Abstract: Disclosed herein are inductor/core assemblies for integrated circuits (ICs), as well as related structures, methods, and devices. In some embodiments, an IC structure may include an inductor and a magnetic core in an interior of the inductor. The magnetic core may be movable perpendicular to a plane of the inductor.

Abstract: A net wig cap for processing a braiding wig includes a plurality of net pieces, where each of the net pieces is provided with patterns composed of wig threads. A method for processing a braiding wig includes: step 1: processing the net wig cap; and step 2: crocheting hair or pre-woven single-dreadlock braids onto embroidered wig threads. The present disclosure creatively applies an embroidery machine to the field of wig processing. The present disclosure first embroiders a layer of patterns composed of wig threads on a base layer of a wig by the embroidery machine, and then crochets pre-woven single-dreadlock braids onto the embroidered wig thread patterns one by one. The present disclosure does not need to manually fix the wig threads on the wig, which greatly reduces the manual workload, improves the processing efficiency and reduces the cost.

Abstract: A contained radiation power metering system for measuring power of a radiation source of an additive manufacturing machine includes a base configured to fit within the additive manufacturing machine, a radiation sensor connected to the base and configured to receive radiation from the radiation source and output a radiation power signal, and a wireless module disposed on the base configured to receive the radiation power signal and transmit the radiation power signal from the system to a separate wireless receiver.

Abstract: An assembly includes at least three layers of sheet metal lying directly on top of one another and joined in a stack of sheet metal. The layers of sheet metal are each joined in pairs by a clinching joint. At least one layer of sheet metal arranged between one of the pairs of layers of sheet metal joined by the clinching joint and an outer side of the stack each have an access opening aligned with the clinching joint.

Abstract: A stitcher (1) for connecting an end portion of an outgoing metal strip to a starting portion of an incoming metal strip for a continuously operated strip processing system comprises a first punching tool (20), which is designed to connect metal strips having a first thickness range and/or strength range to one another, and a second punching tool (30), which is designed to connect metal strips having a second thickness range and/or strength range to one another. Both thickness ranges and/or strength ranges are different from one another.

Abstract: A front-loading washing machine includes a housing; a washing tub including one or more locking holes on a lateral side; and one or more lifters lifting up laundry based on spinning of the washing tub. The lifter includes a locking member passing through the locking hole, bent at an outside of the washing tub and extended in a spinning axis direction of the washing tub. The locking hole includes a first edge to which the locking member is locked to couple the lifter and the washing tub, and a second edge and a third edge adjacent to opposite ends of the first edge and surrounding the locking member to face with each other.

Abstract: Expandable collet bodies with sectional finger-based anti-rotation features are disclosed. The collet body comprises not only a plurality of gripping finger as a first part of a two-part anti-rotation means (ARM), but also a first part of a two part translation arresting means (TAM), which may or may not be sectional in nature. The TAM prevents over translation of a collet body within the work piece(s), and cooperates with a second part of the TAM associated with a work piece or an auxiliary structure. In this manner, a collet body inserted into a work piece or auxiliary structure will not accidentally be pushed beyond the blind side of the work piece(s) during insertion or initial clamp-up.

Abstract: A plate heat exchanger has two metal plates brought into abutment, with a solder material between the plates. The plates are heated up to a first temperature. The plates are placed into a mold, the mold surfaces of which have cavities for envisaged channel structures. Channel structures are formed by local internal pressure forming of at least one plate under pressurization by the tool. The plates are heated up to a second temperature. The plates are solder bonded at the abuted surfaces. A plate heat exchanger has two metal plates, wherein channel structures have been formed in at least one plate and the plates are bonded to one another by soldering away from the channel structures. Eutectic microstructures having a longest extent of less than 50 micrometers are formed in the solder layer.

