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1. 发明授权

US5783302A Thermoplastic elastomers 失效
标题翻译：热塑性弹性体
公开(公告)号：US5783302A
公开(公告)日：1998-07-21
申请号：US445887
申请日：1995-05-22
申请人： Steven P. Bitler , Raymond Clarke , David A. Kemp , Ray F. Stewart , Valentine Y. Yoon , Robert G. Freelin
发明人： Steven P. Bitler , Raymond Clarke , David A. Kemp , Ray F. Stewart , Valentine Y. Yoon , Robert G. Freelin
IPC分类号： C05G3/00 , C06B45/10 , C06B45/18 , C08F283/00 , C08F293/00 , C08G18/10 , C08G18/48 , C08G81/00 , C08G81/02 , C09J7/02 , C09J133/06 , C09J153/00 , C09J171/02 , B32B7/12
CPC分类号： C09J153/00 , C05G3/0029 , C05G3/0047 , C06B45/10 , C06B45/18 , C08F283/006 , C08F293/00 , C08G18/10 , C08G18/4854 , C08G81/00 , C08G81/02 , C09J133/06 , C09J171/02 , C09J7/0221 , C08G2170/40 , C08G2250/00 , C08G2390/00 , C09J2201/606 , Y10T428/28 , Y10T428/2852 , Y10T428/2883 , Y10T428/2887 , Y10T428/2891 , Y10T428/2896
摘要： TPE's which comprise A blocks or B blocks or both A blocks and B blocks, which are crystalline and in which at least a part of the crystallinity result from the presence of crystallizable side chains. Such crystalline blocks are referred to as SCC blocks. TPE's containing SCC A blocks are novel and as such form part of the present invention. The invention also includes processes, compositions, shaped articles and assemblies which make use of TPE's containing SCC A blocks.
摘要翻译： TPE包含A嵌段或B嵌段，或者是两个A嵌段和B嵌段，它们是结晶的，其中至少一部分结晶性是由可结晶侧链的存在引起的。这种结晶块被称为SCC块。含有SCC A嵌段的TPE是新颖的，因此构成本发明的一部分。本发明还包括使用含有SCC A嵌段的TPE的方法，组合物，成型制品和组件。

2. 发明授权

US09011077B2 Cooled airfoil in a turbine engine 有权
标题翻译：涡轮发动机冷却翼型
公开(公告)号：US09011077B2
公开(公告)日：2015-04-21
申请号：US13090294
申请日：2011-04-20
申请人： Paul H. Vitt , David A. Kemp , Ching-Pang Lee , John J. Marra
发明人： Paul H. Vitt , David A. Kemp , Ching-Pang Lee , John J. Marra
IPC分类号： F01D5/18
CPC分类号： F01D5/186 , F01D5/188 , F05D2250/30 , F05D2260/221 , F05D2260/941
摘要： An airfoil in a gas turbine engine includes an outer wall and an inner wall. The outer wall includes a leading edge, a trailing edge opposed from the leading edge in a chordal direction, a pressure side, and a suction side. The inner wall is coupled to the outer wall at a single chordal location and includes portions spaced from the pressure and suction sides of the outer wall so as to form first and second gaps between the inner wall and the respective pressure and suction sides. The inner wall defines a chamber therein and includes openings that provide fluid communication between the respective gaps and the chamber. The gaps receive cooling fluid that provides cooling to the outer wall as it flows through the gaps. The cooling fluid, after traversing at least substantial portions of the gaps, passes into the chamber through the openings in the inner wall.
摘要翻译：燃气涡轮发动机中的翼型件包括外壁和内壁。外壁包括前缘，从前缘朝向方向相对的后缘，压力侧和吸力侧。内壁在单个弦位置处联接到外壁，并且包括与外壁的压力和吸力侧隔开的部分，以便在内壁和相应的压力和吸力侧之间形成第一和第二间隙。内壁在其中限定一个室，并且包括在相应间隙和室之间提供流体连通的开口。间隙接收冷却流体，当其流过间隙时，向外壁提供冷却。冷却流体在穿过至少大部分间隙之后通过内壁中的开口进入腔室。

