专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明申请

US20120025009A1 AIRCRAFT WITH SEGMENTED DEPLOYABLE CONTROL SURFACES 有权
标题翻译：具有可分配控制表面的飞机
公开(公告)号：US20120025009A1
公开(公告)日：2012-02-02
申请号：US12843921
申请日：2010-07-27
申请人： Chris E. Geswender , Craig O. Shott
发明人： Chris E. Geswender , Craig O. Shott
IPC分类号： F42B10/14
CPC分类号： F42B10/16
摘要： An aircraft, such as a missile, has control surfaces that have segments that are hinged together. The control surfaces deploy from a closed position, for example with the segments folded against a fuselage, so as to allow for launching from a launch tube. Once the aircraft is launched the control surfaces deploy from the closed position to an open position, with the segments opening up farther from the body or fuselage. In the open position or deployed state the segments may be substantially planar. Locks of the control surfaces may be used to lock the segments in place in the open position. The locks may include hollow sleeves that slide over the control surface segments. The sleeves and the segments may include a protrusions and depressions that engage each other to hold the segments in the open configuration.
摘要翻译：诸如导弹的飞机具有具有铰接在一起的段的控制表面。控制表面从关闭位置展开，例如，将部分折叠在机身上，以允许从发射管发射。一旦飞机启动，控制表面将从关闭位置部署到打开位置，从而使部件从主体或机身开放得更远。在打开位置或展开状态下，段可以是大致平面的。可以使用控制表面的锁将锁定在打开位置的位置。锁可以包括在控制表面段上滑动的空心套筒。套筒和节段可以包括彼此接合以将段保持在打开构型中的突起和凹陷。

2. 发明申请

US20120199691A1 PROJECTILE THAT INCLUDES AS NEEDED PRESSURE-RELIEVING WRAP-AROUND TAIL FINS 有权
标题翻译：包括需要压力消除缠绕尾灯的项目
公开(公告)号：US20120199691A1
公开(公告)日：2012-08-09
申请号：US12789068
申请日：2010-05-27
申请人： Chris E. Geswender , Mark E. Elkanick , Craig O. Shott
发明人： Chris E. Geswender , Mark E. Elkanick , Craig O. Shott
IPC分类号： F42B15/01
CPC分类号： F42B10/16 , F42B10/20 , F42B10/38
摘要： Some embodiments pertain to a projectile that includes a casing and a plurality of fins which are secured to the casing. Each of the fins is movable between a stowed position and a deployed position. The fins are typically in the stowed position during storage and launch, and move to the deployed position as soon as possible after launch. Each fin includes a first foil that has a first set of openings and a second foil that includes a second set of openings. The first sets of openings in the first foils are aligned with the second sets of openings in the second foils when each of the fins is in the stowed position. The first sets of openings in the first foils are not aligned with the second sets of openings in the second foils when each of the fins is in the deployed position.
摘要翻译：一些实施例涉及一种弹射器，其包括壳体和固定到壳体的多个翅片。每个翅片可在收起位置和展开位置之间移动。散热片通常在储存和发射期间处于收起位置，并且在发射后尽快移动到展开位置。每个翅片包括具有第一组开口的第一箔片和包括第二组开口的第二箔片。当每个翅片处于收起位置时，第一箔中的第一组开口与第二箔中的第二组开口对准。当每个翅片处于展开位置时，第一箔中的第一组开口不与第二箔中的第二组开口对齐。

3. 发明授权

US08294072B2 Projectile that includes as needed pressure-relieving wrap-around tail fins 有权
标题翻译：弹丸包括需要的减压缠绕尾翼
公开(公告)号：US08294072B2
公开(公告)日：2012-10-23
申请号：US12789068
申请日：2010-05-27
申请人： Chris E. Geswender , Mark E. Elkanick , Craig O. Shott
发明人： Chris E. Geswender , Mark E. Elkanick , Craig O. Shott
IPC分类号： F42B15/00
CPC分类号： F42B10/16 , F42B10/20 , F42B10/38
摘要： Some embodiments pertain to a projectile that includes a casing and a plurality of fins which are secured to the casing. Each of the fins is movable between a stowed position and a deployed position. The fins are typically in the stowed position during storage and launch, and move to the deployed position as soon as possible after launch. Each fin includes a first foil that has a first set of openings and a second foil that includes a second set of openings. The first sets of openings in the first foils are aligned with the second sets of openings in the second foils when each of the fins is in the stowed position. The first sets of openings in the first foils are not aligned with the second sets of openings in the second foils when each of the fins is in the deployed position.
摘要翻译：一些实施例涉及一种弹射器，其包括壳体和固定到壳体的多个翅片。每个翅片可在收起位置和展开位置之间移动。散热片通常在储存和发射期间处于收起位置，并且在发射后尽快移动到展开位置。每个翅片包括具有第一组开口的第一箔片和包括第二组开口的第二箔片。当每个翅片处于收起位置时，第一箔中的第一组开口与第二箔中的第二组开口对准。当每个翅片处于展开位置时，第一箔中的第一组开口不与第二箔中的第二组开口对齐。

4. 发明授权

US08274025B2 Aircraft with segmented deployable control surfaces 有权
标题翻译：具有分段可部署控制面的飞机
公开(公告)号：US08274025B2
公开(公告)日：2012-09-25
申请号：US12843921
申请日：2010-07-27
申请人： Chris E. Geswender , Craig O. Shott
发明人： Chris E. Geswender , Craig O. Shott
IPC分类号： F42B15/01
CPC分类号： F42B10/16
摘要： An aircraft, such as a missile, has control surfaces that have segments that are hinged together. The control surfaces deploy from a closed position, for example with the segments folded against a fuselage, so as to allow for launching from a launch tube. Once the aircraft is launched the control surfaces deploy from the closed position to an open position, with the segments opening up farther from the body or fuselage. In the open position or deployed state the segments may be substantially planar. Locks of the control surfaces may be used to lock the segments in place in the open position. The locks may include hollow sleeves that slide over the control surface segments. The sleeves and the segments may include a protrusions and depressions that engage each other to hold the segments in the open configuration.
摘要翻译：诸如导弹的飞机具有具有铰接在一起的段的控制表面。控制表面从关闭位置展开，例如，将部分折叠在机身上，以允许从发射管发射。一旦飞机启动，控制表面将从关闭位置部署到打开位置，从而使部件从主体或机身开放得更远。在打开位置或展开状态下，段可以是大致平面的。可以使用控制表面的锁将锁定在打开位置的位置。锁可以包括在控制表面段上滑动的空心套筒。套筒和节段可以包括彼此接合以将段保持在打开构型中的突起和凹陷。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式