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公开(公告)号：US08104711B2
公开(公告)日：2012-01-31
申请号：US11997720
申请日：2006-08-04
Applicant: Ian Bennett , Richard C. Lang , Robert A. Menezes
Inventor： Ian Bennett , Richard C. Lang , Robert A. Menezes
Abstract: An auxiliary actuator (49) comprises a two stage telescopic hydraulic unit comprising first (59, 63) and second (56, 50) stage piston and cylinder actuators operating coaxially within an outer casing (50). A respective actuator is connected to a respective one of the strut (1) and bogie beam (4). The second stage actuator (56, 60) serves to control the tilt position of the bogie beam (4) relative to the strut (1). The second stage actuator (56. 60), when in the retracted position with the first stage actuator (59, 63) in the extended position, limits the length ol the auxiliary actuator (9) between its connections (62,67) to the strut (1) and bogie beam (4), so as to assume a predetermined intermediate length in which the bogie beam (4) is restrained to tilt about the auxiliary pivot (14) and thereby lengthens the landing gear during take-off.
Abstract translation: 辅助致动器（49）包括两级伸缩液压单元，其包括在外壳（50）内同轴运行的第一（59,63）和第二（56,50）级的活塞和气缸致动器。 相应的致动器连接到支柱（1）和转向架梁（4）中的相应的一个。 第二级致动器（56,60）用于控制转向架（4）相对于支柱（1）的倾斜位置。 当处于处于延伸位置的第一级致动器（59,63）的缩回位置时，第二级致动器（56.60）将辅助致动器（9）在其连接（62,67）之间的长度限制到 支柱（1）和转向架梁（4），以便呈现预定的中间长度，其中转向架梁（4）被限制在辅助枢轴（14）周围倾斜，从而在起飞期间延长起落架。
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公开(公告)号：US20100288878A1
公开(公告)日：2010-11-18
申请号：US12682529
申请日：2008-10-13
Applicant: Ian Bennett
Inventor： Ian Bennett
CPC classification number: B64C25/34 , B64C25/58 , B64D2045/008 , F16F9/3264
Abstract: A landing gear for an aircraft includes a shock absorber strut (1) with upper and lower telescoping portions (2, 3), the upper portion (2) being connectable to the airframe of the aircraft. An arm (4) extends fore and aft relative to the aircraft and carrying a landing wheel, (7, 71), and pivotally connects by a main pivot (5) to the lower portion (3) of the shock absorber strut. A load reacting unit (9) connects between the arm (4) and the shock absorber strut (1) for reacting to load applied between the arm and shock absorber strut on landing. An indicator (60) monitors the load applied to the load reacting unit (9) on landing. The load reacting unit (9) may be connected between a forward end of the arm (4) and the upper portion (2) of the shock absorber strut to make the gear act as a semi-levered landing gear. Alternatively, the load reacting unit (9) may be connected between the arm (4) and the lower portion (3) of the shock absorber strut to act as a pitch trimmer. The arm (4) may include a bogie beam with fore and aft landing wheels (7, 71) with the main pivot (5) therebetween. The load reacting unit (9) preferably has a fluid pressure unit and the indicator (60) includes a mechanical indicator that operates at a predetermined pressure threshold.
