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1. 发明专利

FR2953808B1 UN AVION DONT LE RAPPORT POUSSEE-POIDS EST INFERIEUR A 1 ARRIVE A DECOLLER ET ATTERRIR DE FACON VERTICALE 未知
公开(公告)号：FR2953808B1
公开(公告)日：2016-09-09
申请号：FR1003019
申请日：2010-07-19
申请人： CHEN LI JING
发明人： CHEN LI JING
IPC分类号： B64C29/00

3. 发明专利

DK2338790T3 VTOL-flyvemaskine med jetkraft-til-vægt forhold mindre end 1 未知
公开(公告)号：DK2338790T3
公开(公告)日：2012-05-14
申请号：DK10075425
申请日：2010-09-13
申请人： CHEN LI JING
发明人： CHEN LI JING
IPC分类号： B64C29/00

4. 发明专利

CA2451754C THIENOTHIAZINE COMPOUNDS HAVING ANTI-INFLAMMATORY AND ANALGESIC ACTIVITIES AND THEIR PREPARATION METHODS AND THE USE THEREOF 未知
公开(公告)号：CA2451754C
公开(公告)日：2007-11-20
申请号：CA2451754
申请日：2002-06-24
申请人： LI JING
发明人： LI JING
IPC分类号： C07D513/04 , A61K31/54 , A61K31/542 , A61P29/00 , A61P37/00
摘要： The present invention is related to a type of thieno-[2,3-e]-1,2-thiazine compounds having molecular structure of formula (1) and its pharmaceutically acceptable salts or solvates. The present invention is also related to the method of producing the formula (1) compound, an anti-inflammatory and analgesic pharmaceutical composition containing the formula (1) compound, and the meth od of using the formula (1) compound to prepare anti-inflammatory and analgesic medicine.

5. 发明专利

CA2310065A1 CONTROLLED SYNTHESIS AND METAL-FILLING OF ALIGNED CARBON NANOTUBES 未知
公开(公告)号：CA2310065A1
公开(公告)日：1999-05-27
申请号：CA2310065
申请日：1998-11-18
申请人： MOSKOVITS MARTIN , LI JING , HASLETT THOMAS L
发明人： MOSKOVITS MARTIN , LI JING , HASLETT THOMAS L
IPC分类号： C01B31/02 , D01F9/127
摘要： The present invention provides a powerful new method for producing, uniform sized and uniformly aligned nanotubes through catalytic pyrolysis of a hydrocarbon within the dense, uniform and parallel pores of alumina nanotemplates. The catalyst, Co, Fe, Ni or another suitable substance is deposited electrochemically into the bottom of the channel of the alumina template. The nanotubes with any desired diameter in the range 5-500 nm and lengths up to 100 .mu.m, are generated by the pyrolysis of a suitable hydrocarbon inside the pores of the alumina template with at least one end open at the alumina/air interface. The nanotubes may be filled by metals using for example electroless deposition.

6. 发明专利

IL287347D0 Molecular marker detection and regulating methods in de-servitization state of cells 未知
公开(公告)号：IL287347D0
公开(公告)日：2021-12-01
申请号：IL28734721
申请日：2021-10-18
申请人： UNIV NANJING , ZHANG CHENYU , ZHOU ZHEN , HU XIUTING , LI JING , ZHOU XINYAN
发明人： ZHANG CHENYU , ZHOU ZHEN , HU XIUTING , LI JING , ZHOU XINYAN
摘要： The present invention provides a use for a small nucleolar RNA (snoRNA) or a detection reagent thereof, for use in detection of a servitization state of cells; moreover, detection and regulating methods for the snoRNA are established.

7. 发明专利

AT541782T 未知
公开(公告)号：AT541782T
公开(公告)日：2012-02-15
申请号：AT10075425
申请日：2010-09-13
申请人： CHEN LI JING
发明人： CHEN LI JING
IPC分类号： B64C29/00
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.

8. 发明专利

IL289553D0 Pyrrolo[2,3-b]pyrazines as hpk1 inhibitor and the use thereof 未知
公开(公告)号：IL289553D0
公开(公告)日：2022-03-01
申请号：IL28955322
申请日：2022-01-02
申请人： BEIGENE LTD , LI JING , WANG ZHIWEI , XU SANJIA
发明人： LI JING , WANG ZHIWEI , XU SANJIA
IPC分类号： A61P35/00
摘要： Disclosed herein is a compound of Formula (I), or a stereoisomer thereof, or a pharmaceutically acceptable salt thereof, and pharmaceutical compositions comprising thereof. Also disclosed is a method of treating HPK1 related disorders or diseases by using the compound disclosed herein.

9. 发明专利

AU2011329362A1 Multi-array laterolog tools and methods with differential voltage measurements 未知
公开(公告)号：AU2011329362A1
公开(公告)日：2013-05-30
申请号：AU2011329362
申请日：2011-11-02
申请人： LI SHANJUN , LI JING , SAN MARTIN LUIS , HALLIBURTON ENERGY SERV INC , BITTAR NICHAEL
发明人： LI SHANJUN , SAN MARTIN LUIS E , BITTAR NICHAEL S , LI JING
IPC分类号： G01V3/00
摘要： Multi-array laterolog tool systems and methods acquire a set of array measurements sufficient to provide laterolog tool measurements of differing array sizes. Such systems and method offer multiple depths of investigation while offering greater measurement stability in borehole environments having high resistivity contrasts. In at least some system embodiments, a wireline or LWD tool body has a center electrode positioned between multiple pairs of guard electrodes and a pair of return electrodes. The tool's electronics provide a current from the center electrode to the pair of return electrodes and currents from each pair of guard electrodes to the pair of return electrodes. Each of the currents may be distinguishable by frequency or distinguishable by some other means. This novel arrangement of currents provides a complete set of measurements that enables one tool to simultaneously emulate a whole range of laterolog tools.

10. 发明专利

RS52359B VTOL AIRCRAFT WITH A TRUST-TO-WEIGHT RATIO SMALLER THAN 1 未知
公开(公告)号：RS52359B
公开(公告)日：2012-12-31
申请号：RSP20120156
申请日：2010-09-13
申请人： CHEN LI JING
发明人： CHEN LI JING
IPC分类号： B64C29/00
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.

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