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1. 发明申请

US20080098713A1 GAS TURBINE ENGINE ASSEMBLY AND METHODS OF ASSEMBLING SAME 有权
标题翻译：气体涡轮发动机组件及其组装方法
公开(公告)号：US20080098713A1
公开(公告)日：2008-05-01
申请号：US11553571
申请日：2006-10-27
申请人： Robert Joseph Orlando , Thomas Ory Moniz , Jan Christopher Schilling
发明人： Robert Joseph Orlando , Thomas Ory Moniz , Jan Christopher Schilling
IPC分类号： F02K3/02
CPC分类号： F02K3/06 , F01D15/12 , F02K3/072 , Y02T50/671
摘要： A method of assembling a gas turbine assembly includes providing a core gas turbine engine including a high-pressure compressor, a combustor, and a turbine, coupling a low-pressure turbine to the core gas turbine engine, coupling a booster compressor to a gearbox, and coupling the gearbox to the low-pressure turbine such that the booster compressor is driven by the low-pressure turbine.
摘要翻译：一种组装燃气轮机组件的方法包括提供包括高压压缩机，燃烧器和涡轮机的核心燃气涡轮发动机，将低压涡轮机耦合到核心燃气涡轮发动机，将升压压缩机连接到变速箱，并且将所述齿轮箱联接到所述低压涡轮机，使得所述增压压缩机由所述低压涡轮机驱动。

2. 发明授权

US07832193B2 Gas turbine engine assembly and methods of assembling same 有权
标题翻译：燃气轮机组装及组装方法
公开(公告)号：US07832193B2
公开(公告)日：2010-11-16
申请号：US11553571
申请日：2006-10-27
申请人： Robert Joseph Orlando , Thomas Ory Moniz , Jan Christopher Schilling
发明人： Robert Joseph Orlando , Thomas Ory Moniz , Jan Christopher Schilling
IPC分类号： F02K3/02
CPC分类号： F02K3/06 , F01D15/12 , F02K3/072 , Y02T50/671
摘要： A method of assembling a gas turbine assembly includes providing a core gas turbine engine including a high-pressure compressor, a combustor, and a turbine, coupling a low-pressure turbine to the core gas turbine engine, coupling a booster compressor to a gearbox, and coupling the gearbox to the low-pressure turbine such that the booster compressor is driven by the low-pressure turbine.
摘要翻译：一种组装燃气轮机组件的方法包括提供包括高压压缩机，燃烧器和涡轮机的核心燃气涡轮发动机，将低压涡轮机耦合到核心燃气涡轮发动机，将升压压缩机连接到变速箱，并且将所述齿轮箱联接到所述低压涡轮机，使得所述增压压缩机由所述低压涡轮机驱动。

3. 发明申请

US20090064683A1 POWER TAKE-OFF SYSTEM AND GAS TURBINE ENGINE ASSEMBLY INCLUDING SAME 有权
标题翻译：动力系统和气体发动机组件包括相同的
公开(公告)号：US20090064683A1
公开(公告)日：2009-03-12
申请号：US11695741
申请日：2007-04-03
申请人： Thomas Ory Moniz , Jan Christopher Schilling , Robert Joseph Orlando , Raymond Felix Patt
发明人： Thomas Ory Moniz , Jan Christopher Schilling , Robert Joseph Orlando , Raymond Felix Patt
IPC分类号： F02C7/32 , B23P11/00 , F16H37/00 , F02C3/10
CPC分类号： F02C7/275 , F02C7/32 , F02C7/36 , Y02T50/671 , Y10T29/49245
摘要： A power take-off system for a gas turbine engine includes a starter coupled to a second spool, and a clutch assembly coupled between the starter and a first spool, the clutch assembly configured to couple the first spool to the starter when starting the gas turbine engine assembly. A method of assembling a gas turbine engine assembly that includes the power take-off system, and a gas turbine engine assembly including the power take-off system are also described.
摘要翻译：用于燃气涡轮发动机的动力输出系统包括联接到第二阀芯的起动器和联接在起动器和第一阀芯之间的离合器组件，所述离合器组件构造成当启动燃气轮机时将第一阀芯耦合到起动器发动机总成。还描述了组装包括动力输出系统的燃气涡轮发动机组件的方法和包括动力输出系统的燃气涡轮发动机组件。