Abstract translation: 用于飞机的起落架包括具有上部和下部伸缩部分（2,3）的减震器支柱（1），上部部分（2）可连接到飞行器的机身。 臂（4）相对于飞行器前后延伸，并且承载着陆车轮（7,71），并且通过主枢轴（5）枢转地连接到减震器支柱的下部（3）。 负载反应单元（9）连接在臂（4）和减震器支柱（1）之间，用于在着陆时在臂和减震器支柱之间施加负载作用。 指示器（60）监视在着陆时施加到负载反应单元（9）的负载。 负载反应单元（9）可以连接在臂（4）的前端和减震器支柱的上部（2）之间，以使齿轮作为半起落架起落架。 或者，负载反应单元（9）可以连接在臂（4）和减震器支柱的下部（3）之间，用作俯仰修剪器。 臂（4）可以包括转向架梁，前转和后升降轮（7,71）与主枢轴（5）在其间。 负载反应单元（9）优选地具有流体压力单元，并且指示器（60）包括在预定压力阈值下操作的机械指示器。
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公开(公告)号：US07725321B2
公开(公告)日：2010-05-25
申请号：US12144492
申请日：2008-06-23
Applicant: Ian Bennett
Inventor： Ian Bennett
CPC classification number: G06F17/27 , G06F17/2715 , G06F17/2775 , G06F17/2785 , G06F17/2809 , G06F17/3043 , G06F17/30654 , G06F17/30684 , G09B5/04 , G09B7/00 , G09B7/02 , G09B19/06 , G10L15/142 , G10L15/18 , G10L15/1815 , G10L15/183 , G10L15/22 , G10L15/285 , G10L15/30 , G10L2015/223 , H04M2250/74
Abstract: An intelligent query system for processing voiced-based queries is disclosed, which uses a combination of both statistical and semantic based processing to identify the question posed by the user by understanding the meaning of the user's utterance. Based on identifying the meaning of the utterance, the system selects a single answer that best matches the user's query. The answer that is paired to this single question is then retrieved and presented to the user. The system, as implemented, accepts environmental variables selected by the user and is scalable to provide answers to a variety and quantity of user-initiated queries.
Abstract translation: 公开了一种用于处理基于浊音的查询的智能查询系统，其使用基于统计和语义的处理的组合来通过理解用户的话语的含义来识别用户构成的问题。 基于确定话语的含义，系统选择与用户查询最匹配的单个答案。 然后检索与该单个问题配对的答案并将其呈现给用户。 实施的系统接受用户选择的环境变量，并且是可扩展的，以提供对用户发起的查询的各种和数量的答案。
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公开(公告)号：US20100085195A1
公开(公告)日：2010-04-08
申请号：US12596802
申请日：2008-04-24
Applicant: Steven Ian Bennett
Inventor： Steven Ian Bennett
CPC classification number: G08B29/10 , H04R29/007
Abstract: A method of monitoring an alarm system comprises transmitting a sound alert signal, receiving the transmitted sound alert signal, comparing the received sound alert signal with a reference signal having parameters dependent upon equivalent parameters of the transmitted sound alert signal, and outputting a signal indicating whether or not the equivalent parameters of the received sound alert signal have a predetermined relationship with said parameters of the transmitted sound alert signal.
Abstract translation: 监测报警系统的方法包括发送声音报警信号，接收发送的声音报警信号，将接收的声音报警信号与具有取决于发送的声音报警信号的等效参数的参数的参考信号进行比较，并输出指示是否 或者不是所接收的声音警报信号的等效参数与所发送的声音警报信号的所述参数具有预定的关系。
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公开(公告)号：US20090198282A1
公开(公告)日：2009-08-06
申请号：US12364487
申请日：2009-02-02
Applicant: Louis Fielding , Ian Bennett , Colin Cahill , Pat Arensdorf , Ralph Crisostomo , Todd Alamin
Inventor： Louis Fielding , Ian Bennett , Colin Cahill , Pat Arensdorf , Ralph Crisostomo , Todd Alamin
IPC: A61B17/88
CPC classification number: A61B17/7062
Abstract: A spinal implant system for restricting flexion of a spine includes an elongate band proportioned to engage at least two spinous processes. During use, the band is positioned engaging the spinous processes at a spinal segment of interest, where it restricts flexion at the segment. The length and tension of the band may be adjustable following to implantation using percutaneous or transcutaneous means.