Abstract: Board member fastener used to rivet first board member and second board member. First and second board members each have drilled therein a different diameter of hole. First board member provides first through hole. Second board member provides second through hole. Top of first through hole of first board member is formed with stop surface that tapers toward outer diameter so that when board member fastener is punch impacted, board member fastener sinks into interior of first through hole to cut second board member and to deform, and first board member is forced by sinking stress of board member fastener and tightly pressed on second board member upon punch impact, and thus, board member fastener, first board member and second board member are deformed and fitted to each other, achieving a riveting structure that can be applied to different materials and can overcome deformation caused by heat expansion and contraction.

Abstract: A method is disclosed and includes determining at least one of a height field and an orientation field of a fiber-reinforced structure. The fiber-reinforced structure includes a plurality of fiber portions and a polymer matrix. The method includes generating a reaction-diffusion representation of the fiber-reinforced structure. The reaction-diffusion representation indicates a concentration of at least one of the polymer matrix and the plurality of fiber portions. The method includes designating a reference fiber deposition path based on the reaction-diffusion representation. The method includes generating a continuous fiber deposition path based on the reference fiber deposition path. The method includes transmitting a signal representing the continuous fiber deposition path to a deposition device, the deposition device using the continuous fiber deposition path to deposit a fiber of the fiber-reinforced structure.

Abstract: A method for manufacturing a hollow camshaft is provided, and more particularly, a method for manufacturing a combined hollow camshaft by an axial-compression upsetting-deformation technique. The present method solves a problem that the current camshaft manufactured in an internal high-pressure expansion manner in the prior art has the insufficient locking force to cause the loosening of a cam. The method is as follows: a camshaft is formed by combining two independent units, namely a cam and a shaft tube. Non-circular countersinks are distributed on two sides of the cam. Thrust steps are formed on the shaft tube correspondingly. The cam is placed between the two thrust steps of the shaft tube. The locking force is applied to the cam by utilizing the thrust steps on the two sides of the cam based on thermal expansion and contraction. Simultaneously, the thrust steps lock the cam with the countersinks.

Abstract: A scroll compressor that includes a housing and scroll compressor bodies disposed in the housing. A motor is disposed within the housing and operably connected to a drive shaft for driving one of the scroll compressor bodies. The drive shaft is rotationally supported at one end by a crankcase which includes a bearing housing and a bearing. The crankcase includes a plurality of openings or gas passages passing through the crankcase, as well as a plurality of generally cylindrical sections positioned respectively between adjacent openings. The cylindrical sections define contact regions which can engage an inner periphery of the housing when the crankcase is mounted therein.

Abstract: A female die for a joining tool having an anvil and a shoulder which coaxially surrounds the anvil and which is configured on a main body of the anvil or by an end of a bush, and a sleeve which surrounds the main body or the bush, respectively, and which across the circumference thereof has radial slots penetrating the wall of said sleeve, in each case one sliding piece being guided in said slots so as to be movable in the radial direction (R), said sliding piece in the axial direction (A) being supported at least on the shoulder, is distinguished in that the wall of the sleeve on that end that surrounds the shoulder in the region between the slots has regions which widen in a radially inward manner and which extend in each case between two neighboring sliding pieces and in the radial direction (R) at least in part protrude beyond the shoulder.

Abstract: A continuous strip of T-Nuts formed on a common strip of metal. Each T-Nut of the strip of T-Nuts is integrally connected to the next adjacent T-Nut by carry tabs. The carry tabs can be frangible themselves or contain a frangible portion. Each T-Nut includes a cylindrical bore therein and a threaded interior. A mechanism feeds and severs the endmost T-Nut in endwise fashion. The mechanism to feed and sever the endmost T-Nut includes a cutting blade positioned vertically below the frangible portion of the carry tab. A shearing ram having a guide positioned axially in line with the cylindrical bore in the endmost T-Nut is adapted to move vertically from an upper to a lower position to engage the cutting blade with the frangible portion and sever the endmost T-Nut.

