子分类：
| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 161 | JPH0227688Y2 - | JP9320685 | 1985-06-20 | JPH0227688Y2 | 1990-07-26 | |
| 162 | JPH0227687Y2 - | JP8811285 | 1985-06-11 | JPH0227687Y2 | 1990-07-26 | |
| 163 | JPH0227686Y2 - | JP5561985 | 1985-04-15 | JPH0227686Y2 | 1990-07-26 | |
| 164 | JPS6311300U - | JP10505886 | 1986-07-08 | JPS6311300U | 1988-01-25 | |
| 165 | JPS6213218U - | JP10501385 | 1985-07-10 | JPS6213218U | 1987-01-27 | |
| 166 | JPS6116677B2 - | JP1827181 | 1981-02-10 | JPS6116677B2 | 1986-05-01 | AKAO TOSHIO; OKITA SHIGERU |
| 167 | JPS5935300U - | JP13074182 | 1982-08-31 | JPS5935300U | 1984-03-05 | |
| 168 | Method of launching rocket booster | JP12107177 | 1977-10-08 | JPS5456000A | 1979-05-04 | KUSANO MASAAKI |
| 169 | Method of transport by aircraft | JP11833877 | 1977-10-01 | JPS5453493A | 1979-04-26 | KUSANO MASAAKI |
| 170 | JPS5314838B2 - | JP13764073 | 1973-12-12 | JPS5314838B2 | 1978-05-20 | |
| 171 | JPS5141899U - | JP10023674 | 1974-08-23 | JPS5141899U | 1976-03-27 | |
| 172 | JPS5088799A - | JP13764073 | 1973-12-12 | JPS5088799A | 1975-07-16 | |
| 173 | JPS4833199Y1 - | JP9620069 | 1969-10-11 | JPS4833199Y1 | 1973-10-08 | |
| 174 | JPS4877900U - | JP19687271 | 1971-12-27 | JPS4877900U | 1973-09-26 | |
| 175 | JPS4533840Y1 - | JP3454768 | 1968-04-27 | JPS4533840Y1 | 1970-12-23 | |
| 176 | JPS443175Y1 - | JP2729166 | 1966-03-25 | JPS443175Y1 | 1969-02-05 | |
| 177 | AIRCRAFT PROPULSION MODULE AND AIRCRAFT | EP21186951.6 | 2021-07-21 | EP4032811B1 | 2025-03-05 | VINCEKOVIC, David; PASQUIET, Florian; SAVIN, Olivier |
| An aircraft propulsion module (1) comprises a hydrogen storage system (11), an electrochemical converter (7) connected to the hydrogen storage system, wherein the at least one electrochemical converter is adapted to convert hydrogen supplied from the hydrogen storage system into electric energy, and an electric motor (5) electrically connected to the electrochemical converter, wherein the electric motor is adapted to generate thrust; wherein the propulsion module comprises at least one separation means adapted to separate at least one component of the propulsion module from the propulsion module. An aircraft (3) comprises at least one aircraft propulsion module. A method for operating a propulsion module comprises that: during operation of the propulsion module, at least one separation means (22) is actuated, by which actuation at least one component (8) of the propulsion module is separated from the remaining propulsion module (12) and then falls from the remaining propulsion module. | ||||||
| 178 | VEHICLE, TRANSPORT SYSTEM (VARIANTS) AND METHOD OF MOVING VEHICLE | EP23195276.3 | 2023-09-05 | EP4342794A1 | 2024-03-27 | Andreev, Pavel Ruslanovich |
Provided is a vehicle comprising a fuselage provided with at least one storage module configured each to accommodate therein unmanned aerial systems and at least one docking module configured each to detachably interact with at least one of said unmanned aerial systems so as to enable connection thereof to the fuselage for movement of said a vehicle, and a control module configured to present control commands to at least one of said unmanned aerial systems so as to enable release thereof from the storage module for interaction with one of said docking modules. Furthermore, provided are variants of the transport system, each of which variants comprises the subject vehicle, and a method of moving the subject vehicle.
|
||||||
| 179 | SENSOR SYSTEM WITH AN ATTACHMENT ELEMENT FOR A MANNED OR UNMANNED AIRCRAFT | EP17740028.0 | 2017-07-19 | EP3497485B1 | 2023-06-07 | DØSSING ANDREASEN, Arne; JAKOBSEN, Jakob |
| 180 | ENTANGLEMENT DEVICE AND METHOD OF USE | EP20726889.7 | 2020-04-02 | EP3953657A1 | 2022-02-16 | MORTON, Nicholas |
| An entanglement device (50) has multiple elongate filaments (53) attached together to form a tassel. The entanglement device (50) is of particular use for disabling the propellers (52) of a nuisance airborne drone. When deployed, the filaments (53) spread apart over a relatively wide area before being pulled into the drone's propellers (52), wrapping around them and forcing the drone to land. Also included is a method of disabling a propeller (52) of a drone. | ||||||
QQ群二维码
意见反馈
意见反馈