Abstract translation: 用于限制脊柱弯曲的脊柱植入系统包括成比例的细长带以接合至少两个棘突。 在使用期间，带被定位成与感兴趣的脊髓部分处的棘突接合，其中它限制了该部分的屈曲。 在使用经皮或经皮手段进行植入之后，带的长度和张力可以是可调节的。
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Patent Agency Ranking
公开(公告)号：US20090082820A1
公开(公告)日：2009-03-26
申请号：US12262877
申请日：2008-10-31
Applicant: Louie Fielding , Ian Bennett , Colin Cahill , Pat Arensdorf , Ralph Crisostomo , Todd Alamin
Inventor： Louie Fielding , Ian Bennett , Colin Cahill , Pat Arensdorf , Ralph Crisostomo , Todd Alamin
IPC: A61B17/04
CPC classification number: A61B17/7062
Abstract: A spinal implant system for restricting flexion of a spine includes an elongate band proportioned to engage at least two spinous processes. During use, the band is positioned engaging the spinous processes at a spinal segment of interest, where it restricts flexion at the segment. The length and tension of the band may be adjustable following to implantation using percutaneous or transcutaneous means.
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17.发明授权Landing gear strut damper, and landing gear with independent struts comprising same 失效起落架支柱阻尼器和具有独立支柱的起落架组成公开(公告)号：US07426983B2
公开(公告)日：2008-09-23
申请号：US10541948
申请日：2003-12-29
Applicant: Dominique Ducos , Jean-François Locufier , Ian Bennett , David Smart
Inventor： Dominique Ducos , Jean-François Locufier , Ian Bennett , David Smart
CPC classification number: B64C25/58 , B64C25/60 , B64C2025/008 , B64C2025/125
Abstract: A damper for an airplane landing gear leg comprises a main strut (11) and a rod piston (13) co-operating with the strut (11) to define a main chamber (15) and annular chamber (16) for hydraulic fluid, and presenting internally two adjacent chambers (19, 20) that are isolated from each other by a separator piston (21). The damper (10) further comprises a first secondary strut (26) telescopically Slidable on the above-mentioned rod piston (13), and a second secondary strut (37) telescopically slidable on the other end of the first secondary strut (26). The two second annular chambers (31, 40) as defined in this way are respectively connected to associated control circuits thus enabling the total length of the damper to be shortened or lengthened respectively for the purpose of causing the landing gear to contract or to be extended.
Abstract translation: 用于飞机起落架的减震器包括与支柱（11）配合的主支柱（11）和杆活塞（13），以限定用于液压流体的主室（15）和环形室（16），以及 在内部呈现通过分离器活塞（21）彼此隔离的两个相邻的室（19,20）。 阻尼器（10）还包括在上述杆式活塞（13）上可伸缩地滑动的第一辅助支柱（26）和在第一辅助支柱（26）的另一端可伸缩滑动的第二辅助支柱（37）。 以这种方式定义的两个第二环形腔室（31,40）分别连接到相关联的控制回路，从而能够使阻尼器的总长度分别缩短或延长，以使起落架收缩或延伸 。
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公开(公告)号：US20080052077A1
公开(公告)日：2008-02-28
申请号：US11932023
申请日：2007-10-31
Applicant: Ian Bennett , Bandi Babu , Kishor Morkhandikar , Pallaki Gururaj
Inventor： Ian Bennett , Bandi Babu , Kishor Morkhandikar , Pallaki Gururaj
IPC: G10L15/00
CPC classification number: G06F16/24522 , G06F17/289 , G10L15/005 , G10L15/142 , G10L15/18 , G10L15/183 , G10L15/22 , G10L15/30 , G10L17/22 , Y10S707/99935
Abstract: A speech recognition system includes distributed processing across a client and server for recognizing a spoken query by a user. A number of different speech models for different natural languages are used to support and detect a natural language spoken by a user. In some implementations an interactive electronic agent responds in the user's native language to facilitate an real-time, human like dialogue.
