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公开(公告)号：US20090119694A1
公开(公告)日：2009-05-07
申请号：US11989486
申请日：2006-07-27
CPC分类号： H04L12/185 , H04H20/82 , H04H60/33 , H04L43/0876 , H04L67/22 , H04L69/329
摘要： The invention concerns a method for measuring a multicast stream audience, said multicast stream being capable of being replicated by collecting equipment towards user terminals subscribing to said multicast stream. Said method includes a step of transmitting, via at least one collecting equipment to a counting platform, and in accordance with a counting protocol, at least one counting message comprising at least one audience information concerning the replications of the multicast stream by said at least one collecting equipment to at least one user terminal.
摘要翻译： 本发明涉及一种用于测量多播流受众的方法，所述多播流能够通过向订阅所述多播流的用户终端收集设备进行复制。 所述方法包括通过至少一个收集设备向计数平台发送并根据计数协议的至少一个计数消息的步骤，所述至少一个计数消息包括至少一个关于所述至少一个组播流的复制的受众信息 将设备收集到至少一个用户终端。
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公开(公告)号：US20080289008A1
公开(公告)日：2008-11-20
申请号：US11884244
申请日：2006-02-15
IPC分类号： G06F21/20
CPC分类号： H04L63/08 , H04L12/185 , H04L63/0892
摘要： The invention relates to a method of controlling access to multicast IP flows. Following connection to a collection equipment by a user terminal, the method consists in: transmitting an access authorization request message from said collection equipment to an access control server; and, subsequently, upon successful verification of the user access right, transmitting an access authorization acceptance message comprising at least one multicast filter from the server to the collection equipment or, in the absence of a successful verification, transmitting an access refusal message from the server to the collection equipment in order to inhibit the connection of the user terminal. The invention is suitable for multicast broadcasting over an IP, Internet and/or corporate network.
摘要翻译： 本发明涉及一种控制对组播IP流的访问的方法。 在由用户终端连接到收集设备之后，该方法包括：从所述收集设备向接入控制服务器发送接入授权请求消息; 并且随后，在成功验证用户访问权限后，将包括至少一个多播过滤器的访问授权接受消息从服务器发送到收集设备，或者在没有成功验证的情况下，从服务器发送访问拒绝消息 以收集设备为禁止用户终端的连接。 本发明适用于通过IP，因特网和/或公司网络的组播广播。
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公开(公告)号：US20110020119A1
公开(公告)日：2011-01-27
申请号：US12673696
申请日：2008-06-12
申请人： Gilles Bourdon
发明人： Gilles Bourdon
IPC分类号： F01D25/28
CPC分类号： B64D29/06
摘要： The invention relates to a jet engine nacelle intended to equip an aircraft, comprising a forward air inlet section, a mid-section intended to surround a fan of the jet engine, and an aft section formed from at least first and second hath-shells rotatably mounted about an axis such that they can each be deployed between a working position in which the half-shells are drawn towards one another and a maintenance position in which the half-shells are spaced apart, at least the first half-shell (11) being equipped with a first follower element (19) in a region situated at a distance from the axis of rotation, the nacelle being equipped with a first fixed guide element (28), the first follower element (19) being designed to bear against a first guide element (28) which is fixed with respect to the jet engine during the rotation of the first half-shell (11). The first half-shell (11) is equipped with a second follower element (20), offset angularly from the first follower element (19) with respect to the axis of rotation of the first half-shell (11), designed to bear against a second guide element (29) during the rotation of the first half-shell (11).
摘要翻译： 本发明涉及一种用于装备飞行器的喷气发动机机舱，包括前进气进口部分，用于围绕喷气发动机的风扇的中间部分，以及由至少第一和第二壳体可旋转地形成的后部 安装在轴线周围，使得它们可以各自部署在半壳体彼此相对的工作位置和半壳体间隔开的维护位置，至少第一半壳体（11） 在位于距离旋转轴线一定距离的区域中配备有第一从动元件（19），所述机舱配备有第一固定引导元件（28），所述第一从动元件（19）设计成承受 第一引导元件（28），其在所述第一半壳（11）的旋转期间相对于所述喷气发动机固定。 第一半壳（11）配备有第二从动元件（20），其相对于第一半壳（11）的旋转轴线与第一从动元件（19）成角度地偏置，设计成抵抗 在第一半壳（11）旋转期间的第二引导元件（29）。
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公开(公告)号：US08333343B2
公开(公告)日：2012-12-18
申请号：US12674192
申请日：2008-06-12
申请人： Gilles Bourdon
发明人： Gilles Bourdon
CPC分类号： B64D29/08 , Y10T137/0536
摘要： The invention relates to a jet engine nacelle intended to equip an aircraft, comprising a forward air inlet section, a mid-section intended to surround a fan of the jet engine, and an aft section formed from at least first and second half-shells (9, 10) rotatably mounted about an axis (A) such that they can each be deployed between a working position in which the half-shells (9, 10) are drawn towards one another and a maintenance position in which the half-shells (9, 10) are spaced apart, the mid- and aft sections being connected to one another by a frame (12) which is fixed with respect to the jet engine, the first and second half-shells (9, 10) being equipped with positioning means (13) which in the working position cooperate with complementary positioning means (14) formed on the fixed frame (12). At least the first half-shell (10) is equipped with the locking means (20) which in the maintenance position cooperate with complementary locking means (16, 17) arranged on the fixed frame (12), so as to prevent the first half-shell (10) from moving translationally along its axis (A).
