of aeronautical parts	US12387302	2009-04-30	US08122576B2	2012-02-28	José Manuel Santos Gómez; José Manuel Menéndez Martín; Antonio Durán Quiroga; Aquilino García García; Julián Sánchez Fernández
The system has special application in the manufacture of aircraft wing covers (10 made of carbon fiber and the stringers (3) cured jointly with the wing cover during the polymerization in autoclave. The tool pieces (4) being used are defined by angular elements (5, 6) copying the geometry of the stringers (3). The shape of these stringers corresponds to the “T” section. The angular elements (5, 6) comprise, in their upper part, a pair of battlements (7) in order to be caught by part of the clamps (9) of a head (10) linked to a robot (11) of the spherical type with articulated arm with six axes. The angular elements (5, 6) are made of INVAR material and they are used to keep in position the stringers during the curing cycle in the autoclave.
173	Self-centering ceiling panel	US13082159	2011-04-07	US08572920B2	2013-11-05	David Bailey; Ko Kuperus; Richard Mayer
A panel for a drop ceiling is made of a semi-rigid but resilient material such as spring steel and includes corner clips adapted to cooperate with the inverted T-shaped stringers of a drop ceiling support system so that the panel is self-centering between opposing stringers and is spring biased into a clamped relationship with horizontal flanges of the inverted T-shape stringers to prevent the panel from moving up and down. The corner clips are also designed to transfer any horizontal compressive shear force in the mounting system to vertical edges of the panel so as not to undesirably bow the flat base of the panel.
174	用於太陽能模組之鋼構支架	TW101115873	2012-05-04	TW201346201A	2013-11-16	孫文郁
本發明係配合鋼構之柱樑間距，利用鋼構件(鋼結構制式規格構件)，將間接結合之鋁合金支架省略，直接將鋼構之桁條或小樑或支架等構件作為太陽能模組支架，可採銲接式或螺接式結合，以隔絕不同金屬間因電位差造成之鏽蝕問題。本發明之一種用於太陽能模組之背鎖式鋼構支架，其係包括複數條鋼構件、複數條L型角鋼、複數條T型角鋼、複數個墊片與複數個鎖固件。其中，鋼構件呈長條狀且相互平行排列，用以結合於建築物之鋼構的桁條或小樑上。L型角鋼設置於最外圍之該鋼構件上，並使兩側之L型角鋼的缺口彼此相對。T型角鋼設置於位於內側之該鋼構件上。鎖固件係分別穿設於L型角鋼與T型角鋼及位於L型角鋼與T型角鋼上方的墊片後，再鎖入一太陽能模組。
175	Form for a concrete wall structure	US3638382D	1969-12-22	US3638382A	1972-02-01	MERRILL RONALD E
A permanent wall form for construction of a concrete wall including expanded metal lath side members tied in spaced-apart relationship by wire truss members in place intermediate the metal laths. Channels on the lath receive the inserted truss members for secure assembly of the lath side members. The lath permits migration of the concrete therethrough for subsequent smooth finishing by troweling. Provision is made for the including of insulative strips on one side of the form prior to concrete pouring.
176	Reinforced stringer and method of manufacture thereof	US14139147	2013-12-23	US09440725B2	2016-09-13	Ignacio Outon Hernández; Yolanda Miguez Charines; Oscar Miguel Macías Jareño; Juan José Pastrana Bermejo; Antonio Torres Esteban
The present invention relates to a stringer, particularly to a stiffening and structural longitudinal element for skin of aircraft airfoil surfaces, characterized in that it incorporates two separate and independent reinforcement areas, one in the foot and the other at the end of the web (head) of the stringer, where the reinforcement areas are obtained by a widening of the section of the stringer, the widening being formed by a localized stack of reinforcing plies of composite material which are embedded within the stringer. The invention also relates to the method of manufacture and is particularly applicable to stringers having an L-shaped or T-shaped section.
177	REINFORCED STRINGER AND METHOD OF MANUFACTURE THEREOF	US14139147	2013-12-23	US20140186578A1	2014-07-03	Ignacio OUTON HERNÁNDEZ; Yolanda MIGUEZ CHARINES; Oscar Miguel MACÍAS JARENO; Juan José PASTRANA BERMEJO; Antonio TORRES ESTEBAN
The present invention relates to a stringer, particularly to a stiffening and structural longitudinal element for skin of aircraft airfoil surfaces, characterized in that it incorporates two separate and independent reinforcement areas, one in the foot and the other at the end of the web (head) of the stringer, where the reinforcement areas are obtained by a widening of the section of the stringer, the widening being formed by a localized stack of reinforcing plies of composite material which are embedded within the stringer. The invention also relates to the method of manufacture and is particularly applicable to stringers having an L-shaped or T-shaped section.
178	Composite and structure, particularly in the aerospace sector	US12915207	2010-10-29	US08403263B2	2013-03-26	Helmut Luettig
The present invention provides a composite, in particular in the field of aviation and aerospace, comprising an omega-stringer that comprises a comb portion, and a connecting member that is connected at one end to the comb portion of the omega-stringer and can be connected at its other end to a standard coupling member. The idea underlying the present invention consists in forming omega-stringers with a connection zone that, on the one hand, is coupled to the comb portion of the omega-stringer and therefore makes it possible to transfer comparatively high loads and, on the other hand, can be connected to a standard coupling member so as to utilize the advantages of standard coupling members of this type when connecting omega-stringers to other stringers, for example T-stringers or other omega-stringers.
179	Positioning, handling and assembling system for manufacture of aeronautical parts	US12387302	2009-04-30	US20100154186A1	2010-06-24	Jose Manuel Santos Gomez; Jose Manuel Menendez Martin; Antonio Duran Quiroga; Aquilino Garcia Garcia; Julian Sanchez Fernandez
The system has special application in the manufacture of aircraft wing covers (1) made of carbon fiber and the stringers (3) cured jointly with the wing cover during the polymerization in autoclave.The tool pieces (4) being used are defined by angular elements (5, 6) copying the geometry of the stringers (3). The shape of these stringers corresponds to the “T” section. The angular elements (5, 6) comprise, in their upper part, a pair of battlements (7) in order to be caught by part of the clamps (9) of a head (10) linked to a robot (11) of the spherical type with articulated arm with six axes.The angular elements (5, 6) are made of INVAR material and they are used to keep in position the stringers during the curing cycle in the autoclave.
180	COMPOSITE AND STRUCTURE, PARTICULARLY IN THE AEROSPACE SECTOR	US12915207	2010-10-29	US20110095130A1	2011-04-28	Helmut Luettig
The present invention provides a composite, in particular in the field of aviation and aerospace, comprising an omega-stringer that comprises a comb portion, and a connecting member that is connected at one end to the comb portion of the omega-stringer and can be connected at its other end to a standard coupling member. The idea underlying the present invention consists in forming omega-stringers with a connection zone that, on the one hand, is coupled to the comb portion of the omega-stringer and therefore makes it possible to transfer comparatively high loads and, on the other hand, can be connected to a standard coupling member so as to utilise the advantages of standard coupling members of this type when connecting omega-stringers to other stringers, for example T-stringers or other omega-stringers.

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