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1. 发明授权

EP3263454B1 VTOL AIRCRAFT WITH A THRUST-TO-WEIGHT RATIO SMALLER THAN 0.1 有权
公开(公告)号：EP3263454B1
公开(公告)日：2018-09-26
申请号：EP17020335.0
申请日：2014-04-17
申请人： Chen, Li Jing
发明人： Chen, Li Jing
IPC分类号： B64C29/00 , B64C21/04
CPC分类号： B64C29/00 , B64C9/00 , B64C15/02 , B64C21/04 , B64C23/005 , B64C29/005 , B64C29/0066 , B64C2009/005 , B64D27/16 , Y02T50/166
摘要： An aircraft includes: ailerons (1,2); a turbofan engine (3) comprising a high-temp duct (4) with an openable/ closable propelling nozzle (5), and a low-temp duct (6) with an openable/closable propelling nozzle (7); a high-temp bypass duct (9) comprising an openable/closable inlet (8) connected to the high-temp duct(4), an outer wall(10) and a rectangle outlet(12) with a height-to-width ratio smaller than 0.1; a low-temp bypass duct (15) comprising an openable/closable inlet (14) connected to the low-temp duct (7), an outer wall (16), an inner wall (17) and a rectangle outlet (19) with a height-to-width ratio smaller than 0.1. During vertical take-off/lading, closing the propelling nozzles (5, 7) of turbofan engine (3), and opening the inlets (8,14) of high-temp and low-temp bypass ducts(9,15), low-temp planar air jet (20) is cause to flow over upper surface of the aircraft, thereby generating lift and no air flow over lower one.

2. 发明授权

EP1510217B1 AN ANTI-RHEUMATISM MEDICAMENT AND METHOD FOR ITS PREPARATION 有权
标题翻译：抗风湿及其制造方法
公开(公告)号：EP1510217B1
公开(公告)日：2015-11-11
申请号：EP02724085.2
申请日：2002-04-09
申请人： Sichuan Institute of Chinese Materia Medica , Guangzhou Chen Li Ji Pharmaceutical Factory
发明人： DENG, Wenlong
IPC分类号： A61P29/00
CPC分类号： A61K36/37 , A61K36/296 , A61K36/43 , A61K36/815 , A61K2300/00

3. 发明公开

EP3050662A1 SCREW TAP WITH REPLACEABLE TOOL BIT 审中-公开
标题翻译： TAPS具有可互换切削刀片
公开(公告)号：EP3050662A1
公开(公告)日：2016-08-03
申请号：EP13894719.7
申请日：2013-11-01
申请人： Chen, Li-Cheng
发明人： Chen, Li-Cheng
IPC分类号： B23G5/06 , B23G1/46
CPC分类号： B23G5/06 , B23G2200/10 , B23G2200/12 , B23G2200/36
摘要： A screw tap with replaceable tool bit has a holding body (10), a detachable blade (20), and a fixing element. The holding body (10) has a receiving area (13) and a first engaging portion. The detachable blade (20) is mounted in the receiving area (13) of the holding body (10) and has a second engaging portion, and the second sharp part of the second engaging portion engages with the first sharp part of the first engaging portion. The fixing element is securely mounted through the holding body (10) and the detachable blade (20). The detachable blade (20) can disassemble from the holding body (10), and thus one holding body (10) could be installed with detachable blades (20) of various dimensions. As the detachable blade (20) is damaged, the damaged detachable blade (20) is replaced with a new detachable blade (20) to keep processing.

4. 发明公开

EP1510217A4 AN ANTI-RHEUMATISM MEDICAMENT AND METHOD TO PREPARE THEREOF 有权
标题翻译：抗风湿及其制造方法
公开(公告)号：EP1510217A4
公开(公告)日：2007-08-01
申请号：EP02724085
申请日：2002-04-09
申请人： SICHUAN INST OF CHINESE MATERI , GUANGZHOU CHEN LI JI PHARMACEU
发明人： DENG WENLONG
IPC分类号： A61K31/7048 , A61K36/00 , A61K36/18 , A61K36/29 , A61K36/296 , A61K36/37 , A61K36/43 , A61K36/58 , A61K36/81 , A61K36/815 , A61P17/00 , A61P29/00 , A61P37/02 , A61K35/78
CPC分类号： A61K36/37 , A61K36/296 , A61K36/43 , A61K36/815 , A61K2300/00
摘要： This invention discloses an anti-rheumatism medicament. This invention also provides a method of its preparation. The medicament can be made from these herbal materials including Tripterygium hypoglaucum (Levl.) Hutch, Epimedium brevicornum Maxim, Lycium barbarum L. and Cuscuta chinensis Lam., or C. Australis R. Br. It has advantages such as notable therapeutic effect, low side effect and easy intake.