Abstract: A method of reducing the cycle time required for flow-drill screw operations by providing a dimple on a part that is engaged by a flow-drill screw. A tip of the flow-drill screw engages a contact band at a location spaced from the tip of the distal end of the flow-drill screw and base portion of the dimple. Friction between the flow-drill screw tip and dimple creates a heat concentration area and results in displaced material fanning a threaded collar. The flow-drill screw is secured by the threads of the threaded collar.

Abstract: A masking foil, for a shaving cartridge, and a shaving cartridge comprising a housing having a top surface, a bottom surface, a front edge, a rear edge, and a pair of side edges extending between the front edge and the rear edge. The housing includes a main blade disposed between the front edge and the rear edge. The main blade includes a main cutting edge extending toward the top surface and is movable in the housing. The shaving cartridge further comprises a masking foil. The masking foil includes a front portion located forward of the main cutting edge, a back portion located rearward the main cutting edge, and at least one ribbon which extends between the front portion and the back portion and which partially covers the main cutting edge.

Abstract: A functional element having a section that has a flange, that projects away from a side of the flange, and is adapted for an aperture-free punching into a sheet metal part and having a shaft part that projects away from a side of the flange opposite the first side, that satisfies a function and that is provided with a longitudinal axis. The flange and the section are arranged at least substantially coaxially to the shaft part. The section is formed as a hollow cylinder that has notches extending in parallel with the longitudinal direction at at least one of its outer jacket surface and its inner jacket surface. The section has a diverging frustoconical shape that runs out at least substantially at the free end at the inner side of the section in the region of its free end and that serves for the widening of the section on the punching in the sheet metal part. A component assembly and a method of producing the latter is also claimed.

Abstract: In particular embodiments, a mission payload mounting apparatus comprises a pressurized door plug assembly on a side of an aircraft fuselage and a strut having a first end and a second end. The strut extends from an interior of the aircraft fuselage through the pressurized door plug assembly to an exterior of the aircraft fuselage. The strut is capable of being rotationally actuated about an axis exterior to the aircraft fuselage. The first end of the strut is connected to the interior of the aircraft fuselage. One or more payloads are attached to the strut between the axis and the second end.

Abstract: A clinching or swaging fastener for securely mounting a secondary article, such as a magnet, flush to a surrounding surface. An interference fit fastening feature holds the secondary article flush by using a deformable center knob on the end wall at the bottom of the retainer. Alignment features on the outer portion of the retainer body can fixture the magnet in a desired orientation. A radial flange surrounds the mouth of the bore which has a peripheral lip that extends upwardly. Clinch attachment means comprising a circular peripheral undercut is located on the outside of the body just below the flange for attaching the body to a host object. The article may have a peripheral chamfer at the top which receives the lip as it is deformed against the article to provide a flush alignment to the host object.

Abstract: A safety power assist for a manual press is provided. In another aspect, a press includes a tool, a manual actuator, a switch and an automatically powered actuator. A further aspect of the present press employs a spring which must be compressed beyond a predetermined pinching force before a switch is activated, where switch activation causes an automatically powered actuator to advance a workpiece-contacting punch or tool.

Abstract: A building support column includes a lower assembly with a connection bracket with a bottom plate and first and second connection blades extending away from the bottom plate in a first direction. A body includes plastic and defines an exterior perimeter about a plurality of support rods extending from the bottom plate. A center hole through the body is aligned with a hole through the bottom plate. An upper assembly includes a plurality of elongated layers of wood secured to each other along elongated faces of the layers of wood. The connection bracket secures the upper assembly to the lower assembly with a connection blade extending between the elongated faces of adjacent elongated layers of the supper assembly. A reinforcement plate with a plurality of teeth that extend away from a first side of the plate into a single elongated layer of the plurality of elongated layers.

Abstract: Particular embodiments include a non-dedicated, temporarily installed, airborne special mission payload mounting system comprising a pressurized door plug assembly installed in an opening on the side of an aircraft fuselage. A rotationally-actuated strut extends from a first end connected to an interior of the aircraft fuselage, through the pressurized door plug assembly, to a second end of the strut connected to one or more payloads. The rotational axis of the strut is exterior to the aircraft fuselage.

