| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 101 | Radar transmitting structures | US943013 | 1992-09-10 | US5405107A | 1995-04-11 | Joseph W. Bruno |
| Internal conformal antenna arrays are mounted in aircraft aerosurface and fuselage primary and secondary load carrying structures. These radar transmitting structures are dual role structures capable of efficiently transmitting and receiving radio frequency energy, and efficiently carrying and transmitting aerodynamic loads. The internal conformal antenna arrays are mounted in the leading and trailing edges of the wings, in the empennage, and behind the outer shell of the fuselage. In order to achieve radar transmitting structures capable of transmitting radio frequency energy and meeting primary aerodynamic load carrying requirements, ceramic, quartz, or silicone-carbide fiber-reinforced organic matrix composites are combined with advanced structures technology. | ||||||
| 102 | Protective flexible boot | US92544 | 1993-07-16 | US5318251A | 1994-06-07 | Eugene H. Bergh |
| A flexible boot for covering and protecting protruding aircraft structures. The flexible boot is especially well adapted to cover and protect aircraft nose cones. In such an application the boot also protects electronic equipment including radar equipment typically located within the nose cone or radome area of the aircraft. The flexible boot has the advantage that it may be packaged by rolling it up. Preferably no discernible creases or wrinkles develop in the surface of the boot while it remains in rolled-up condition or thereafter when unrolled prior to use. The boot is formed of a flexible curved and continuous cap having a closed end and an opposed open end. The peripheral edge at the open end of the cap lies at or above the equator of the largest sphere which can be inscribed within the cap. | ||||||
| 103 | Radar apparatus | US531323 | 1990-05-31 | US5132693A | 1992-07-21 | Richard E. Werp |
| An imaging radar system for an aircraft includes four transmit antennas, connected to a central transmitter, and four receive antenna arrays for respectively receiving reflections of signals transmitted by the transmit antennas. A receiver circuit, associated with each antenna element of each receive antenna array, heterodynes the received signal to yield a resultant signal and combines the resultant signal with a reference signal to yield an interference grating signal. The grating signal of each receiver circuit is digitized and provided to a central processing unit that performs a spatial Fourier transform on the grating signals to determine angles of reflecting objects relative to each receive array. | ||||||
| 104 | Pod assembly with integrated radiofrequency emitting and aerial refueling equipment | US254694 | 1988-10-07 | US4905937A | 1990-03-06 | David T. Spotswood; Richard C. Robinson |
| A pod assembly for attachment to an aircraft including a pod housing and a fairing housing mounted on the pod housing. A bulkhead divides the pod housing into first and second compartments. The first compartment is for containing radiating electronic apparatus, such as an electronic countermeasures system. The second compartment and the fairing housing are for containing aerial refueling equipment, such as a hose-and-drogue system and power generating apparatus for the provision of power to the electronics and refueling equipment contained therein. Air from the first compartment is used for cooling the first compartment and ventilating the second compartment. | ||||||
| 105 | Aluminum nitride-boron nitride composite article and method of making same | US541914 | 1983-10-14 | US4666873A | 1987-05-19 | John R. Morris, Jr.; Richard A. Tanzilli |
| A process for making a structural ceramic article, such as, an electromagnetic window, is disclosed, wherein the ceramic article is comprised of a densified mixture of not less than 50% by volume aluminum nitride and up to about 50% by volume boron nitride. The ceramic article of the present invention may be used as a shield or protective barrier such as an electromagnetic window for communication or detection devices on high speed transportation or delivery vehicles passing through extremely hostile environments, where it exhibits radar transparency, congruent vaporization kinetics, tailorable dielectric properties, improved thermal shock resistance, improved mechanical toughness and strength, improved spall resistance, improved recession rate, i.e. erosion rate and ablation rate, and high refractoriness. | ||||||