3. 发明授权

US08820091B2 External cooling fluid injection system in a gas turbine engine 有权
标题翻译：燃气涡轮发动机中的外部冷却液喷射系统
公开(公告)号：US08820091B2
公开(公告)日：2014-09-02
申请号：US13670788
申请日：2012-11-07
申请人： Kok-Mun Tham , Ching-Pang Lee , Vincent P. Laurello , Abdullatif M. Chehab , David A. Kemp , John A. Fussner , Yan Yin , Bijay K. Sultanian , Weidong Cai
发明人： Kok-Mun Tham , Ching-Pang Lee , Vincent P. Laurello , Abdullatif M. Chehab , David A. Kemp , John A. Fussner , Yan Yin , Bijay K. Sultanian , Weidong Cai
IPC分类号： F02C6/04 , F02C7/12
CPC分类号： F02C7/12 , F01D5/088 , F01D21/00 , F01D25/12 , F01D25/34 , F05D2270/3032
摘要： A cooling fluid air injection system for use in a gas turbine engine includes at an external cooling fluid source, at least one rotor cooling pipe, which is used to inject cooling fluid from the source into a rotor chamber, a piping system that provides fluid communication between the source and the rotor cooling pipe(s), a blower system for conveying the cooling fluid through the piping system and the rotor cooling pipe(s) into the rotor chamber, and a valve system. The valve system is closed during full load engine operation to prevent cooling fluid from the source from passing through the piping system, and open during less than full load engine operation to allow cooling fluid from the source to pass through the piping system.
摘要翻译：用于燃气涡轮发动机的冷却流体空气喷射系统包括在外部冷却流体源处的至少一个转子冷却管，其用于将来自所述源的冷却流体注入到转子室中;提供流体连通的管道系统在源和转子冷却管之间，用于将冷却流体通过管道系统和转子冷却管输送到转子室中的鼓风机系统和阀系统。在全负载发动机运行期间，阀系统关闭，以防止来自源的冷却流体通过管道系统，并且在小于满载发动机运行期间打开以允许来自源的冷却流体通过管道系统。

4. 发明申请

US20140123657A1 EXTERNAL COOLING FLUID INJECTION SYSTEM IN A GAS TURBINE ENGINE 有权
标题翻译：气体涡轮发动机外部冷却流体注入系统
公开(公告)号：US20140123657A1
公开(公告)日：2014-05-08
申请号：US13670788
申请日：2012-11-07
申请人： Kok-Mun Tham , Ching-Pang Lee , Vincent P. Laurello , Abdullatif M. Chehab , David A. Kemp , John A. Fussner , Yan Yin , Bijay K. Sultanian , Weidong Cai
发明人： Kok-Mun Tham , Ching-Pang Lee , Vincent P. Laurello , Abdullatif M. Chehab , David A. Kemp , John A. Fussner , Yan Yin , Bijay K. Sultanian , Weidong Cai
IPC分类号： F02C7/12
CPC分类号： F02C7/12 , F01D5/088 , F01D21/00 , F01D25/12 , F01D25/34 , F05D2270/3032
摘要： A cooling fluid air injection system for use in a gas turbine engine includes at an external cooling fluid source, at least one rotor cooling pipe, which is used to inject cooling fluid from the source into a rotor chamber, a piping system that provides fluid communication between the source and the rotor cooling pipe(s), a blower system for conveying the cooling fluid through the piping system and the rotor cooling pipe(s) into the rotor chamber, and a valve system. The valve system is closed during full load engine operation to prevent cooling fluid from the source from passing through the piping system, and open during less than full load engine operation to allow cooling fluid from the source to pass through the piping system.
摘要翻译：用于燃气涡轮发动机的冷却流体空气喷射系统包括在外部冷却流体源处的至少一个转子冷却管，其用于将来自所述源的冷却流体注入到转子室中;提供流体连通的管道系统在源和转子冷却管之间，用于将冷却流体通过管道系统和转子冷却管输送到转子室中的鼓风机系统和阀系统。在全负载发动机运行期间，阀系统关闭，以防止来自源的冷却流体通过管道系统，并且在小于满载发动机运行期间打开以允许来自源的冷却流体通过管道系统。

5. 发明授权

US5683525A Method for making cargo vessel sidewall having a seamless interior liner 失效
标题翻译：制造具有无缝内衬的货船侧壁的方法
公开(公告)号：US5683525A
公开(公告)日：1997-11-04
申请号：US502327
申请日：1995-07-13
申请人： David A. Kemp , Albert Hughes Berry, III
发明人： David A. Kemp , Albert Hughes Berry, III
IPC分类号： B62D29/00 , B62D33/04 , B65D90/04 , E06B9/26
CPC分类号： B62D29/001 , B62D33/046 , B65D90/046 , Y10S220/918 , Y10T156/1062 , Y10T428/24 , Y10T428/24008 , Y10T428/283 , Y10T428/31786
摘要： The invention is a sidewall for a cargo vessel having a seamless, snag-free interior liner. The wall includes an exterior skin that is rivetted to a first side of a supporting sidepost, and a seamless, snag-free interior liner that is mounted to the second side of the sidepost. The method for making the sidewall includes rivetting the exterior skin to the first side of the supports, and then gluing the seamless interior liner material to the second side of the supports with or without tension, and so that the interior liner is not at all pierced by fasteners, or only pierced in areas that are not likely to contact cargo. In a preferred embodiment, the interior liner is mounted to the second side of the supports under tension to maximize the interior liners' ability to absorb and deflect cargo impact and remain snag-free, sag-free and puncture resistant.
摘要翻译：本发明是一种具有无缝，无阻碍的内衬的货船的侧壁。墙壁包括铆接到支撑侧面的第一侧的外部皮肤，以及安装在侧面的第二侧上的无缝的，无阻碍的内衬。制造侧壁的方法包括将外部皮肤铆接到支撑件的第一侧，然后将无缝内衬材料粘合到具有或不具有张力的支撑件的第二侧，并且使得内衬没有被刺穿通过紧固件，或仅在不太可能接触货物的地方穿孔。在优选实施例中，内衬在张力下安装到支撑件的第二侧，以最大限度地提高内衬的吸收和偏转货物冲击的能力，并且保持无松动，无松弛和防刺穿。

