公开(公告)号：US12129038B2

公开(公告)日：2024-10-29

申请号：US18086841

申请日：2022-12-22

申请人： Air Cruisers Company, LLC

发明人： Thomas W. Swierkocki

IPC分类号： B64D25/00 ,  D06M11/83

CPC分类号： B64D25/00 ,  D06M11/83 ,  D10B2505/12

摘要： Described is a fabric or flexible composite material for an inflatable safety product having an emissivity of less than or equal to 0.25. The fabric or flexible composite material may include a substrate defining a surface and a metallic layer covering at least one surface of the substrate.

公开(公告)号：US11960303B2

公开(公告)日：2024-04-16

申请号：US17146699

申请日：2021-01-12

申请人： Skyryse, Inc.

发明人： Mark Groden ,  Mitch Adler ,  Jonathan Reeves ,  Nur Harell ,  Christopher Ward

IPC分类号： G05D1/10 ,  B64C13/16 ,  B64C27/57 ,  B64D17/80 ,  B64D19/02 ,  B64D25/00 ,  G05D1/00 ,  G08G5/00 ,  G08G5/02 ,  B64D45/00

CPC分类号： G05D1/106 ,  B64C13/16 ,  B64C27/57 ,  B64D17/80 ,  B64D19/02 ,  B64D25/00 ,  G05D1/0055 ,  G05D1/0072 ,  G05D1/0088 ,  G05D1/105 ,  G08G5/0013 ,  G08G5/0039 ,  G08G5/0056 ,  G08G5/0086 ,  G08G5/0091 ,  G08G5/025 ,  B64D2045/0085

摘要： A method, preferably including: sampling inputs, determining aircraft conditions, and/or acting based on the aircraft conditions. A method, preferably including: sampling inputs, determining input reliability, determining guidance, and/or controlling aircraft operation. A method, preferably including: operating the vehicle, planning for contingencies, detecting undesired flight conditions, and/or reacting to undesired flight conditions. A system, preferably an aircraft such as a rotorcraft, configured to implement the method.

公开(公告)号：US11958619B2

公开(公告)日：2024-04-16

申请号：US16485846

申请日：2018-02-27

申请人： RPS AEROSPACE s.r.l.

发明人： Giacomo Lunerti ,  Nausicaa Asia Vezzoli ,  Andrea Berna

IPC分类号： B64D17/72 ,  B64C39/02 ,  B64D17/02 ,  B64D17/26 ,  B64D17/34 ,  B64D25/00 ,  B64D27/24 ,  B64U10/13 ,  B64U70/83 ,  B64D35/02 ,  B64D35/04 ,  B64U50/19

CPC分类号： B64D17/72 ,  B64C39/024 ,  B64D17/02 ,  B64D17/26 ,  B64D17/34 ,  B64D25/00 ,  B64D27/24 ,  B64D35/02 ,  B64D35/04 ,  B64D2201/00 ,  B64U10/13 ,  B64U50/19 ,  B64U70/83

摘要： A remote piloted aircraft comprising a secondary flight assembly adapted to intervene in case of failure or an emergency of the aircraft, said secondary flight assembly being provided with an additional control unit configured to process flight relevant data and which includes an additional receiver configured to receive commands from the remote pilot by means of a remote control unit, in case of failure or emergency said additional control unit being configured to generate, as a response, an activation command adapted to activate a first device to expel an upper wing placed in a first compartment of the aircraft and to inflate a lower wing housed in a second compartment of the aircraft, and also to generate an interdiction command of the primary propulsion unit, said upper wing being maneuverable by means of a further remote control unit.

公开(公告)号：US11838366B2

公开(公告)日：2023-12-05

申请号：US17477789

申请日：2021-09-17

申请人： FEDEX CORPORATE SERVICES, INC.

发明人： Ole-Petter Skaaksrud

IPC分类号： B65D90/22 ,  A62C37/36 ,  H04L67/12 ,  G08B17/10 ,  G06Q10/0832 ,  A62C3/00 ,  B65D90/48 ,  A62C3/08 ,  A62C3/10 ,  A62C31/22 ,  A62C37/44 ,  G01J5/00 ,  G01J5/02 ,  G06Q10/0833 ,  B64D9/00 ,  G08B21/18 ,  H04Q9/00 ,  B65D90/06 ,  H04W4/38 ,  H04W4/35 ,  G06K19/07 ,  G06K19/077 ,  B60Q9/00 ,  G01C5/06 ,  G01K3/00 ,  G01K3/10 ,  G01N33/00 ,  G01T1/17 ,  H04Q9/02 ,  H04W4/021 ,  B64D25/00 ,  B64D45/00 ,  G08B23/00 ,  G08B25/00 ,  A62C3/07 ,  A62C37/40 ,  G08B25/10 ,  H04W24/08 ,  H04W12/06 ,  H02J7/00 ,  G08B17/06 ,  H04L41/04 ,  H04L41/06 ,  B65D25/02 ,  H04W12/108 ,  B60C9/00 ,  H04W84/18 ,  G08B19/00 ,  H04W88/18 ,  G06Q10/087 ,  G01J5/48