| 106 | Linkage apparatus for synchronizing aircraft door movements with the deployment of a door-enclosed antenna | US915345 | 1978-06-13 | US4188631A | 1980-02-12 | Richard H. Dougherty; Thomas E. Fealy |
| An extendable infra-red antenna is carried in a bay portion of the aircraftormally closed by laterally-swinging, clam-shell doors. Separate, unconnected linkage assemblies driven by a common crank extend and retract both the doors and the antenna. When retracted, the antenna linkage is driven into an overcenter disposition but the door linkage is not. As a result, the doors begin to open before the antenna begins to deploy. Conversely, when the antenna is fully extended, its linkage is not overcenter but the door linkage is. The antenna then begins to retract before the doors begin to close. The overcenter relationships cause one member to first move in a direction opposite to that of the other so as to insure against any interference between the moving members. Stop means are provided to permit the antenna to be firmly secured in both its extended and retracted disposition. | ||||||
| 107 | Rain erosion resistant material for airborne vehicle | US3616140D | 1968-05-17 | US3616140A | 1971-10-26 | COPELAND ROBERT L; CHASE VANCE A |
| A radome or other like structure defining a leading edge of an airborne vehicle, which is of light weight and formed to close tolerances, including a reinforced plastic shell which may be of glass fiber reinforced epoxy or polyester laminate, and a preformed rain erosion resistant coasting or ''''boot'''' of thermoplastic material on the outer exposed surface. The thermoplastic material is a preformed coating having high electrical transparency or transmissability and good abrasion and impact resistance. The coating can be secured to the shell by a suitable adhesive system.
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| 108 | Retractable and rotatable scanning device | US67521357 | 1957-07-30 | US2984834A | 1961-05-16 | HOWARD JR GEORGE J; SMITH RODERICK L |
| 109 | Sandwich-type radome panel | US11463149 | 1949-09-08 | US2641561A | 1953-06-09 | BLACK ERIC A |
| 110 | Antenna system | US6178648 | 1948-11-24 | US2555857A | 1951-06-05 | ANN NELSON JESSIE; ARTHUR DORNE |
| 111 | Antenna installation on airplanes | US7248849 | 1949-01-24 | US2495748A | 1950-01-31 | MATSON CARROLL H |
| 112 | PAYLOAD SHROUD FOR AIR VEHICLE | EP14876435 | 2014-10-08 | EP3094554A4 | 2017-09-06 | ATZERT MONICA; WALLACE JASON; HURN ROBERT; DEARDORFF DOUG; ZELENY TERRY |
| A UAV includes a body. The body defines a payload opening 14. The payload opening is circular, but any shape may be used. A payload of the UAV is arranged in the payload opening. The payload may be a camera, sensors, a package, etc. A payload shroud may be installed which prohibits or reduced ingress of foreign material via payload opening. A payload shroud may include a diverter. The diverter may act as a barrier wall preventing the water or debris from entering the body of the UAV. The diverter should fit flush with the payload opening in the body of the UAV. | ||||||
| 113 | Antenna support bracket | EP11183455.2 | 2011-09-30 | EP2439136B1 | 2017-06-28 | Lundeen, Eric J. |
| 114 | A POLYUREA GASKET AND GASKET TAPE AND A METHOD OF MAKING AND USING THE SAME | EP15827906.7 | 2015-07-31 | EP3175154A1 | 2017-06-07 | BUSBY, Jeff; DRY, Mike; BOOMER, Kent; BOYD, Matt |
| A gasket or tape material for sealing between two members. The gasket or tape material, in one embodiment, includes a skeletal member and/or metallic and/or non-metallic particles. Enclosing the skeletal member and/or particles is a flexible, compressible resilient polyurea body member having a tacky outer surface, the tacky outer surface for engagement between the two members. The resilient body may be comprised of polyurea. The skeletal member may be comprised of a metallic or a non-metallic material, woven or non-woven metallic or non-metallic. | ||||||
