Harris Corporation

Eagle Technology, LLC

Gregory M Jandzio

Walter M Whybrew

Gary A Rief

Alan William Mast

Anders P Pedersen

Donald J Beck

Joseph B Brief

Charles F Dull

Robert S Vinson

Brinnan C Riley

Jay D Warshowsky

Daniel A Robison

Brett A Pigon

Charles Michael Newton

Douglas E Heckaman

Steven Robert Snyder

Brian Scott Smith

Edward G Palmer

Timothy L Fetterman

James B Nichols

Edward J Bajgrowicz

Randy Eugene Boozer

Hector Deju

Scott Burri

Charlie Dull

Larry E Crider

Jason Naylor

Joseph Kreuzpaintner

Kristopher M Peebles

Alan W Mast

An outer space deployable antenna may include a waveguide antenna feed section. A first plurality of wires and a first plurality of biased hinges may couple the first plurality of wires together to be self-biased to move between a collapsed stored configuration and an extended deployed configuration. A horn antenna section may be coupled to the waveguide antenna feed section and may include a second plurality of wires and a second plurality of biased hinges coupling the second plurality of wires together to be self-biased to move between the collapsed stored configuration and the extended deployed configuration. A flexible electrically conductive layer may cover the waveguide antenna feed section and the horn antenna section in at least the extended deployed configuration.

Deployable horn antenna and associated methods

An outer space deployable antenna may include a ground plane and a flexible antenna coupled to the ground plane and moveable between a flat stored configuration and a conical deployed configuration. The flexible antenna may include a dielectric layer and a plurality of antenna arms. The flexible antenna may have a circular shape with a circular sector notch in the flat stored configuration that closes in the conical deployed configuration.

Deployable conical space antenna and associated methods

An antenna may include a base, a gimbal mount coupled to the base, and a first guide body coupled to the base and having a first guide slot. The antenna may include a second guide body rotatably coupled with respect to the base and having a second guide slot defining a steerable intersection position with respect to the first guide slot. The antenna may also have an antenna member coupled to the gimbal mount and extending through the steerable intersection position, and an actuator configured to selectively rotate the second guide body to steer the antenna member.

Antenna with single motor positioning and related methods

Antenna system includes an elongated antenna feed tower structure having a tower base at one end which includes a plurality of feet arranged to align with a plurality of predetermined structural mounting points associated with a space vehicle bus. The antenna system also includes a deployable reflector assembly comprising a hub ring. The hub ring includes a reflector deployment mechanism around which a plurality of reflector ribs are disposed. The hub ring is advantageously arranged to engirdle the feed tower assembly. As such, the central aperture is configured to receive the feed tower assembly therein after the feed tower has already been mounted to the space vehicle.

Modular center fed reflector antenna system

Microclip appliance formed from a single conductive planar metal sheet includes portions defined along an elongated length including a pin receiver, a solder paddle and a bridge. The pin receiver includes first and second planar rings, and a spring bar extending from a periphery of the first ring to a periphery of the second ring. The solder paddle is comprised of a portion of the conductive metal sheet distal from the pin receiver and the bridge extends from a peripheral portion of the solder paddle to the second ring. Lateral bends are disposed along a length of the conductive planar metal sheet to facilitate the various portions of the microclip.

Coaxial to planar strain relief appliance and method

An antenna device includes a housing having a plurality of printed circuit board (PCB) panels connected together with folded joints therebetween to define a polyhedral shape having a first open end. Each of the PCB panels includes a dielectric substrate and an electrically conductive layer thereon inside of the housing. Wireless communication circuitry is mounted on at least one of the plurality of PCB panels outside the housing, and an antenna feed is connected to the wireless communication circuitry adjacent a second end opposite the first open end of the housing.

Horn antenna including integrated electronics and associated method

A method is for making a structural printed wiring board panel that includes a multilayer printed wiring board having opposing, outer faces and interlayer interconnects that route RF, power and control signals. Connection areas are formed in or on at least on one face for connecting the interlayer interconnects and any electrical components. A metallic face sheet is secured onto at least one outer face, adding structural rigidity to the multilayer printed wiring board. A metallic face sheet can have apertures positioned to allow access to connection areas. RF components can be carried by a face sheet and operatively connected to connection areas. Antenna elements can be positioned on the same or an opposing face sheet and operatively connected to RF components to form a phased array printed wiring board (PWB) panel.

Method of making printed wiring board with enhanced structural integrity

A printed circuit board (PCB) is disclose such that the PCB has enhanced structural integrity. The PCB has opposing, outer faces and interlayer interconnects that route RF, power and control signals. Connection areas are formed in or on at least on one face for connecting the interlayer interconnects and any electrical components. A metallic face sheet is secured onto at least one outer face, adding structural rigidity to the multilayer printed wiring board. A metallic face sheet can have apertures positioned to allow access to connection areas. RF components can be carried by a face sheet and operatively connected to connection areas. Antenna elements can be positioned on the same or an opposing face sheet and operatively connected to RF components to form a phased array printed wiring board (PWB) panel.

Printed circuit board (PCB)with enhanced structural integrity

An integrated circuit module, decoupling capacitor assembly and method are disclosed. The integrated circuit module includes a substrate and integrated circuit die mounted on the substrate and having die pads and an exposed surface opposite from the substrate. A plurality of substrate bonding pads are positioned on the substrate adjacent the integrated circuit die. A decoupling capacitor assembly is mounted on each integrated circuit die and includes a capacitor carrier secured onto the exposed surface of the integrated circuit die and a decoupling capacitor carried by the capacitor carrier. A wire bond extends from the decoupling capacitor assembly to a die pad and from a die pad to a substrate bonding pad.

Decoupling capacitor closely coupled with integrated circuit

A structural printed wiring board panel includes a multilayer printed wiring board having opposing, outer faces and interlayer interconnects that route RF, power and control signals. Connection areas are formed in or on at least on one face for connecting the interlayer interconnects and any electrical components. A metallic face sheet is secured onto at least one outer face, adding structural rigidity to the multilayer printed wiring board. A metallic face sheet can have apertures positioned to allow access to connection areas. RF components can be carried by a face sheet and operatively connected to connection areas. Antenna elements can be positioned on the same or an opposing face sheet and operatively connected to RF components to form a phased array printed wiring board (PWB) panel.

Printed wiring board with enhanced structural integrity

At least one flexible appliance () and related method () for orthogonal, non-planar interconnections of at least a first electronic interface () disposed on a substrate () to an associated second electronic interface () positioned beneath the substrate (). The flexible appliance () is comprised of a planar body () having at least one electrical connector () extending from and orthogonally oriented relative to the planar body (). In one aspect of the invention, the electrical connector () is four electrical connectors (). There is at least one aperture () formed in the substrate () for allowing the first electronic interface () to be electrically interconnected to the associated second electronic interface (). The flexible appliance () is positioned on the substrate () by automated means. Contacts pads () on the resilient connector () are electrically connected to the second electronic interface () and the first electronic interface () by automated means such as soldering, thermo sonic bonding, or gap welding.

Growing community of inventors

Melbourne, FL, United States of America

Gregory M Jandzio