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    • 2. 发明申请
    • AIRCRAFT RIB-SPAR JOINT
    • 飞机RIB-SPAR接头
    • US20120073137A1
    • 2012-03-29
    • US13238468
    • 2011-09-21
    • Richard BESTWICKScott GRANT
    • Richard BESTWICKScott GRANT
    • B21D53/92
    • B64C3/187B64C3/185B64F5/10Y10T29/49622Y10T29/4978Y10T29/53978Y10T408/55
    • A method of forming a rib-spar joint during assembly of an aircraft wing, the method comprising: providing a spar with a fixedly attached rib post, the rib post having a first coordination feature; providing a rib having a web with a first tooling feature; providing a tooling component having a second tooling feature for cooperating with the first tooling feature, a second coordination feature for cooperating with the first coordination feature, and a plurality of drill bushings; fixedly attaching the tooling component to the rib web by aligning the first and second tooling features; aligning the rib with the spar by aligning the first and second coordination features; drilling fastener holes in the rib and the rib post off the drill bushings of the tooling component; removing the tooling component from the rib web; and fastening the rib to the rib post using the fastener holes to form a rib-spar joint. The method may be applied to form front and/or rear rib-spar joints.
    • 一种在飞行器机翼的组装期间形成肋 - 翼梁接头的方法,所述方法包括:提供具有固定附接的肋柱的翼梁,所述肋柱具有第一协调特征; 提供具有带有第一工具特征的网的肋; 提供具有用于与所述第一工具特征配合的第二工具特征的模具部件,用于与所述第一协调特征配合的第二协调特征以及多个钻套筒; 通过对准第一和第二工具特征将工具组件固定地连接到肋腹板上; 通过对准第一和第二协调特征来对准肋骨与翼梁; 在所述肋和所述肋中钻紧所述紧固件孔,从所述工具部件的所述钻套中脱出; 从所述肋网移除所述加工部件; 并且使用所述紧固件孔将所述肋条紧固到所述肋柱上以形成肋 - 翼梁接头。 该方法可以应用于形成前肋和/或后肋骨接头。
    • 5. 发明授权
    • Aircraft rib-spar joint
    • 飞机肋骨接头
    • US08567066B2
    • 2013-10-29
    • US13238468
    • 2011-09-21
    • Richard BestwickScott Grant
    • Richard BestwickScott Grant
    • B21D53/88
    • B64C3/187B64C3/185B64F5/10Y10T29/49622Y10T29/4978Y10T29/53978Y10T408/55
    • A method of forming a rib-spar joint during assembly of an aircraft wing, the method comprising: providing a spar with a fixedly attached rib post, the rib post having a first coordination feature; providing a rib having a web with a first tooling feature; providing a tooling component having a second tooling feature for cooperating with the first tooling feature, a second coordination feature for cooperating with the first coordination feature, and a plurality of drill bushings; fixedly attaching the tooling component to the rib web by aligning the first and second tooling features; aligning the rib with the spar by aligning the first and second coordination features; drilling fastener holes in the rib and the rib post off the drill bushings of the tooling component; removing the tooling component from the rib web; and fastening the rib to the rib post using the fastener holes to form a rib-spar joint. The method may be applied to form front and/or rear rib-spar joints.
    • 一种在飞行器机翼的组装期间形成肋 - 翼梁接头的方法,所述方法包括:提供具有固定附接的肋柱的翼梁,所述肋柱具有第一协调特征; 提供具有带有第一工具特征的网的肋; 提供具有用于与所述第一工具特征配合的第二工具特征的模具部件,用于与所述第一协调特征配合的第二协调特征以及多个钻套筒; 通过对准第一和第二工具特征将工具组件固定地连接到肋腹板上; 通过对准第一和第二协调特征来对准肋骨与翼梁; 在所述肋和所述肋中钻紧所述紧固件孔,从所述工具部件的所述钻套中脱出; 从所述肋网移除所述加工部件; 并且使用所述紧固件孔将所述肋条紧固到所述肋柱上以形成肋 - 翼梁接头。 该方法可以应用于形成前肋和/或后肋骨接头。
    • 6. 发明申请
    • Antisense composition and method for treating cancer
    • 反义成分和治疗癌症的方法
    • US20050261249A1
    • 2005-11-24
    • US11077871
    • 2005-03-10
    • Patrick IversenHemant RoyRichard Bestwick
    • Patrick IversenHemant RoyRichard Bestwick
    • A61K48/00C12N15/113C12N15/85
    • A01K67/0276A01K2217/075A01K2227/105A01K2267/0331C12N15/113C12N15/8509C12N2310/11C12N2310/3145C12N2310/3233
    • A method and composition for of treating cancer, and in particular, for arresting the progression of a solid or primary cancer to a more invasive, metastatic state, are disclosed. The composition includes a substantially uncharged antisense compound (i) having a nuclease-resistant backbone, (ii) capable of uptake by target cancer cells in the subject, (iii) containing between 10-40 nucleotide bases, and (iv) having a base sequence effective to hybridize to a region of processed or preprocessed human SNAIL RNA transcript. The compound, when administered to the subject, is effective to form within target cancer cells in the subject, a base-paired heteroduplex structure composed of human SNAIL RNA transcript and the oligonucleotide compound, where this structure is characterized by a Tm of dissociation of at least 45° C. The compound is administered in an amount sufficient to inhibit SNAIL expression in target cancer cells, thereby to inhibit the progression of the patient's cancer to a more invasive, metastatic state. Also disclosed are methods for preventing the transdifferentiation of peritoneal mesothelial cells and failure of ultrafiltration in a patient undergoing peritoneal dialysis, by including the compound in the patient dialysis fluid.
    • 公开了用于治疗癌症的方法和组合物,特别是用于将固体或原发癌的进展阻止到更具侵袭性的转移状态。 组合物包括具有核酸酶抗性骨架的基本上不带电的反义化合物(i),(ii)能够被摄体中靶细胞摄取的能力,(iii)含有10-40个核苷酸碱基和(iv)具有碱基 有效地与经处理或预处理的人SNAIL RNA转录物区域杂交的序列。 该化合物当被施用于受试者时,在受试者的靶癌细胞内形成,由人SNAIL RNA转录物和寡核苷酸化合物组成的碱基配对的异源双链结构是有效的,其中该结构的特征在于解离的Tm 至少45℃。化合物以足以抑制靶癌细胞中SNAIL表达的量施用,从而抑制患者癌症进展到更具侵袭性的转移状态。 还公开了通过将化合物包括在患者透析液中来防止腹膜间皮细胞的转分化和经历腹膜透析的患者中的超滤失败的方法。