Abstract: A luminaire configured for mounting to a grid ceiling system includes first and second portions. The first portion includes a first housing, one or more first mating elements, and a light engine coupled with the first housing that generates light from electrical power, and is oriented to emit the light away from the first housing. The second portion includes a second housing and one or more second mating elements. The second mating elements are adapted to couple with the first mating elements. At least one of the first portion and the second portion includes an electrical receptacle for receiving the electrical power for the light engine. When the first mating elements couple with the second mating elements, the first housing and the second housing together define a cavity for one or more members of the grid ceiling system.

Abstract: In one embodiment, an apparatus includes a collapsible workstation assembly to be used in a temporarily-mounted control system of an aircraft. The collapsible workstation assembly is mounted to a floor of the aircraft via one or more mounting plates and one or more adaptive floor plates. The collapsible workstation assembly includes a number of modules for display and user controls. Each of the modules are connected via hinges and hinge locks to be moved between a deployed position for use and a stowed position when not in use. The collapsible workstation assembly is further connected to an observer chair assembly and a temporary door plug.

Abstract: The disclosed concrete anchor driver tool is coupled to a rotary hammer drill to install a concrete anchor. The tool includes a rod having multi-faceted bolt head end, such as a hexagonal bolt head end, and a socket having a multi-faceted opening in the socket end of the socket. The socket is slipped over the rod and held against the bolt head end of the rod by a compressible spring. The concrete anchor driver tool is operated by coupling the concrete anchor driver tool to a rotary hammer drill, slipping the socket over the concrete anchor, and operating the drill in the hammer mode to hammer the concrete anchor bolt into the concrete. The rotary hammer drill is then put in rotate mode and used to rotate the concrete anchor driver tool rod, which rotates the socket, which, in turn, tightens the nut on the concrete anchor.

Abstract: A spin fastening system includes a first member and an adhesive layer applied to the first member. A second member is positioned in contact with the adhesive layer. At least a portion of the adhesive layer is cured after the second member is positioned in contact with the adhesive layer to render at least the portion of the adhesive layer substantially rigid. At least one spin fastener is inserted successively through each of the second member, the cured portion of the adhesive layer, and the first member.

Abstract: A laminated composite part, which includes a first member having a predetermined mating surface, and a second member that is made of an elastically deformable resin material, that has a plate portion substantially parallel to the mating surface and having a multiplicity of protrusions formed integrally therewith so as to protrude toward the mating surface so that space is created between the plate portion and the mating surface, and that is placed on the first member such that the protrusions contact the mating surface, which has cushioning properties as tip ends of the protrusions are pressed against the mating surface and elastically deformed, and in which one of the first and second members which is located on a design surface side has an engaging projection that projects to a larger extent than the protrusions, and the engaging projection is inserted through an insertion hole formed in the other of the first and second members and is retained in the insertion hole, whereby the first and second members are

Abstract: A method of forming a coupling between a first part and a second part is disclosed. The method includes providing a first surface of the first part. The first surface has a first shape and a surface roughness average that is less than or equal to about 500 microinches (13 microns). The method also includes forming a second surface of the second part where the second surface has a second shape and the first shape and the second shape are substantially complementary shapes. Projections form at least a portion of the second surface in a preselected pattern, and are configured to produce a friction fit between the first surface and the second surface when the first surface and the second surface are biased against each other. The projections have an average elastic compressive range substantially equal to the surface roughness average.

Abstract: Particular embodiments include a non-dedicated, temporarily installed, airborne special mission payload mounting system which is mechanically interfaced to the Air Deployment System (ADS) rails of a host cargo aircraft. An Adaptive Mounting System (AMS) plate is placed over an ADS rail section and restrained in position. Once the AMS plate is secured, an articulated or fixed position strut can be attached to the AMS plate through the opened side doorway without removing the original door. A removable load transfer brace (LTB) can be coupled from the AMS plate inboard to the floor of the aircraft. The LTB is hinged to the AMS plate, and can be disconnected from the floor of the aircraft and rotated to a vertical position from the AMS plate.