| 115 | AIRCRAFT AND SIGNAL LINE PROTECTION ASSEMBLY THEREOF | EP14896036 | 2014-06-26 | EP3162704A4 | 2017-06-07 | OU DI |
| The present invention discloses an aerial vehicle and a signal line protection assembly thereof. The signal line protection assembly comprises a foot stand and a protection sleeve. The foot stand comprises a foot stand sleeve. At least a portion of the protection sleeve is received in the foot stand sleeve. The protection sleeve receives a signal line therein to prevent the signal line from damages of external environment. | ||||||
| 116 | ELASTMERIC GEL BODY GASKET HAVING A SUBSTANTIALLY INCOMPRESSIBLE SKELETON, A METHOD OF MAKING AND USING THE SAME | EP14843364 | 2014-09-12 | EP3043993A4 | 2017-06-07 | BOYD MATT; BUSBY JEFF; BOOMER KENT; DRY MICHAEL |
| Gaskets, including aircraft gaskets, are disclosed, the gaskets having an elastomeric gel body and substantially incompressible skeletons. The bodies may be pliable and deformable and, in one example, may be comprised of a two-part chemically cured polyurethane that sets up as a gel after mixing with the web so that it is fully integral with the web and so that there is substantially no air bubbles or air pockets left in the web. The web may be a regular shaped web and made of nylon. | ||||||
| 117 | AIRCRAFT AND SIGNAL LINE PROTECTION ASSEMBLY THEREOF | EP14896036.2 | 2014-06-26 | EP3162704A1 | 2017-05-03 | OU, Di |
The present invention discloses an aerial vehicle and a signal line protection assembly thereof. The signal line protection assembly comprises a foot stand and a protection sleeve. The foot stand comprises a foot stand sleeve. At least a portion of the protection sleeve is received in the foot stand sleeve. The protection sleeve receives a signal line therein to prevent the signal line from damages of external environment. |
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| 118 | ELASTMERIC GEL BODY GASKET HAVING A SUBSTANTIALLY INCOMPRESSIBLE SKELETON, A METHOD OF MAKING AND USING THE SAME | EP14843364.2 | 2014-09-12 | EP3043993A2 | 2016-07-20 | BOYD, Matt; BUSBY, Jeff; BOOMER, Kent; DRY, Michael |
| Gaskets, including aircraft gaskets, are disclosed, the gaskets having an elastomeric gel body and substantially incompressible skeletons. The bodies may be pliable and deformable and, in one example, may be comprised of a two-part chemically cured polyurethane that sets up as a gel after mixing with the web so that it is fully integral with the web and so that there is substantially no air bubbles or air pockets left in the web. The web may be a regular shaped web and made of nylon. | ||||||
| 119 | CABLE CUTTER ANTENNA FOR AIRCRAFT | EP14717803.2 | 2014-03-12 | EP2976258A1 | 2016-01-27 | HIRONS, Paul |
| A cable cutter (10) for an aircraft (27) comprises an electrically-conducting body (12) configured to be mounted on an aircraft (27) and to cut a cable and an electrically-conducting auxiliary member (38) attached to, and electrically isolated from, the body (12). The body (12) and auxiliary member (38) are configured to together form an antenna. A method of manufacturing an antenna for an aircraft comprises the steps of providing a cable cutter (10) for an aircraft, the cable cutter comprising an electrically-conducting body (12) configured to be mounted on an aircraft (27) and to cut a cable; providing an electrically conducting auxiliary member (38) and attaching it to the body (12) so as to be electrically isolated from the body (12); and providing an antenna connector (42) and connecting the terminals thereof to the body (12) and auxiliary member (38) respectively. | ||||||
| 120 | PROCÉDÉ D'OUVERTURE D'UN DÔME DE PROTECTION, EN PARTICULIER D'UN RÂDOME, ET RÂDOME ÉQUIPÉ D'UN PANTOGRAPHE DE MISE EN OEUVRE | EP12734989.2 | 2012-06-26 | EP2724417B1 | 2015-08-12 | FOURNIE, Jacques; BERNUS, Christophe; DUPAS, Thony; PHALIPPOU, Jérôme; MERCADIER, Gilles; TOUREILLE, Nicolas; MILIN, Frédéric; REDON, Jean |
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