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1. 发明申请

US20210399403A1 ARTICULATED MECHANISM AND ARTICULATED AIMING SYSTEM COMPRISING THE MECHANISM 有权
公开(公告)号：US20210399403A1
公开(公告)日：2021-12-23
申请号：US17285662
申请日：2018-10-17
申请人： AIRBUS DEFENCE AND SPACE SA
发明人： Carlos CRESPO MENÉNDEZ , Alejandro GARCÉS DE MARCILLA RODRÍGUEZ
IPC分类号： H01Q1/12 , H01Q1/18 , H01Q3/08
摘要： An articulated mechanism is included in an articulated pointing system. The articulated mechanism includes first, second, and third spherical joints, and a first, second, and third lever. The first and second spherical joints are linked by the first lever. The first lever includes a first projecting portion. The first and third spherical joints are linked by the second lever, the second lever including a second projecting portion projecting in an opposite direction of the first projecting portion. The second and third spherical joints are linked by the third lever, such that the longitudinal axes of the first lever and of the second lever are perpendicular. The articulated pointing system includes a basement platform and a mobile platform joined by two articulated hinges. The hinges are moved by actuators. The articulated mechanism has the first lever attached to the mobile platform and the second lever attached to the basement platform.

2. 发明申请

US20200328134A1 HIGH-CONDUCTANCE THERMAL CONNECTOR 审中-公开
公开(公告)号：US20200328134A1
公开(公告)日：2020-10-15
申请号：US16957671
申请日：2017-12-29
申请人： AIRBUS DEFENCE AND SPACE SA
发明人： Felipe CÁCERES DEL VISO , Marc PERELLÓN MARSÁ , María José APARICIO ORDOBÁS , Carlos Roberto SAMARTÍN PULIÁN
IPC分类号： H01L23/373
摘要： A high conductance thermal link (1) includes a thermal conductive strap (2) having pyrolytic graphite layers arranged in stacks (5) and polyimide film (6) at least partially covering each stack (5). Adhesive material is between the pyrolytic graphite layers. The thermal conductive strap (2) has two opposite ends (4) and two end fittings (3, 3′) that house the corresponding ends (4) of the thermal conductive strap (2). An adhesive material is in the ends (4) of the thermal conductive strap (2) between the pyrolytic graphite layers and between the stacks (5) of pyrolytic graphite layers. At least one of the ends (4) of the thermal conductive strap (2) has a geometry including protrusions (7) separated by intermediate gaps (8).

3. 发明授权

US11521910B2 High-conductance thermal connector 有权
公开(公告)号：US11521910B2
公开(公告)日：2022-12-06
申请号：US16957671
申请日：2017-12-29
申请人： AIRBUS DEFENCE AND SPACE SA
发明人： Felipe Cáceres Del Viso , Marc Perellón Marsá , María José Aparicio Ordobás , Carlos Roberto Samartín Pulián
IPC分类号： B64G1/50 , H01L23/373
摘要： A high conductance thermal link (1) includes a thermal conductive strap (2) having pyrolytic graphite layers arranged in stacks (5) and polyimide film (6) at least partially covering each stack (5). Adhesive material is between the pyrolytic graphite layers. The thermal conductive strap (2) has two opposite ends (4) and two end fittings (3, 3′) that house the corresponding ends (4) of the thermal conductive strap (2). An adhesive material is in the ends (4) of the thermal conductive strap (2) between the pyrolytic graphite layers and between the stacks (5) of pyrolytic graphite layers. At least one of the ends (4) of the thermal conductive strap (2) has a geometry including protrusions (7) separated by intermediate gaps (8).

4. 发明授权

US10399692B2 Aircraft fuel system with heating of stored fuel 有权
公开(公告)号：US10399692B2
公开(公告)日：2019-09-03
申请号：US15101786
申请日：2014-11-27
申请人： Airbus Defence and Space GmbH , Airbus Defence and Space SA
发明人： Enrique Soriano , Sven Kopp , Winfried Lohmiller , Christian Thiele , Sergio Fernandez , Pablo Blazques
IPC分类号： B64D37/34 , B64D37/00 , F02C7/224 , B64D37/04
摘要： An aircraft fuel system comprises a fuselage tank and wing fuel tanks each connected to the fuselage fuel tank by a respective fuel line. A first fuel line connects the fuselage fuel tank to a collector fuel tank, which is connected by second fuel lines to aircraft engines in use of the system. Unspent fuel output from the aircraft engines is returned to the collector fuel tank via third fuel lines. A fuel line arrangement is arranged to draw fuel from, and return that fuel to, the wing fuel tanks. Fuel within the third fuel lines is thermally coupled to fuel within the fuel line arrangement by a heat exchanger. Heat energy within unspent fuel output from the aircraft engines is transferred to the wing fuel tanks, reducing the likelihood of fuel freezing within these tanks during extended flying in cold environments.