Abstract: An impeller rotator (21) includes a turbine impeller (11), a compressor impeller (12), a shaft (13) connecting the turbine impeller (11) to the compressor impeller (12), and a connecting member (16) fastening one of the turbine impeller and the compressor impeller to one axial end region of the shaft, and the connecting member (16) is plastic-deformed so as to decrease overall imbalance of the turbine impeller (11), the compressor impeller (12), and the shaft (13).

Abstract: The present invention is directed to a method of preparing a blue-colored whiskey by mixing methylene blue, pure alcohol and distilled water. This process creates a staining solution and would allow the staining solution be aged in a cask prior to adding the whiskey into the cask. The stained cask colors the whiskey solution. This whiskey making method is designed to generate blue whiskey in which the color of the distillate is not directly altered. Further, this method provides a new way of presenting such beverages to potential customers in a pleasing way that could potentially enhance market share, and provides a new method to change beverages into new and unusual colors which may provide fun and additional marketing/branding opportunities.

Abstract: Disclosed herein is a method for assembling a module for a motor vehicle engine, which module comprises at least one supporting structure with bearing seats and at least one camshaft which is mounted rotatably in the bearing seats, the camshaft being constructed during the assembly of the module from a support shaft which is configured at least in sections as a hollow shaft and components which are to be connected to the support shaft at predefined joining positions. The method includes providing a supporting structure having bearing seats, positioning components to be affixed to a support shaft in a preliminary position with respect to the bearing seats, pushing the support shaft through the bearing seats and through-openings of the components, enlarging portions of the outer diameter of the support shaft at defined joining positions thereof, and axially moving the components on the support shaft onto the joining positions.

Abstract: A piercing nut element having a strength in the range between 700 and 900 MPa which is designed to be pressed into the sheet metal part. The nut element is characterized in that the self-piercing attachment of the nut element into a sheet metal part of higher strength, or into a sheet metal part with a thickness greater than 3.5 mm, the nut element is designed in such a way that the piercing section has a peripheral extending groove below the sheet metal contact surface and in that the piercing section has a piercing edge at its free end face with the piercing edge being spaced from the boundary of the groove adjacent to the piercing section by a peripheral surface having an axial height which corresponds to at least 30% and preferably to at least 50% of the sheet metal thickness, wherein the radial wall thickness of the piercing section in the region of its free end face from the outer side of the piercing section up to the nominal diameter of the thread corresponds to a thickness between 1.2 to 1.

Abstract: A system for preventing fluid from entering a walled structure includes a support structure configured for fixing to at least one surface of the walled structure; and a barrier apparatus attachable and anchorable to the support structure, the barrier apparatus including a fluid retention member configured for intercepting a fluid entering the walled structure, and a collar for holding the fluid retention member against an interior surface of the walled structure, proximate the opening. As fluid enters the barrier apparatus, the pressure increases against the interior surface of the fluid retention member, pressing it against the walled structure. The collar in combination with the fluid retention member to which it is attached acts like a gasket to tighten a seal between the barrier apparatus and the walled structure.

Abstract: A method for the manufacture of reinforced core composites, comprises: inserting of a pin into a foamed core material or a filled honeycomb-shaped core material, wherein the pin and the core material contain a thermoplastic polymer, or a mixture of thermoplastic polymers; the pin is heated such that as the pin is inserted the core material softens or melts at the point of insertion; and/or the core material is heated at the point of insertion such that the core material softens or melts.

Abstract: A coaxial assembly includes a first member, a second member, and at least two position members. The first member has an assembly hole with a sidewall. The second member having a lateral wall. The at least two position members are evenly arranged along a circumference of the lateral wall of the second member. The second member and assembly hole are configured such that when the second member is within the assembly hole, the at least two position members tightly abut the sidewall of the assembly hole, thereby causing the second member to be coaxial with the first member. An assembly method is also provided.

