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1. 发明授权

US4526421A Multi-passenger aircraft seat having composite panel frame 失效
标题翻译：多用途飞机座椅具有复合面板框架
公开(公告)号：US4526421A
公开(公告)日：1985-07-02
申请号：US429340
申请日：1982-09-30
申请人： Edward J. Brennan , William A. Long , Rene J. Brunelle
发明人： Edward J. Brennan , William A. Long , Rene J. Brunelle
IPC分类号： A47C7/00 , B60N2/00 , B60N2/20 , B60N2/22 , B60N2/42 , B60N2/75 , B60N2/90 , B64D11/06 , A47C15/00
CPC分类号： B64D11/0638 , B64D11/06 , B64D11/064 , B64D11/0647 , B64D11/0696 , Y02T50/46 , Y10S108/901 , Y10S297/02 , Y10T428/236
摘要： Improved, lightweight multi-passenger aircraft seating unit utilizes an elongated, generally S-shaped, composite panel to provide the sole support for the seat cushions, the seat back and seat back tray table, the seat belt anchors and the armrests. Front legs and rear legs made of thin sheet metal can be attached directly to the panel by bolts passing through the panel. A downwardly projecting front portion of the panel and an upwardly projecting rear portion, in cooperation with channel-shaped members bonded to the panel's peripheral edges, enhance the rigidity of the panel. The unit provides cantilever support without the necessity for the front and rear tubular stretcher members and the fore and aft support members used in conventional seats. The composite panel has a honeycomb core and its top and bottom skin surfaces are formed of continuous layers of resin-impregnated fibrous material such as graphite fibers, with additional swatches of such material overlying and integrally bonded into the skin. The additional reinforcement material is laminated into regions of additional stress such as those where the legs, back, seat belt anchors and armrests are to be attached. The seat back is doubly curved to provide lumbar and shoulder support and good comfort with a thin constant thickness rear pad. The seat allows spacing between seat rows to be determined virtually solely by the dimensions of the occupants.
摘要翻译：改进的，轻便的多客机飞机座椅单元利用细长的大致S形复合面板来为座垫，座椅靠背和座椅靠背托盘台，座椅安全带锚和扶手提供唯一的支撑。由薄金属板制成的前腿和后腿可以通过穿过面板的螺栓直接连接到面板。面板的向下突出的前部和向上突出的后部与结合到面板的周边边缘的通道状构件配合，增强了面板的刚性。该单元提供悬臂支撑，而不需要前后管状担架构件和用于常规座椅中的前后支撑构件。复合面板具有蜂窝芯，其顶部和底部皮肤表面由连续的树脂浸渍的纤维材料层（例如石墨纤维）形成，其中附加的这种材料的样本覆盖并整体地粘合到皮肤中。附加的增强材料被层压到附加应力的区域中，例如将要连接腿，背，座椅安全带锚和扶手的区域。座椅靠背双重弯曲以提供腰部和肩部的支撑，并具有良好的舒适度，具有薄的恒定厚度后垫。座椅允许座椅排之间的间距几乎仅由居住者的尺寸确定。

2. 外观设计

USD267372S Multi-passenger aircraft seat 失效
公开(公告)号：USD267372S
公开(公告)日：1982-12-28
申请号：US135846
申请日：1980-03-31
申请人： William A. Long , Ward E. Fischer , Rene J. Brunelle
设计人： William A. Long , Ward E. Fischer , Rene J. Brunelle

3. 发明授权

US4375300A Framing system for aircraft passenger seat 失效
标题翻译：飞机乘客座椅构架系统
公开(公告)号：US4375300A
公开(公告)日：1983-03-01
申请号：US208955
申请日：1980-11-20
申请人： William A. Long , Ward E. Fischer , Rene J. Brunelle
发明人： William A. Long , Ward E. Fischer , Rene J. Brunelle
IPC分类号： B60N2/24 , B60N2/90 , B64D11/06 , A47C15/00
CPC分类号： B64D11/0648 , B60N2/242 , B64D11/06 , B64D11/0696
摘要： Improved framing system for a multi-passenger seat incorporates a generally inverted L-shaped rear leg whose shorter leg portion is joined to the rear stretcher tube at its free end and to a compression member at its point of intersection with its longer leg portion. The compression member and short leg portion form one side of a triangle which includes the front leg and a support member connecting the front and rear stretcher tubes. The longer leg portion forms one leg of a triangle which includes the compression member and a seat track covering member. The design provides greatly improved passenger leg room for close pitch seating arrangements.
摘要翻译：用于多乘客座椅的改进的框架系统包括大体上倒置的L形后腿，其较短的腿部部分在其自由端处连接到后拉伸管并且与其较长的腿部相交点处的压缩构件。压缩构件和短腿部分形成包括前腿的三角形的一侧和连接前后担架管的支撑构件。较长的腿部形成包括压缩构件和座椅轨道覆盖构件的三角形的一个腿。该设计提供了极大改善的乘客腿空间，用于紧凑座椅安排。