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19.发明申请公开(公告)号：US20060163427A1
公开(公告)日：2006-07-27
申请号：US10541948
申请日：2003-12-29
Applicant: Dominique Ducos , Ian Bennett , David Smart
Inventor： Dominique Ducos , Ian Bennett , David Smart
IPC: B64C25/58
CPC classification number: B64C25/58 , B64C25/60 , B64C2025/008 , B64C2025/125
Abstract: A damper for an airplane landing gear leg comprises a main strut (11) and a rod piston (13) co-operating with the strut (11) to define a main chamber (15) and annular chamber (16) for hydraulic fluid, and presenting internally two adjacent chambers (19, 20) that are isolated from each other by a separator piston (21). The damper (10) further comprises a first secondary strut (26) telescopically slidable on the above-mentioned rod piston (13), and a second secondary strut (37) telescopically slidable on the other end of the first secondary strut (26). The two second annular chambers (31, 40) as defined in this way are respectively connected to associated control circuits thus enabling the total length of the damper to be shortened or lengthened respectively for the purpose of causing the landing gear to contract or to be extended.
Abstract translation: 用于飞机起落架的减震器包括与支柱（11）配合的主支柱（11）和杆活塞（13），以限定用于液压流体的主室（15）和环形室（16），以及 在内部呈现通过分离器活塞（21）彼此隔离的两个相邻的室（19,20）。 阻尼器（10）还包括可在上述杆式活塞（13）上可伸缩滑动的第一辅助支柱（26）和在第一辅助支柱（26）的另一端可伸缩滑动的第二辅助支柱（37）。 以这种方式定义的两个第二环形腔室（31,40）分别连接到相关联的控制回路，从而能够使阻尼器的总长度分别缩短或延长，以使起落架收缩或延伸 。
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公开(公告)号：US20050080625A1
公开(公告)日：2005-04-14
申请号：US10684357
申请日：2003-10-10
Applicant: Ian Bennett , Bandi Babu , Kishor Morkhandikar , Pallaki Gururaj
Inventor： Ian Bennett , Bandi Babu , Kishor Morkhandikar , Pallaki Gururaj
CPC classification number: G10L17/22 , G06F17/289 , G06F17/3043 , G10L15/005 , G10L15/142 , G10L15/18 , G10L15/183 , G10L15/22 , G10L15/30 , Y10S707/99935
Abstract: A real-time system incorporating speech recognition and linguistic processing for recognizing a spoken query by a user and distributed between client and server, is disclosed. The system accepts user's queries in the form of speech at the client where minimal processing extracts a sufficient number of acoustic speech vectors representing the utterance. These vectors are sent via a communications channel to the server where additional acoustic vectors are derived. Using Hidden Markov Models (HMMs), and appropriate grammars and dictionaries conditioned by the selections made by the user, the speech representing the user's query is fully decoded into text (or some other suitable form) at the server. This text corresponding to the user's query is then simultaneously sent to a natural language engine and a database processor where optimized SQL statements are constructed for a full-text search from a database for a recordset of several stored questions that best matches the user's query. Further processing in the natural language engine narrows the search to a single stored question. The answer corresponding to this single stored question is next retrieved from the file path and sent to the client in compressed form. At the client, the answer to the user's query is articulated to the user using a text-to-speech engine in his or her native natural language. The system requires no training and can operate in several natural languages.
Abstract translation: 公开了一种包含语音识别和语言处理的实时系统，用于识别由用户进行的口语查询并分发在客户端与服务器之间。 该系统以客户端的语音形式接受用户的查询，其中最小处理提取足够数量的表示话语的声学语音向量。 这些向量经由通信信道被发送到服务器，其中导出附加的声向量。 使用隐马尔可夫模型（HMM），以及由用户做出的选择所限制的适当的语法和词典，表示用户查询的语音在服务器处被完全解码为文本（或其他合适的形式）。 然后将与用户查询相对应的文本同时发送到自然语言引擎和数据库处理器，其中为数据库构建优化的SQL语句，用于针对与用户查询最匹配的多个存储问题的记录集的全文搜索。 自然语言引擎中的进一步处理将搜索缩小到单个存储的问题。 对应于该单个存储问题的答案接下来从文件路径中检索并以压缩形式发送给客户端。 在客户端，使用他或她的母语自然语言的文本到语音引擎向用户阐述用户查询的答案。 该系统不需要培训，可以使用多种自然语言进行操作。
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