CPC分类号： H04L67/12 ,  A62C3/002 ,  A62C3/07 ,  A62C3/08 ,  A62C3/10 ,  A62C31/22 ,  A62C37/04 ,  A62C37/40 ,  A62C37/44 ,  B60C9/00 ,  B60Q9/00 ,  B64D9/00 ,  B64D9/003 ,  B64D25/00 ,  B64D45/00 ,  B65D25/02 ,  B65D90/06 ,  B65D90/22 ,  B65D90/48 ,  G01C5/06 ,  G01J5/0014 ,  G01J5/0066 ,  G01J5/025 ,  G01K3/005 ,  G01K3/10 ,  G01N33/004 ,  G01N33/0075 ,  G01T1/17 ,  G06K19/0702 ,  G06K19/0717 ,  G06K19/07758 ,  G06Q10/0832 ,  G06Q10/0833 ,  G08B17/06 ,  G08B17/10 ,  G08B21/182 ,  G08B23/00 ,  G08B25/001 ,  G08B25/009 ,  G08B25/10 ,  H02J7/00036 ,  H02J7/0047 ,  H04L41/04 ,  H04L41/06 ,  H04Q9/00 ,  H04Q9/02 ,  H04W4/021 ,  H04W4/35 ,  H04W4/38 ,  H04W12/06 ,  H04W12/108 ,  H04W24/08 ,  B60Y2200/14 ,  B60Y2200/30 ,  B60Y2200/50 ,  B65D2203/10 ,  B65D2590/0083 ,  B65G2201/0235 ,  B65G2203/0216 ,  G01J5/48 ,  G06K19/07766 ,  G06Q10/087 ,  G08B19/00 ,  H04Q2209/40 ,  H04Q2209/826 ,  H04W84/18 ,  H04W88/18

摘要： A system for detecting and verifying an environmental anomaly within a shipping container (transported on a transit vehicle having an external transceiver) has wireless sensor-based ID nodes at different locations within the container and multiple command nodes mounted to the container. A first command node is programmatically configured to be operative to detect the sensor data broadcasted from the ID nodes; responsively identify the anomaly based upon the sensor data detected by that command node; and transmit a validation request to another command node. The other command node is configured to be operative to also detect the sensor data broadcasted from the ID nodes; receive the validation request from the first command node; verify the anomaly in response to the validation request and based upon the sensor data detected by the second command node; and broadcast a verification message based upon whether the anomaly for the shipping container is verified.

公开(公告)号：US20230381560A1

公开(公告)日：2023-11-30

申请号：US18360549

申请日：2023-07-27

申请人： AML GLOBAL ECLIPSE LLC

发明人： Peter D. Haaland ,  Ken Harness

IPC分类号： A62C3/06 ,  A62C99/00 ,  A62C3/08 ,  B64D25/00 ,  F02C7/25

CPC分类号： A62C3/06 ,  A62C99/0009 ,  A62C3/08 ,  A62C99/009 ,  B64D25/00 ,  F02C7/25 ,  A62C99/0018 ,  A62C3/065 ,  F05D2260/80

摘要： A method of fire suppression may include injecting a reactive agent into a reaction zone to produce a catalytically active species for fire suppression and conveying the catalytically active species to a fire to catalytically interfere with flame chemistry of the fire. Fire in a fuel tank may be suppressed by injecting the reactive agent into a convective flow of a mixture of fuel and oxidizer in a fuel tank, the reactive agent reacting in the fuel tank to release a species which catalytically interferes with flame chemistry to suppress fire in the fuel tank. Fire at an airplane crash may be suppressed by releasing the reactive agent from the container at the crash site to produce an active species to catalytically interfere with a fire at the crash site.

公开(公告)号：US20230373633A1

公开(公告)日：2023-11-23

申请号：US18184541

申请日：2023-03-15

申请人： AmSafe, Inc.