4. 发明授权

US4396175A Track fitting 失效
标题翻译：轨道配件
公开(公告)号：US4396175A
公开(公告)日：1983-08-02
申请号：US214392
申请日：1980-12-08
申请人： William A. Long , Ward E. Fischer , Rene J. Brunelle
发明人： William A. Long , Ward E. Fischer , Rene J. Brunelle
IPC分类号： B60N2/90 , B64D11/06 , A47B97/00
CPC分类号： B64D11/0696
摘要： An improved track fitting for anchoring an aircraft seat to a seat track has a threaded "anti-rattle" fastener for forcing a flanged top portion of a movement restricting shear pin against the top of the seat track to prevent rattle and wear due to aircraft vibrations. A pivoted lever which also functions as a cover for the fitting is mounted on the body of the fitting for lifting the shear pin against the force of a shear pin spring which normally urges the pin into locking engagement with one of the slots in a seat track. To prevent tampering by a passenger, the lever is rendered inoperable when the anti-rattle fastener is actuated. A leaf spring carried by the lever engages the body and prevents the lever from rattling due to vibration. The lever can lock the shear pin in its upper disengaged position as the seat fitting is lowered into the seat track and can then be released so that the shear pin will drop into one of the slots in the seat track automatically as the fitting is moved fore or aft.
摘要翻译：用于将飞行器座椅锚定到座椅轨道的改进的轨道配件具有螺纹“防拨”紧固件，用于迫使法兰的顶部部分将剪切销限制在座椅轨道的顶部，以防止由于飞行器振动引起的拨浪和磨损。还用作配件的盖的枢转杠杆安装在配件的主体上，用于提升剪切销以克服剪切销弹簧的力，该剪力销弹簧通常促使销与座椅轨道中的一个槽中的一个锁定接合。为了防止乘客的篡改，当防拨扣紧固件被致动时，杠杆变得不可操作。由杠杆承载的板簧接合主体并防止杠杆由于振动而发出咔嗒声。当座椅配件下降到座椅轨道中时，杠杆可以将剪切销锁定在其上部脱离位置，然后可以被释放，使得剪切销将随着配件向前移动而自动落入座椅轨道中的一个槽中或船尾。

5. 发明授权

US5890014A System for transparently identifying and matching an input/output profile to optimal input/output device parameters 失效
标题翻译：用于将输入/输出配置文件透明地识别和匹配到最佳输入/输出设备参数的系统
公开(公告)号：US5890014A
公开(公告)日：1999-03-30
申请号：US691018
申请日：1996-08-05
申请人： William A. Long
发明人： William A. Long
IPC分类号： G06F13/10
CPC分类号： G06F13/10
摘要： A system and method is provided for optimizing the data transfer performance between a host computer and a peripheral data storage device adapted to transfer data in accordance with an internal set of configurable, performance setting parameters which determine the device's data transfer performance. A device driver program evaluates the I/O request stream of application programs hosted by the computer, and identifies any patterns evident in the I/O request stream. Identified I/O request patterns are matched to a corresponding set of data storage device performance setting parameters, i.e., mode parameter pages, which have been predetermined as able to optimize the data transfer performance of a data storage device for the identified I/O pattern. The new performance setting parameters are written to the data storage device which is operated in accordance therewith, thus tuning the data storage device for an application's I/O request pattern. An I/O emulator and characterization program determines various optimized performance setting parameters for a particular data storage device issuing I/O requests in an arbitrary pattern, iteratively adjusting the performance setting parameters, and evaluating the data transfer performance resulting from each parameter setting alteration until an optimized data transfer rate is achieved for that particular pattern.
摘要翻译：提供了一种用于优化主计算机和外围数据存储设备之间的数据传输性能的系统和方法，适用于根据确定设备数据传输性能的可配置性能设置参数的内部集合传输数据。设备驱动程序评估由计算机托管的应用程序的I / O请求流，并识别I / O请求流中明显的任何模式。识别的I / O请求模式与已经预先确定的能够优化用于所识别的I / O模式的数据存储设备的数据传输性能的相应的数据存储设备性能设置参数集合（即，模式参数页面）相匹配。新的性能设置参数被写入依照其操作的数据存储设备，从而调整数据存储设备的应用的I / O请求模式。 I / O仿真器和表征程序确定用于以任意模式发出I / O请求的特定数据存储设备的各种优化的性能设置参数，迭代地调整性能设置参数，以及评估由每个参数设置改变导致的数据传输性能，直到为该特定模式实现了优化的数据传输速率。

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