5. 发明申请

WO2022229546A1 SATELLITE RÉFLECTEUR ET ENSEMBLE SATELLITAIRE COMPRENANT UN TEL SATELLITE 审中-公开
公开(公告)号：WO2022229546A1
公开(公告)日：2022-11-03
申请号：PCT/FR2022/050762
申请日：2022-04-21
申请人： AIRBUS DEFENCE AND SPACE SAS , AIRBUS DEFENCE AND SPACE SA
发明人： CAVIGNAC, Axel , MONTESANO, Antonio
IPC分类号： B64G1/24 , B64G1/22 , B64G1/10 , B64G1/64 , H01Q1/28
摘要： L'invention concerne un satellite réflecteur (1) comprenant au moins une surface de réflexion (11) incurvée, caractérisé par le fait qu'il comprend au moins une structure porteuse (10) reliée à au moins quatre systèmes de positionnement et d'orientation (12) du satellite réflecteur pour réaliser un contrôle d'attitude et d'orbite, lesdits systèmes de positionnement et d'orientation comprenant au moins un système propulseur, lesdits systèmes de positionnement et d'orientation étant synchronisés et disposés de façon à permettre une orientation du satellite réflecteur selon au moins deux axes de rotation. Il est également décrit un ensemble satellitaire comprenant un satellite source et un satellite réflecteur.

6. 发明申请

WO2019129896A1 CONECTOR TÉRMICO DE ALTA CONDUCTANCIA 审中-公开
公开(公告)号：WO2019129896A1
公开(公告)日：2019-07-04
申请号：PCT/ES2017/070866
申请日：2017-12-29
申请人： AIRBUS DEFENCE AND SPACE SA
发明人： CÁCERES DEL VISO, Felipe , PERELLÓN MARSÁ, Marc , APARICIO ORDOBÁS, María José , SAMARTÍN PULIÁN, Carlos Roberto
IPC分类号： B64G1/50 , F28F21/02
CPC分类号： B64G1/50 , C09K5/14 , H01L23/367 , H01L23/373 , H01L23/3736 , H01L23/3737
摘要： Conector térmico (1) de alta conductancia, que comprende : -una banda conductora térmica (2) que comprende capas de grafito pirolítico dispuestas en pilas (5) y película de poliimida (6) que cubre al menos parcialmente cada pila (5), con material adhesivo entre las capas de grafito pirolítico, teniendo la banda conductora térmica (2) dos extremos (4) opuestos, y - dos terminales extremos (3, 3') que alojan los extremos (4) correspondientes de la banda conductora térmica (2), en el que en los extremos (4) de la banda conductora térmica (2) hay un material adhesivo entre las capas de grafito pirolítico y entre las pilas (5) de capas de grafito pirolítico, y al menos uno de los extremos (4) de la banda conductora térmica (2) tiene una geometría que comprende varios salientes (7) separados por espacios intermedios (8).

7. 发明专利

FR3122410A1 Satellite réflecteur et ensemble satellitaire comprenant un tel satellite 未知
公开(公告)号：FR3122410A1
公开(公告)日：2022-11-04
申请号：FR2104584
申请日：2021-04-30
申请人： AIRBUS DEFENCE & SPACE SAS , AIRBUS DEFENCE AND SPACE SA
发明人： CAVIGNAC AXEL , MONTESANO ANTONIO
IPC分类号： B64G1/10 , B64G1/22 , B64G1/24 , B64G1/28 , H01Q1/28 , H01Q15/14 , H01Q19/19
摘要： L’invention concerne un satellite réflecteur (1) comprenant au moins une surface de réflexion (11) incurvée, caractérisé par le fait qu’il comprend au moins une structure porteuse (10) reliée à au moins quatre systèmes de positionnement et d’orientation (12) du satellite réflecteur pour réaliser un contrôle d’attitude et d’orbite, lesdits systèmes de positionnement et d’orientation comprenant au moins un système propulseur, lesdits systèmes de positionnement et d’orientation étant synchronisés et disposés de façon à permettre une orientation du satellite réflecteur selon au moins deux axes de rotation. Il est également décrit un ensemble satellitaire comprenant un satellite source et un satellite réflecteur. Figure de l’abrégé : Figure 1