摘要翻译： 本发明涉及一种旨在装备飞行器的喷气发动机机舱，包括前进气进口部分，用于围绕喷气发动机的风扇的中间部分以及由至少第一和第二半壳形成的后部（ 9，10）围绕轴线（A）可旋转地安装，使得它们可以各自部署在半壳（9,10）彼此相对的工作位置和维持位置之间，半壳 9,10）间隔开，中间和后部通过相对于喷气发动机固定的框架（12）彼此连接，第一和第二半壳（9,10）装备有 定位装置（13）在工作位置与形成在固定框架（12）上的互补定位装置（14）配合。 至少第一半壳（10）配备有锁定装置（20），其在维护位置与布置在固定框架（12）上的互补锁定装置（16,17）配合，以防止前半部 - 壳（10）沿其轴线（A）平移运动。
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公开(公告)号：US20110272533A1
公开(公告)日：2011-11-10
申请号：US12674192
申请日：2008-06-12
申请人： Gilles Bourdon
发明人： Gilles Bourdon
CPC分类号： B64D29/08 , Y10T137/0536
摘要： The invention relates to a jet engine nacelle intended to equip an aircraft, comprising a forward air inlet section, a mid-section intended to surround a fan of the jet engine, and an aft section formed from at least first and second half-shells (9, 10) rotatably mounted about an axis (A) such that they can each be deployed between a working position in which the half-shells (9, 10) are drawn towards one another and a maintenance position in which the half-shells (9, 10) are spaced apart, the mid- and aft sections being connected to one another by a frame (12) which is fixed with respect to the jet engine, the first and second half-shells (9, 10) being equipped with positioning means (13) which in the working position cooperate with complementary positioning means (14) formed on the fixed frame (12). At least the first half-shell (10) is equipped with the locking means (20) which in the maintenance position cooperate with complementary locking means (16, 17) arranged on the fixed frame (12), so as to prevent the first half-shell (10) from moving translationally along its axis (A).
摘要翻译： 本发明涉及一种旨在装备飞行器的喷气发动机机舱，包括前进气进口部分，用于围绕喷气发动机的风扇的中间部分以及由至少第一和第二半壳形成的后部（ 9，10）围绕轴线（A）可旋转地安装，使得它们可以各自部署在半壳（9,10）彼此相对的工作位置和维持位置之间，半壳 9,10）间隔开，中间和后部通过相对于喷气发动机固定的框架（12）彼此连接，第一和第二半壳（9,10）装备有 定位装置（13）在工作位置与形成在固定框架（12）上的互补定位装置（14）配合。 至少第一半壳（10）配备有锁定装置（20），其在维护位置与布置在固定框架（12）上的互补锁定装置（16,17）配合，以防止前半部 - 壳（10）沿其轴线（A）平移运动。
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公开(公告)号：US08783614B2
公开(公告)日：2014-07-22
申请号：US12673696
申请日：2008-06-12
申请人： Gilles Bourdon
发明人： Gilles Bourdon
IPC分类号： B64D29/08
CPC分类号： B64D29/06
摘要： The invention relates to a jet engine nacelle intended to equip an aircraft, comprising a forward air inlet section, a mid-section intended to surround a fan of the jet engine, and an aft section formed from at least first and second hath-shells rotatably mounted about an axis such that they can each be deployed between a working position in which the half-shells are drawn towards one another and a maintenance position in which the half-shells are spaced apart, at least the first half-shell (11) being equipped with a first follower element (19) in a region situated at a distance from the axis of rotation, the nacelle being equipped with a first fixed guide element (28), the first follower element (19) being designed to bear against a first guide element (28) which is fixed with respect to the jet engine during the rotation of the first half-shell (11). The first half-shell (11) is equipped with a second follower element (20), offset angularly from the first follower element (19) with respect to the axis of rotation of the first half-shell (11), designed to bear against a second guide element (29) during the rotation of the first half-shell (11).
摘要翻译： 本发明涉及一种用于装备飞行器的喷气发动机机舱，包括前进气进口部分，用于围绕喷气发动机的风扇的中间部分，以及由至少第一和第二壳体可旋转地形成的后部 安装在轴线周围，使得它们可以各自部署在半壳体彼此相对的工作位置和半壳体间隔开的维护位置，至少第一半壳体（11） 在位于距离旋转轴线一定距离的区域中配备有第一从动元件（19），所述机舱配备有第一固定引导元件（28），所述第一从动元件（19）设计成承受 第一引导元件（28），其在所述第一半壳（11）的旋转期间相对于所述喷气发动机固定。 第一半壳（11）配备有第二从动元件（20），其相对于第一半壳（11）的旋转轴线与第一从动元件（19）成角度地偏置，设计成抵抗 在第一半壳（11）旋转期间的第二引导元件（29）。
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公开(公告)号：US08386777B2
公开(公告)日：2013-02-26
申请号：US11884244
申请日：2006-02-15
CPC分类号： H04L63/08 , H04L12/185 , H04L63/0892
摘要： The invention relates to a method of controlling access to multicast IP flows. Following connection to a collection equipment by a user terminal, the method consists in: transmitting an access authorization request message from said collection equipment to an access control server; and, subsequently, upon successful verification of the user access right, transmitting an access authorization acceptance message comprising at least one multicast filter from the server to the collection equipment or, in the absence of a successful verification, transmitting an access refusal message from the server to the collection equipment in order to inhibit the connection of the user terminal. The invention is suitable for multicast broadcasting over an IP, Internet and/or corporate network.
摘要翻译： 本发明涉及一种控制对组播IP流的访问的方法。 在由用户终端连接到收集设备之后，该方法包括：从所述收集设备向接入控制服务器发送接入授权请求消息; 并且随后，在成功验证用户访问权限后，将包括至少一个多播过滤器的访问授权接受消息从服务器发送到收集设备，或者在没有成功验证的情况下，从服务器发送访问拒绝消息 以收集设备为禁止用户终端的连接。 本发明适用于通过IP，因特网和/或公司网络的组播广播。
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