Abstract: In one embodiment, an apparatus includes a door plug assembly with a sonotube-launch system to be used in a temporarily-mounted control system for an aircraft. The door plug assembly is built from one or more panels designed to fit an opening in the fuselage of the aircraft, the opening being created by the removal of a door on the side of the fuselage. The door plug assembly includes a segmented bubble window with transparent glazing, with a kick panel on the lower portion of the bubble. The door plug assembly further includes a door strut indent which allows a strut to extend from the interior of the aircraft through the indent to the exterior of the aircraft. When a strut is not being used, a close-out panel is secured to the door plug assembly to allow the interior of the aircraft to be pressurized.

Abstract: A metal insert having a body at a base diameter, a plurality of retention regions spaced apart and extending radially from the body, and an end effector at one end, for engaging a mating member. Each retention region consists of a circumferential series of alternating prongs and recesses. The insert is manufactured by selecting or processing a solid raw bar to produce an engineered rod having a plurality of axially continuous protrusions at a protrusion diameter alternating circumferentially with a plurality of axially continuous channels at a channel diameter. At axial intervals, the diameter of the engineered rod is decreased with a form tool to a base diameter smaller than the channel diameter, thereby producing a featured rod having a series of axially alternating spacer regions at the base diameter and radially outwardly extending feature regions consisting of a circumferential series of alternating prongs and recesses.

Abstract: Various devices and methods for breaking and retaining surgical reduction tabs are provided. In general, the devices and methods can allow a single surgical instrument to break a plurality of surgical reduction tabs off one or more surgical implants and retain the broken tabs within the instrument. In an exemplary embodiment, a surgical instrument can include an opening at a distal end thereof that is configured to receive a surgical reduction tab therein when the tab is connected to a surgical implant. A retention element at least partially disposed within the instrument can be configured to engage the tab received in the opening so as to hold the tab securely within the instrument. With the tab received in the opening and held by the retention element, the surgical instrument can be configured to be manipulated to break the tab off the surgical implant. The broken tab can be retained within the surgical instrument by being held therein by the retention element.

Abstract: A recessed head screw includes a shank, a head, a drilling portion and threads. The head includes a top face where a socket portion is formed. The socket portion has a driving recess and a driving socket formed between the driving recess and the top face. The driving socket communicates with the driving recess. A diameter value of the driving socket is a maximum circumscribed circle diameter value of the driving recess plus a value within 20% of the maximum circumscribed circle diameter value. When a driving tool engages the socket portion, the driving socket can be in close-fitting engagement with the driving tool to increase the engagement between the driving tool and the head and prevent the screw from falling off the tool easily during the driving action of the tool, thereby delivering a full driving force to the head to improve the working efficiency and smoothness.

Abstract: In one embodiment, a temporarily-mounted control system is installed in an aircraft. The temporarily-mounted control system includes a temporary door plug assembly that is adapted to in an opening in a fuselage of the aircraft, such as an opening created by removing a door in the fuselage. The temporary door plug is connected to a retraction rail assembly that connects the temporary door plug and the fuselage. One or more workstation assemblies is mounted to the floor of the aircraft using mounting plates that are attached to adaptive floor plates connected to the floor of the aircraft. An observer chair assembly is connected to the floor of the aircraft and to the workstation assemblies.

Abstract: A drywall brace and system or method for using the same can include a body including a length L, a width W, and a thickness T. The body can include a first surface defined by a first plane comprising the length L and width W, a second surface opposite the first surface, and a first end sharpened to a point adapted to form an opening through drywall. A mounting aperture can be formed completely through a central portion of the body and be sized to receive a threaded bolt for mounting a device. A first portion and second portion of flexible line can be coupled within 3 centimeters (cm) of the mounting aperture. An adhesive can be coupled to the first surface of the body and covered with a removable adhesive protective layer. A cleaning pad can be coupled to the second surface of the body.

