| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 81 | Automatically self-releasing | US2486418D | US2486418A | 1949-11-01 | ||
| 82 | Automatically self-releasing aircraft landing hook | US48485243 | 1943-04-28 | US2486397A | 1949-11-01 | FEILBACH HARVEY O |
| 83 | Emergency arresting device for aircraft | US61341445 | 1945-08-29 | US2475597A | 1949-07-12 | DICKSON JAMES J |
| 84 | Arresting hook retracting mechanism | US58527845 | 1945-03-28 | US2428684A | 1947-10-07 | SANBORN DANIEL S; KOPS EARL A |
| 85 | Tailless airplane arresting hook | US48566843 | 1943-05-04 | US2419456A | 1947-04-22 | LEE JOHN G |
| 86 | Telescoping-retracting hook for | US2419438D | US2419438A | 1947-04-22 | ||
| 87 | Release mechanism | US61825732 | 1932-06-20 | US2413713A | 1947-01-07 | JOLLY CARL H |
| 88 | Manually operated arresting hook | US15827437 | 1937-08-10 | US2407709A | 1946-09-17 | LESCHER GEORGE W; STEET WALTER H |
| 89 | Arresting mechanism for aircraft | US18414238 | 1938-01-10 | US2399244A | 1946-04-30 | NICHOLSON CHARLES A |
| 90 | Device for arresting the motion of vehicles | US19689738 | 1938-03-19 | US2151704A | 1939-03-28 | KING DENVER R |
| 91 | Sliding oleo landing hook | US52300631 | 1931-03-16 | US1816228A | 1931-07-28 | MINSHALL ROBERT J |
| 92 | Shock-absorbing landing hook | US30553028 | 1928-09-12 | US1749438A | 1930-03-04 | MINSHALL ROBERT J |
| 93 | Airplane-arresting hook | US21912927 | 1927-09-12 | US1668113A | 1928-05-01 | HAASE HERMAN H; ARNOLD FREDERICK G |
| 94 | Airplane | US68410824 | 1924-01-03 | US1562549A | 1925-11-24 | WARD HALL CHARLES |
| 95 | Landing gear for aeroplanes | US52394321 | 1921-12-21 | US1488572A | 1924-04-01 | VROOM GUYSBERT B |
| 96 | Mboeait-akchob | US1316620D | US1316620A | 1919-09-23 | ||
| 97 | UNMANNED AERIAL VEHICLE (UAV) AND SYSTEM AND METHOD FOR CAPTURE OF THREAT UAVS | US15898850 | 2018-02-19 | US20180244401A1 | 2018-08-30 | James C. Kilian; Brede J. Wegener; Eric Wharton; David R. Gavelek |
| An apparatus for use as part of, or attached to, an unmanned aerial vehicle (UAV) to intercept and entangle a threat unmanned aerial vehicle, includes a flight and payload control system for controlling power to the UAV and for controlling maneuvering of the UAV. A host-side mount may be coupled to the UAV and is in communication with the flight and payload control system. A payload-side mount is removably attached to the host-side mount and includes a power interface and a control interface between the payload-side mount and the host-side mount. A counter-UAV system is coupled to the payload-side mount and includes a deployable chute net having a cross-sectional area sized for intercepting and entangling the threat unmanned aerial vehicle; and a deployment mechanism for mounting to the unmanned aerial vehicle. | ||||||
| 98 | AERIAL LAUNCH AND/OR RECOVERY FOR UNMANNED AIRCRAFT, AND ASSOCIATED SYSTEMS AND METHODS | US15839592 | 2017-12-12 | US20180162528A1 | 2018-06-14 | James Statelar McGrew; Matthew David Grubb; Andrew Keith Dickson; Andrew Royds Hayes |
| Aerial launch and/or recovery for unmanned aircraft, and associated systems and methods. A representative system includes a first, carrier aircraft having an airframe a propulsion system carried by the airframe and positioned to support the carrier aircraft in hover, and a capture line carried by the carrier aircraft and deployable to hang from the carrier aircraft. The capture line is sized to releasably engage with a capture device of a second, carried aircraft. The system further includes a retrieval device positioned to support the carried aircraft for detachment from the capture line. | ||||||
| 99 | Aerial system and vehicle for continuous operation | US15291878 | 2016-10-12 | US09926084B2 | 2018-03-27 | James Peverill; Adam Woodworth; Benjamin Freudberg; Dan Cottrell; Terrence McKenna |
| An aerial vehicle landing station comprising a first post and a second post, wherein the second post is spaced apart from the first post and a cable to capture an aerial vehicle, wherein the cable is stretched between the first post and the second post and configured to support the weight of the aerial vehicle once captured and the cable may provide a charging current to the aerial vehicle once captured. One or more markers may be further positioned on the cable to designate a landing point, wherein the one or more markers are configured to be visually tracked by the aerial vehicle. A cable management device coupled to the cable via one or more pulleys may regulate tension of the cable. A communications transceiver at the aerial vehicle landing station may wirelessly communicate data with the aerial vehicle. | ||||||
| 100 | Unmanned aerial vehicle (UAV) having a deployable net for capture of threat UAVs | US14803888 | 2015-07-20 | US09896221B1 | 2018-02-20 | James C. Kilian; Brede J. Wegener; Eric Wharton; David R. Gavelek |
| An apparatus for use as part of, or attached to, an unmanned aerial vehicle (UAV) to intercept and entangle a threat unmanned aerial vehicle, includes a flight and payload control system for controlling power to the UAV and for controlling maneuvering of the UAV. A host-side mount may be coupled to the UAV and is in communication with the flight and payload control system. A payload-side mount is removably attached to the host-side mount and includes a power interface and a control interface between the payload-side mount and the host-side mount. A counter-UAV system is coupled to said payload-side mount and includes a deployable net having a cross-sectional area sized for intercepting and entangling the threat unmanned aerial vehicle; and a deployment mechanism for mounting to the unmanned aerial vehicle including a rigid mounting bar and a pair of cords, between which the deployable net is disposed. | ||||||
QQ群二维码
意见反馈
意见反馈