4. 发明授权

US08015828B2 Power take-off system and gas turbine engine assembly including same 有权
标题翻译：动力输出系统和包括其的燃气涡轮发动机总成
公开(公告)号：US08015828B2
公开(公告)日：2011-09-13
申请号：US11695741
申请日：2007-04-03
申请人： Thomas Ory Moniz , Jan Christopher Schilling , Robert Joseph Orlando , Raymond Felix Patt
发明人： Thomas Ory Moniz , Jan Christopher Schilling , Robert Joseph Orlando , Raymond Felix Patt
IPC分类号： F02C7/26 , F02C7/22 , F02C7/275
CPC分类号： F02C7/275 , F02C7/32 , F02C7/36 , Y02T50/671 , Y10T29/49245
摘要： A power take-off system for a gas turbine engine includes a starter coupled to a second spool, and a clutch assembly coupled between the starter and a first spool, the clutch assembly configured to couple the first spool to the starter when starting the gas turbine engine assembly. A method of assembling a gas turbine engine assembly that includes the power take-off system, and a gas turbine engine assembly including the power take-off system are also described.
摘要翻译：用于燃气涡轮发动机的动力输出系统包括联接到第二阀芯的起动器和联接在起动器和第一阀芯之间的离合器组件，所述离合器组件构造成当启动燃气轮机时将第一阀芯耦合到起动器发动机总成。还描述了组装包括动力输出系统的燃气涡轮发动机组件的方法和包括动力输出系统的燃气涡轮发动机组件。

5. 发明申请

US20080148881A1 POWER TAKE-OFF SYSTEM AND GAS TURBINE ENGINE ASSEMBLY INCLUDING SAME 审中-公开
标题翻译：动力系统和气体发动机组件包括相同的
公开(公告)号：US20080148881A1
公开(公告)日：2008-06-26
申请号：US11614623
申请日：2006-12-21
申请人： Thomas Ory Moniz , Jan Christopher Schilling , Robert Joseph Orlando , Raymond Felix Patt
发明人： Thomas Ory Moniz , Jan Christopher Schilling , Robert Joseph Orlando , Raymond Felix Patt
IPC分类号： F16H37/00
CPC分类号： F02C7/32 , F05D2220/50 , F05D2220/76 , F05D2260/4031 , Y02T50/671 , Y10T29/4932
摘要： A power take-off system for a gas turbine engine includes a starter coupled to a first spool using a first shaft, and a generator coupled to the second spool using a second shaft, the first shaft is circumferentially offset by the second shaft by an angle α. A method of assembling a gas turbine engine assembly that includes the power take-off system, and a gas turbine engine assembly including the power take-off system are also described.
摘要翻译：用于燃气涡轮发动机的动力输出系统包括使用第一轴联接到第一阀芯的起动器和使用第二轴联接到第二阀芯的发电机，第一轴由第二轴沿周向偏移一定角度 α。还描述了组装包括动力输出系统的燃气涡轮发动机组件的方法和包括动力输出系统的燃气涡轮发动机组件。

6. 发明授权

US10917036B2 Tilting solar panel mount 有权
公开(公告)号：US10917036B2
公开(公告)日：2021-02-09
申请号：US16856371
申请日：2020-04-23
申请人： Jan Christopher Schilling
发明人： Jan Christopher Schilling
IPC分类号： H02S20/30 , H02S30/10
摘要： An example device for mounting for a solar array may include a solar panel carrier configured to receive a solar array to form a panel assembly; a pivot configured to pivotably secure the solar panel carrier with respect to a support structure; and/or a restoring moment element operatively connected to the solar panel carrier and configured to exert a restoring moment on the solar panel carrier opposite in direction and approximately equal in magnitude to a gravitational moment of the panel assembly when the solar panel carrier is tilted to various angular positions. When the solar panel carrier is at a nominal angular position, a center of gravity of the panel assembly may be above and substantially vertically aligned with the pivot axis.

7. 发明申请

US20200350853A1 TILTING SOLAR PANEL MOUNT 审中-公开
公开(公告)号：US20200350853A1
公开(公告)日：2020-11-05
申请号：US16856371
申请日：2020-04-23
申请人： Jan Christopher Schilling
发明人： Jan Christopher Schilling
IPC分类号： H02S20/30 , H02S30/10
摘要： An example device for mounting for a solar array may include a solar panel carrier configured to receive a solar array to form a panel assembly; a pivot configured to pivotably secure the solar panel carrier with respect to a support structure; and/or a restoring moment element operatively connected to the solar panel carrier and configured to exert a restoring moment on the solar panel carrier opposite in direction and approximately equal in magnitude to a gravitational moment of the panel assembly when the solar panel carrier is tilted to various angular positions. When the solar panel carrier is at a nominal angular position, a center of gravity of the panel assembly may be above and substantially vertically aligned with the pivot axis.