8. 发明专利

TR201910443T4 Modüler uyarlanabilir barınak mimarisi. 未知
公开(公告)号：TR201910443T4
公开(公告)日：2019-08-21
申请号：TR201910443
申请日：2014-01-23
申请人： AIRBUS DEFENCE AND SPACE SA
发明人： JUAN MANUEL ROS GARCIA , JAVIER CAMACHO DIEZ , LUIS CASILLAS GAMBOA , CARLOS MIGUEL IGLESIAS SANZ
IPC分类号： E04H15/02 , E04H15/56
摘要： İçinde zeminin, her bir çerçevenin eliptik destekleme kısmının eğriliği kullanılarak veya çerçevelerin geri geçilebilir destekleme parçaları kullanılarak yerden yükseltildiği bir düz zemin çözümü sağlarken polimer veya tekstil kaplama levhaları tarafından oluşturulan kabuk ile bir panel bazlı iç zemin plağını desteklemek amacıyla metal veya kompozit materyallerden yapılmış çapraz düzenlenen ovoid çerçevelerin ve aynı materyalden yapılmış düz çerçevelerin çiftleri tarafından oluşturulan ardışık yapısal modüllerin mekanik olarak mafsallı montajını içeren, esnek bir şekilde arttırılabilen ve genişletilebilen bir oval kesite sahip olan barınağın yapısı ile karakterize edilen bir sosyal acil durumlara yönelik modüler uyarlanabilir barınak mimarisi vardır. Sonuç, araziye ve kullanım gereksinimlerine uyacak şekilde uyarlanabilen, stabil, güçlü ve çevre dostu olan ve herhangi bir ilave işlem gerektirmeksizin ve bölgeye özgü bir bitirişe olanak vererek herhangi bir konumda sökülmüş parçalar halinde taşınabilen ve hızlışekilde monte edilebilen bir kendinden gerilme sağlayan geometriye sahip bir modüler sığınaktır.

9. 发明专利

CA3086811A1 HIGH CONDUCTANCE THERMAL LINK 未知
公开(公告)号：CA3086811A1
公开(公告)日：2019-07-04
申请号：CA3086811
申请日：2017-12-29
申请人： AIRBUS DEFENCE AND SPACE SA
发明人： CACERES DEL VISO FELIPE , PERELLON MARSA MARC , APARICIO ORDOBAS MARIA JOSE , SAMARTIN PULIAN CARLOS ROBERTO
IPC分类号： B64G1/50 , F28F21/02
摘要： A high-conductance thermal connector (1) comprises: - a heat-conducting band (2) comprising pyrolitic graphite layers arranged in stacks (5), each stack (5) being at least partially covered by a polyimide layer (6), an adhesive material being arranged between the pyrolitic graphite layers and the heat-conducting band (2) having two opposite ends (4); and - two end terminals (3, 3') in which the corresponding ends (4) of the heat-conducting band (2) are received, an adhesive material being arranged at the ends (4) of the heat-conducting band (2) between the pyrolytic graphite layers and between the stacks (5) of pyrolytic graphite layers, and at least one of the ends (4) of the heat-conducting strip (2) has a geometry with multiple projections (7) separated by intermediate gaps (8).

10. 发明专利

ES2628599T3 Util de guiado de la broca de un aparato de taladrado y método de efectuar taladros 未知
公开(公告)号：ES2628599T3
公开(公告)日：2017-08-03
申请号：ES12197166
申请日：2012-12-14
申请人： AIRBUS DEFENCE AND SPACE SA
发明人： MARTINEZ QUINTERO JAVIER
IPC分类号： B23B49/02
摘要： Útil (11) de guiado de la broca de un aparato de taladrado sobre una superficie de trabajo para que se sitúe perpendicularmente a ella que comprende un cuerpo (13) con un orificio (15) para el paso de la broca y una base (14) de la que sobresalen al menos tres pies (19) de apoyo en dicha superficie de trabajo, los pies (19) configurados con agujeros interiores (21) con una boca de salida en sus extremos, y el útil (11) de guiado que comprende también: -una canalización de gas a presión hasta dichos pies (19), y -un dispositivo neumático (31) que suministra gas a presión conectado a la canalización de gas a presión, caracterizado por que dicho dispositivo neumático (31) incluye medios para activar una señal indicativa de un posicionamiento correcto del útil (11) para efectuar un taladro cuando, estando activado el suministro de gas a presión al útil (11), se produce un taponamiento simultáneo de la salida de gas por dichos pies (19) al entrar en contacto todos ellos con dicha superficie de trabajo, donde dicho dispositivo neumático (31) comprende un circuito de suministro de gas a presión, con una fuente de gas a presión (33) y una válvula de regulación (35), y un circuito paralelo de accionamiento de un emisor (37) de dicha señal controlado por una válvula biestable de presión (39) conectada a la fuente de gas a presión (33) y al circuito de suministro de gas, y donde la canalización de gas a presión comprende un conducto (25) conectado en su entrada (26) con dicho circuito de suministro de gas a presión y una cámara de distribución del gas (27) conectada a los orificios (21) de los pies (19) delimitada entre la base (14) y una pieza adicional (17) unida de manera estanca a ella y al cuerpo (13).

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