发明人： Ronald A. Shields ,  Peter Anthony Settles ,  Willard F. Hagan ,  Giuseppe Gullotto

IPC分类号： B64D11/06 ,  B64D25/00 ,  B60R21/015 ,  B60R21/01 ,  B60R21/017 ,  B64D25/02 ,  G07C5/08

CPC分类号： B64D11/0621 ,  B64D25/00 ,  B64D11/06205 ,  B64D11/062 ,  B60R21/01546 ,  B60R21/01 ,  B60R21/0173 ,  B64D25/02 ,  G07C5/0808 ,  G07C5/0841 ,  B64D2201/00 ,  B60R21/0132

摘要： An electronic module assembly (EMA) for use in controlling one or more personal restraint systems. A programmed processor within the EMA is configured to determine when a personal restraint system associated with each seat in a vehicle should be deployed. In addition, the programmed processor is configured to perform a diagnostic self-test to determine if the EMA and the personal restraint systems are operational. In one embodiment, results of the diagnostic self-test routine are displayed on a display included on the electronic module assembly. In an alternative embodiment, the results of the diagnostic self-test routine are transmitted via a wireless transceiver to a remote device. The remote device can include a wireless interrogator or can be a remote computer system such as a cabin management computer system.

公开(公告)号：US11738216B2

公开(公告)日：2023-08-29

申请号：US16924911

申请日：2020-07-09

申请人： B/E Aerospace, Inc.

发明人： Heiko Marz ,  Thomas Sauerbaum

IPC分类号： A62B9/02 ,  B64D25/00 ,  A62B7/14 ,  A62B18/02 ,  A62B7/02

CPC分类号： A62B9/02 ,  A62B7/02 ,  A62B7/14 ,  A62B18/02 ,  B64D25/00 ,  B64D2231/025

摘要： In a preferred embodiment, methods and systems for the control of the breathing gas supply from a pressure-leading supply conduit to one or more breathing masks of an oxygen emergency supply device in a passenger aircraft include an on/off valve arranged between the supply conduit and the one or more breathing masks. The valve can be blocked or released to control air supply based upon monitoring mass flow to the breathing masks. The valve, for example, is actuated to an open position until the error between the actual mass flow and a desired mass flow exceeds a maximal error value, whereupon the valve is actuated to a closed position until the error between the actual mass flow and the desired mass flow exceeds a minimal error value whereupon the valve is actuated to the open position and the mass flow monitoring cycle is repeated.

公开(公告)号：US11591087B2

公开(公告)日：2023-02-28

申请号：US16842670

申请日：2020-04-07

申请人： Donald Lee Chalker ,  Eyal Wirsansky

发明人： Donald Lee Chalker ,  Eyal Wirsansky

IPC分类号： B64C39/02 ,  B64C27/20 ,  B64C27/52 ,  B64D25/00 ,  B64U10/13 ,  B64U30/20 ,  B64U50/14 ,  B64U101/00

摘要： The present disclosure provides a system and device for drones with ducted rotors. In some aspects, drones may comprise one or more systems of ducted rotors. In some embodiments, ducted rotors may increase the durability of the drone, limiting exposure of the rotors to external conditions and objects. In some aspects, a drone with ducted rotors may comprise a control vane or cone that may direct airflow within the drone as a mechanism to control flight path. In some implementations, a drone may comprise expandable landing gear than may allow for controlled landing, even in the event of rotor failure. In some aspects, a drone may comprise rotatable ducted rotors.

公开(公告)号：US20220371719A1

公开(公告)日：2022-11-24

申请号：US17326911

申请日：2021-05-21

申请人： U.S. Army DEVCOM Army Research Laboratory

发明人： Todd C. Henry ,  John T. Hrynuk ,  Christopher M. Kroninger ,  Michael R. Dorothy ,  Robert A. Haynes

IPC分类号： B64C3/40 ,  B64D25/00

摘要： A yaw alleviation device for an aircraft containing rotatable wing roots attached to wings. The device includes a spring configured to operatively connect to a wing; and a buckling member to operatively connect to the wing. The spring is configured to extend from an original unstrained position upon the buckling member undergoing buckling from an original unbuckled position to cause rotation of one or both wings in rotationally opposite directions. The buckling member may be positioned parallel and at an offset distance to the spring.

公开(公告)号：US11442475B2

公开(公告)日：2022-09-13

申请号：US16464274

申请日：2017-10-23

申请人： Autonomous Control Systems Laboratory Ltd.

发明人： Daisuke Iwakura ,  Yuji Ogawa ,  Nobuyuki Togashi

IPC分类号： G05D1/10 ,  B64C39/02 ,  B64D25/00 ,  B64D27/24 ,  B64D31/06 ,  B64D47/08

摘要： An unmanned aircraft 1 according to an embodiment of the present invention provides an unmanned aircraft that properly makes a forced landing in case of an abnormality. The unmanned aircraft 1 is configured as a multicopter that flies with lift and thrust generated by rotation of six rotors 13. The unmanned aircraft 1 identifies a forced landing site in a case of having detected an abnormality during flight and controls motors 12 configured to drive the respective rotors 13, to make a landing at the identified forced landing site. The unmanned aircraft 1 is consequently enabled to make an autonomous forced landing at a specific site in case of an abnormality.