8. 发明授权

US08166748B2 Gas turbine engine booster having rotatable radially inwardly extending blades and non-rotatable vanes 有权
标题翻译：燃气涡轮发动机助力器具有可旋转的径向向内延伸的叶片和不可转动的叶片
公开(公告)号：US08166748B2
公开(公告)日：2012-05-01
申请号：US12275813
申请日：2008-11-21
申请人： Jan Christopher Schilling
发明人： Jan Christopher Schilling
IPC分类号： F02K3/00
CPC分类号： F01D1/26 , F02C3/067 , F02K3/072 , Y02T50/671
摘要： A gas turbine engine booster includes one or more rotatable booster stages having booster blades extending radially inwardly from a rotatable drum and one or more non-rotatable vane stages having booster vanes extending radially outwardly from a non-rotatable shell. The booster stages may be interdigitated with the vane stages. The booster may be co-rotatable or counter-rotatable with respect to a fan stage of an aircraft gas turbine engine. The booster may be driven by a single turbine or one of counter-rotatable turbines or though a gearbox by these turbines. The booster blades and the booster vanes extend across a core engine inlet duct having an entrance downstream of the first fan stage. A fan section with the booster may have counter-rotatable first and second fan stages with fan blades of the second fan stages connected to and mounted radially outwardly of the rotatable drum.
摘要翻译：燃气涡轮发动机增压器包括一个或多个可旋转助力器级，其具有从可旋转鼓径向向内延伸的辅助叶片和一个或多个不可旋转叶片级，其具有从不可旋转外壳径向向外延伸的辅助叶片。增压器级可以与叶片级相互指指。增压器可以相对于飞机燃气涡轮发动机的风扇台共同旋转或反向旋转。增压器可以由单个涡轮机或一个反向旋转涡轮机驱动，或者由这些涡轮机驱动。增压叶片和增压叶片延伸穿过具有在第一风扇台下游的入口的核心发动机入口管道。具有助力器的风扇部分可以具有可反转的第一和第二风扇级，其中第二风扇级的风扇叶片连接到可旋转滚筒的径向向外并且被安装在径向向外。

9. 发明申请

US20100126141A1 GAS TURBINE ENGINE BOOSTER HAVING ROTATABLE RADIALLY INWARDLY EXTENDING BLADES AND NON-ROTATABLE VANES 有权
标题翻译：燃气涡轮发动机起动器具有可旋转的径向延伸的叶片和不可旋转的风扇
公开(公告)号：US20100126141A1
公开(公告)日：2010-05-27
申请号：US12275813
申请日：2008-11-21
申请人： Jan Christopher Schilling
发明人： Jan Christopher Schilling
IPC分类号： F02K3/072 , F02C3/067 , F01D9/04
CPC分类号： F01D1/26 , F02C3/067 , F02K3/072 , Y02T50/671
摘要： A gas turbine engine booster includes one or more rotatable booster stages having booster blades extending radially inwardly from a rotatable drum and one or more non-rotatable vane stages having booster vanes extending radially outwardly from a non-rotatable shell. The booster stages may be interdigitated with the vane stages. The booster may be co-rotatable or counter-rotatable with respect to a fan stage of an aircraft gas turbine engine. The booster may be driven by a single turbine or one of counter-rotatable turbines or though a gearbox by these turbines. The booster blades and the booster vanes extend across a core engine inlet duct having an entrance downstream of the first fan stage. A fan section with the booster may have counter-rotatable first and second fan stages with fan blades of the second fan stages connected to and mounted radially outwardly of the rotatable drum.
摘要翻译：燃气涡轮发动机增压器包括一个或多个可旋转助力器级，其具有从可旋转鼓径向向内延伸的辅助叶片和一个或多个不可旋转叶片级，其具有从不可旋转外壳径向向外延伸的辅助叶片。增压器级可以与叶片级相互指指。增压器可以相对于飞机燃气涡轮发动机的风扇台共同旋转或反向旋转。增压器可以由单个涡轮机或一个反向旋转涡轮机驱动，或者由这些涡轮机驱动。增压叶片和增压叶片延伸穿过具有在第一风扇台下游的入口的核心发动机入口管道。具有助力器的风扇部分可以具有可反转的第一和第二风扇级，其中第二风扇级的风扇叶片连接到可旋转滚筒的径向向外并且被安装在径向向外。

10. 发明授权

US07694505B2 Gas turbine engine assembly and method of assembling same 有权
标题翻译：燃气轮机组装及组装方法
公开(公告)号：US07694505B2
公开(公告)日：2010-04-13
申请号：US11461019
申请日：2006-07-31
申请人： Jan Christopher Schilling
发明人： Jan Christopher Schilling
IPC分类号： F02K3/02
CPC分类号： F02K3/06 , F02C7/36 , F05D2230/60 , F05D2260/40311 , Y02T50/671
摘要： A method of assembling a gas turbine assembly includes providing a core gas turbine engine including a high-pressure compressor, a combustor, and a turbine, coupling a low-pressure turbine axially aft from the core gas turbine engine, coupling a fan assembly axially forward from the core gas turbine engine, and coupling a booster compressor to the low-pressure turbine such that the booster compressor and the low-pressure turbine rotate at a first rotational speed.
摘要翻译：一种组装燃气轮机组件的方法包括提供包括高压压缩机，燃烧器和涡轮机的核心燃气涡轮发动机，将低压涡轮轴向与核心燃气涡轮发动机轴向耦合，将风扇组件轴向前进从所述核心燃气涡轮发动机，并且将增压压缩机耦合到所述低压涡轮机，使得所述增压压缩机和所述低压涡轮机以第一转速旋转。

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