Abstract: Particular embodiments include a non-dedicated, temporarily installed, airborne special mission payload mounting system which is mechanically interfaced to the Air Deployment System (ADS) rails of a host cargo aircraft. An Adaptive Mounting Plate (AMP) is placed over an ADS rail section and restrained in position. Once the AMP is secured, an articulated or fixed position strut can be attached to the AMP through the opened side doorway without removing the original door. Once the strut is secured to the AMP, a one-piece or segmented two-piece pressurized door plug is installed within the vacant doorway above the strut providing an airtight seal and thereby permitting pressurization of the aircraft. The mission payload mounting system can be housed in a strut transport and alignment case which is temporarily attached to the floor of the aircraft during installation of the system, then removed.

Abstract: A gear unit for an actuating drive, in particular a window lifter drive, of a motor vehicle is provided that includes a gear housing and a pivot bolt rotatably fixedly connected thereto for rotatably supporting a gear wheel, in particular of a worm gear, the pivot bolt has a second pivot section, which is adjacent to a first pivot section having a first outer diameter, and which has a free end section on the front, the outer diameter of the second pivot section being smaller than the outer diameter of the first pivot section at least over one part of it pivot section length.

Abstract: Various devices and methods for breaking and retaining surgical reduction tabs are provided. In general, the devices and methods can allow a single surgical instrument to break a plurality of surgical reduction tabs off one or more surgical implants and retain the broken tabs within the instrument. In an exemplary embodiment, a surgical instrument can include an opening at a distal end thereof that is configured to receive a surgical reduction tab therein when the tab is connected to a surgical implant. A retention element at least partially disposed within the instrument can be configured to engage the tab received in the opening so as to hold the tab securely within the instrument. With the tab received in the opening and held by the retention element, the surgical instrument can be configured to be manipulated to break the tab off the surgical implant. The broken tab can be retained within the surgical instrument by being held therein by the retention element.

Abstract: In one embodiment, a non-dedicated, temporarily-installed, aircraft observer bubble door, chair, sonotube ejection system, mission electronics LRU rack and workstation assembly are affixed to a host aircraft, thereby precluding the requirement for dedicated airframe modifications. One embodiment of the present invention also utilizes a multi-axis, articulated, foldable chair temporarily-installed in conjunction with a segmented or one piece pressurized observer bubble door plug and door retraction system. Once installed the subject apparatus can be stowed outboard of the fuselage cargo transit envelope to permit use of the ADS rail system in-flight, without affecting normal air drop operations, crew egress, the flight performance envelope, or emergency procedures of the host aircraft.

Abstract: There is provided a joined body in which two or more members Yi including a fitting hole are fastened, in which a fastening rod including reinforcing fibers and a thermoplastic resin is positioned in the fitting hole, the fastening rod is caulked by heat, and the members Yi are caulking-fastened.

Abstract: In one aspect of the invention, a clip nut for shaft assembly having a tubular shaft is provided. The clip nut includes a first end having a first aperture, a second end having an inwardly extending projection portion with a second aperture extending therethrough, and a connecting portion extending between the first end and the second end. The first and second ends are configured to extend around the tubular shaft such that the projection portion extends into the tubular shaft, and the first and second apertures are configured to receive a fastener to couple the clip nut to the tubular shaft.

Abstract: A wheel spindle drive element for a wheel disconnect system. The wheel spindle assembling onto an outer diameter of a spindle, displacing material to form a joint with high torque transmission characteristics.

Abstract: A scroll compressor that includes a housing and scroll compressor bodies disposed in the housing. A motor is disposed within the housing and operably connected to a drive shaft for driving one of the scroll compressor bodies. The drive shaft is rotationally supported at one end by a crankcase which includes a bearing housing and a bearing. The crankcase includes a plurality of openings or gas passages passing through the crankcase, as well as a plurality of generally cylindrical sections positioned respectively between adjacent openings. The cylindrical sections define contact regions which can engage an inner periphery of the housing when the crankcase is mounted therein.