6. 发明授权

US5492747A Cargo vessel sidewall having a seamless interior liner and method for making the same 失效
标题翻译：具有无缝内衬的货船侧壁及其制造方法
公开(公告)号：US5492747A
公开(公告)日：1996-02-20
申请号：US231372
申请日：1994-04-21
申请人： David A. Kemp , Albert H. Berry, III
发明人： David A. Kemp , Albert H. Berry, III
IPC分类号： B62D29/00 , B62D33/04 , B65D90/04 , B32B7/00
CPC分类号： B62D29/001 , B62D33/046 , B65D90/046 , Y10S220/918 , Y10T156/1062 , Y10T428/24 , Y10T428/24008 , Y10T428/283 , Y10T428/31786
摘要： The invention is a sidewall for a cargo vessel having a seamless, snag-free interior liner. The wall includes an exterior skin that is rivetted to a first side of a supporting sidepost, and a seamless, snag-free interior liner that is mounted to the second side of the sidepost. The method for making the sidewall includes rivetting the exterior skin to the first side of the supports, and then gluing the seamless interior liner material to the second side of the supports with or without tension, and so that the interior liner is not at all pierced by fasteners, or only pierced in areas that are not likely to contact cargo. In a preferred embodiment, the interior liner is mounted to the second side of the supports under tension to maximize the interior liners' ability to absorb and deflect cargo impact and remain snag-free, sag-free and puncture resistant.
摘要翻译：本发明是一种具有无缝，无阻碍的内衬的货船的侧壁。墙壁包括铆接到支撑侧面的第一侧的外部皮肤，以及安装在侧面的第二侧上的无缝的，无阻碍的内衬。制造侧壁的方法包括将外部皮肤铆接到支撑件的第一侧，然后将无缝内衬材料粘合到具有或不具有张力的支撑件的第二侧，并且使得内衬没有被刺穿通过紧固件，或仅在不太可能接触货物的地方穿孔。在优选实施例中，内衬在张力下安装到支撑件的第二侧，以最大限度地提高内衬的吸收和偏转货物冲击的能力，并且保持无松动，无松弛和防刺穿。

7. 发明申请

US20120269647A1 COOLED AIRFOIL IN A TURBINE ENGINE 有权
标题翻译：涡轮发动机冷却空气
公开(公告)号：US20120269647A1
公开(公告)日：2012-10-25
申请号：US13090294
申请日：2011-04-20
申请人： Paul H. Vitt , David A. Kemp , Ching-Pang Lee , John J. Marra
发明人： Paul H. Vitt , David A. Kemp , Ching-Pang Lee , John J. Marra
IPC分类号： F01D5/18
CPC分类号： F01D5/186 , F01D5/188 , F05D2250/30 , F05D2260/221 , F05D2260/941
摘要： An airfoil in a gas turbine engine includes an outer wall and an inner wall. The outer wall includes a leading edge, a trailing edge opposed from the leading edge in a chordal direction, a pressure side, and a suction side. The inner wall is coupled to the outer wall at a single chordal location and includes portions spaced from the pressure and suction sides of the outer wall so as to form first and second gaps between the inner wall and the respective pressure and suction sides. The inner wall defines a chamber therein and includes openings that provide fluid communication between the respective gaps and the chamber. The gaps receive cooling fluid that provides cooling to the outer wall as it flows through the gaps. The cooling fluid, after traversing at least substantial portions of the gaps, passes into the chamber through the openings in the inner wall.
摘要翻译：燃气涡轮发动机中的翼型件包括外壁和内壁。外壁包括前缘，从前缘朝向方向相对的后缘，压力侧和吸力侧。内壁在单个弦位置处联接到外壁，并且包括与外壁的压力和吸力侧隔开的部分，以便在内壁和相应的压力和吸力侧之间形成第一和第二间隙。内壁在其中限定一个室，并且包括在相应间隙和室之间提供流体连通的开口。间隙接收冷却流体，当其流过间隙时，向外壁提供冷却。冷却流体在穿过至少大部分间隙之后通过内壁中的开口进入腔室。

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