5. 发明公开

EP3639658A1 ASSEMBLED PET TOY DEVICE 审中-公开
公开(公告)号：EP3639658A1
公开(公告)日：2020-04-22
申请号：EP18200914.2
申请日：2018-10-17
申请人： Chen, Li-Chen
发明人： Chen, Li-Chen
IPC分类号： A01K15/02
摘要： An assembled pet toy device (1) includes a base (10), a post assembly (50) and a plurality of lateral cylinders (32). The base (10) includes a plurality of first plates (12) are stacked one upon another, and the post assembly (50) is disposed on a top surface of the base (10). The post assembly (50) includes a plurality of first assemblies (20) and a plurality of second assemblies (30). The plurality of first assemblies (20) includes a plurality of second plates (21), and the plurality of second assemblies (30) includes a plurality of third plates (31). The plurality of lateral cylinders (32) is disposed on a side surface of the plurality of second assemblies (30), and the plurality of lateral cylinders (32) includes a plurality of fourth plates (34) stacked one upon another. The first plates (12), the second plates (21), the third plates (31) and the fourth plates (34) are respectively corrugated paper plates.

6. 发明公开

EP3050662A4 SCREW TAP WITH REPLACEABLE TOOL BIT 审中-公开
标题翻译： GEWINDEBOHRER麻省理工学院AUSWECHSELBAREM SCHNEIDINSATZ
公开(公告)号：EP3050662A4
公开(公告)日：2017-04-26
申请号：EP13894719
申请日：2013-11-01
申请人： CHEN LI-CHENG
发明人： CHEN LI-CHENG
IPC分类号： B23G5/06
CPC分类号： B23G5/06 , B23G2200/10 , B23G2200/12 , B23G2200/36
摘要： A screw tap with replaceable tool bit has a holding body (10), a detachable blade (20), and a fixing element. The holding body (10) has a receiving area (13) and a first engaging portion. The detachable blade (20) is mounted in the receiving area (13) of the holding body (10) and has a second engaging portion, and the second sharp part of the second engaging portion engages with the first sharp part of the first engaging portion. The fixing element is securely mounted through the holding body (10) and the detachable blade (20). The detachable blade (20) can disassemble from the holding body (10), and thus one holding body (10) could be installed with detachable blades (20) of various dimensions. As the detachable blade (20) is damaged, the damaged detachable blade (20) is replaced with a new detachable blade (20) to keep processing.
摘要翻译：具有可更换刀头的螺丝攻具有保持体（10），可拆卸刀片（20）和固定元件。保持体（10）具有容纳区域（13）和第一接合部分。可拆卸刀片（20）安装在保持体（10）的容纳区域（13）中并具有第二接合部分，并且第二接合部分的第二尖锐部分与第一接合部分的第一尖锐部分。固定元件通过保持体（10）和可拆卸刀片（20）牢固地安装。可拆卸的刀片20可以从保持体10上拆卸下来，因此一个保持体10可以安装有各种尺寸的可拆卸的刀片20。当可拆卸刀片（20）损坏时，损坏的可拆卸刀片（20）被替换为新的可拆卸刀片（20）以保持处理。

7. 发明公开

EP2933188A1 VTOL aircraft with a thrust-to-weight ratio smaller than 0.1 审中-公开
标题翻译： Senkrechtstarterflugzeug mit einemSchubgewichtsverhältniskleiner als 0,1
公开(公告)号：EP2933188A1
公开(公告)日：2015-10-21
申请号：EP14075023.3
申请日：2014-04-17
申请人： Chen, Li Jing
发明人： Chen, Li Jing
IPC分类号： B64C29/00 , B64C21/04
CPC分类号： B64C29/00 , B64C9/00 , B64C15/02 , B64C21/04 , B64C23/005 , B64C29/005 , B64C29/0066 , B64C2009/005 , B64D27/16 , Y02T50/166
摘要： An aircraft includes: ailerons (1,2); a turbofan engine (3) comprising a high-temp duct (4) with an openable/ closable propelling nozzle (5), and a low-temp duct (6) with an openable/closable propelling nozzle (7); a high-temp bypass duct (9) comprising an openable/closable inlet (8) connected to the high-temp duct(4), an outer wall(10) and a rectangle outlet(12) with a height-to-width ratio smaller than 0.1; a low-temp bypass duct (15) comprising an openable/closable inlet (14) connected to the low-temp duct (7), an outer wall (16), an inner wall (17) and a rectangle outlet (19) with a height-to-width ratio smaller than 0.1. During vertical take-off/lading, closing the propelling nozzles (5, 7) of turbofan engine (3), and opening the inlets (8,14) of high-temp and low-temp bypass ducts(9,15), low-temp planar air jet (20) is cause to flow over upper surface of the aircraft, thereby generating lift and no air flow over lower one.
摘要翻译：飞机包括：副翼（1,2）; 涡轮风扇发动机（3）包括具有可打开/关闭的推进喷嘴（5）的高温管道（4）和具有可打开/关闭的推进喷嘴（7）的低温管道（6）; 包括连接到高温管道（4）的可打开/关闭的入口（8）的高温旁通管道（9），外壁（10）和矩形出口（12），高度 - 宽度比小于0.1; 包括连接到低温管道（7）的可打开/关闭的入口（14）的低温旁通管道（15），外壁（16），内壁（17）和矩形出口（19）高度比宽度小于0.1。在垂直起飞期间，关闭涡轮风扇发动机（3）的推进喷嘴（5,7），并打开高温和低温旁通管道（9,15）的入口（8,14），低 - 平面空气喷射（20）导致飞行器的上表面流动，从而产生升力，而不会在较低的空气流中流动。

8. 发明公开

EP3263454A1 VTOL AIRCRAFT WITH A THRUST-TO-WEIGHT RATIO SMALLER THAN 0.1 有权
标题翻译： VTOL AIRCRAFT的推重比小于0.1
公开(公告)号：EP3263454A1
公开(公告)日：2018-01-03
申请号：EP17020335.0
申请日：2014-04-17
申请人： Chen, Li Jing
发明人： Chen, Li Jing
IPC分类号： B64C29/00 , B64C21/04
CPC分类号： B64C29/00 , B64C9/00 , B64C15/02 , B64C21/04 , B64C23/005 , B64C29/005 , B64C29/0066 , B64C2009/005 , B64D27/16 , Y02T50/166
摘要： VTOL aircraft with a thrust-to-weight ratio smaller than 0.1, during vertical take-off/landing, obtains an another lift, besides a lift generated by low-temp bypass duct (15) directing the low-temp air (18) from the turbofan engine (3) to flow, through its outlet (19) in form of low-temp planar jet (20), over the upper surface of the wing and in the direction of the wingspan, by high-temp bypass duct (15) directing the high-temp air (18) from the turbofan engine (3) to flow, through its outlet (12) in form of high-temp planar jet (13), above the low-temp planar jet (20) in the direction of the wingspan and enables the ailerons (1, 2) to control the balances of the aircraft more efficiently.
摘要翻译：在垂直起飞/着陆期间推力重量比小于0.1的VTOL飞机除了由低温旁路导管（15）引导低温空气（18）产生的升力之外还获得另一升力涡轮风扇发动机3通过其低温平面射流20形式的出口19流过机翼上表面和翼展方向，并通过高温旁路导管15 ）将来自涡轮风扇发动机（3）的高温空气（18）引导通过其高温平面射流（13）形式的其出口（12），在低温平面射流（20）并且使副翼（1,2）更有效地控制飞机的平衡。

9. 发明授权

EP2338790B1 VTOL aircraft with a thrust-to-weight ratio smaller than 1 有权
标题翻译：垂直起落飞机用的推重比小于1
公开(公告)号：EP2338790B1
公开(公告)日：2012-01-18
申请号：EP10075425.8
申请日：2010-09-13
申请人： Chen, Li Jing
发明人： Chen, Li Jing
IPC分类号： B64C29/00
CPC分类号： B64C29/005

10. 发明公开

EP2338790A1 VTOL aircraft with a thrust-to-weight ratio smaller than 1 有权
标题翻译： VTOL Flugzeug mit einem Schub-Gewichtsverhältniskleiner als 1
公开(公告)号：EP2338790A1
公开(公告)日：2011-06-29
申请号：EP10075425.8
申请日：2010-09-13
申请人： Chen, Li Jing
发明人： Chen, Li Jing
IPC分类号： B64C29/00
CPC分类号： B64C29/005
摘要： An aircraft with this VTOL technology (the Invention) (6,7,8,9,10,18,19,20) can achieve VTOL even its thrust-to-weight ratio is smaller than 1.
It is impossible for an aircraft with a thrust-to-weight ratio smaller than 1 to take off and land vertically with traditional technologies. The present invention, however, can achieve VTOL on these aircraft (6,7,8,9,10,18,19,20) by generating another lift force for VTOL by horizontally setting a Thin Wing (2) at the middle of the perpendicular line of the horizontal section inside the Air Intake Duct (5,6) in addition to the lift force obtained by traditional ways.
This invention can be used to retrofit an existing aircraft to achieve VTOL or manufacture a VTOL aircraft with a thrust-to-weight ratio smaller than 1.
摘要翻译：具有这种VTOL技术的飞机（本发明）（6,7,8,9,10,18,19,20）可以实现垂直起降，甚至其推力重量比小于1.对于具有小于1的推力重量比用传统技术起飞和垂直落地。然而，本发明可以通过在VTOL的中间水平设置薄翼（2）来产生用于VTOL的另一提升力来实现这些飞机上的垂直起伏（6,7,8,9,10,18,19,20）除了通过传统方式获得的提升力之外，进气管（5,6）内水平截面的垂直线。本发明可用于改装现有的飞机以实现VTOL或制造推力重量比小于1的垂直起降飞机。

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