44results about How to "Minimizing volume" patented technology

A polyphase electrosurgical system and method are provided. In embodiments, a radiofrequency generator having the capability of delivering a plurality of independent electrosurgical signals is disclosed. An electrosurgical instrument having an array of electrodes that correspond to the plurality of signals may be used to deliver the electrosurgical signals to tissue. In embodiments, three RF signals having a phase offset of about 120° therebetween, i.e., a three-phase configuration, may be used to achieve a balanced delivery of electrosurgical energy, which may lead to increased rates of energy delivery, improved control of tissue ablation regions, and improved operative outcomes. The phase, amplitude, and / or frequency of each signal may be independently variable in response to user inputs and / or biological parameters such as tissue impedance or return electrode current.

An airbag configuration for braking the landing impact of flying payloads has a central airbag (17) and at least one torus ring (11, 12, 13) surrounding the central airbag. A payload (L) is attachable on the central airbag (17). A stabilizing device (19) is provided which extends from the lowermost portion of the at least one torus ring (11, 12, 13) to the central airbag (17). The central airbag provides primarily vertical braking of the landing impact while the torus ring provides primarily horizontal braking of the landing impact.

Disclosed herein is a washing machine which has a detergent supply part formed in a door. The detergent supply part is formed in the door and has a function of containing detergent and supplying detergent into a tub through the door. The washing machine has an advantage of considerable space saving compared with the washing machine having the detergent supply part formed in an inner space thereof, thereby minimizing the volume and the number of components of the washing machine.

An optical coherent receiver in one embodiment has a heterodyne configuration, and in another embodiment has a homodyne configuration, in each configuration employs multiple feedback signaling and analog / digital processing to optimize response to a modulated optical input signal, the provision of both individual RF I and RF Q channel outputs.

A self-charging organic electroluminescent display is disclosed. A solar cell and an organic electroluminescent device are installed on a same substrate or different substrates. Using the photoelectric conversion property of the solar cell, the solar energy is converted into electrical energy and stored in a battery. Therefore, the electrical energy converted from the solar energy can be provided for the organic electroluminescent device to emit light, forming a self-charging organic electroluminescent display module.

An insert comprising a lightweight structure configured for filling the gaps between axially spaced C-shaped lamination stacks and circumferentially spaced non-magnetic cradles on a permanent magnet rotor. The insert is secured to a rib by a dovetail tongue that fits within a dovetail groove provided along the length of each rib. The insert engages the adjacent cradles and has a circumferential surface that has the same radius of curvature as the top surface of the cradles.

A novel loop antenna containing a thin-walled ferrite box or other hollow; magnetic core structure of high permeability (considerably greater than 100), particularly useful for crossed loop antennas, and of optimal geometry and configuration for minimum volume, weight and space.

The blurring determination device references image data in which are recorded coefficients that are obtained when pixel values forming the image in the spatial domain are converted to the frequency domain, and detects edges oriented in two or more directions, from among the image data, by comparing a series of the coefficients in each of the directions with various types of basic edge patterns whereby typical gradient patterns of the changes in pixel values are represented by values corresponding the coefficients. The representative values of the width of the detected edges is determined in each of the directions, and the image data is determined to not be blurred when the representative values meet the condition of being at or below a certain threshold.

An acoustic assembly including a thin sound absorbing panel supported by foldable mounting brackets is adapted to be mounted upon the walls of an indoor listening enclosure. The space behind the panel functions as an acoustic diffusion chamber which augments the acoustic performance of the panel. A number of such assemblies are employed in a manner such that the panels are offset from the wall and downwardly angled.

A dolly on which a grand piano can be mounted to facilitate movement thereof over a surface from one location to another, which includes a central hub shaped in the form of a miniature grand piano, two fixed length arms of equal length pivotally connected to the front of the hub at opposite corners thereof, and a fixed length rear arm having a longitudinal slot which is pivotally connected to the rear of the hub at selectively adjustable positions along the length of the slot to accommodate grand pianos having a range of different lengths.

The stimulated Brillouin scattering optical amplifier includes a first control optics assembly, a driver element, a second control optics assembly, a Brillouin active medium, and egressing optics. The first control optics assembly receives an incoming laser beam and adjusts that incoming laser beam in accordance with first desired wavelength, polarization and beam propagation parameters. A driver element produces a driver laser beam. A second control optics assembly receives the driver laser beam and adjusts that driver laser beam in accordance with second desired wavelength, polarization and beam propagation parameters. A Brillouin active medium receives an output from the first control optics assembly and an output from the second control optics assembly. The Brillouin active medium provides a non-linear optical interaction between the outputs such that the incoming laser beam is amplified producing an amplified Brillouin active medium output laser beam and a depleted driver laser beam. Egressing optics receives the amplified Brillouin active medium output laser beam and the depleted driver laser beam. The egressing optics controllably transmits the amplified Brillouin active medium output laser beam in accordance with third desired wavelength, polarization, and beam propagation parameters and prevents transmission of the depleted driver laser beam. The output of the egressing optics includes an amplified egressing optics output laser beam.

A hybrid kinetic energy rod warhead includes a projectile core including a plurality of projectiles, explosive segments about the projectile core, and isolators between the explosive segments. There is an initiator for each explosive segment and a shell about the explosive segments. A deployable casing including multiple fragment members is attached to the shell, and there is a housing about the deployable casing.

The present invention is directed to improved designs and methods for improving engine fuel efficiency by providing two-stage engine variable compression in running engines using connecting rod force reversals to rotate eccentric bushings to change the connecting rod length. Compression ratio changes are initiated by shifting a block-mounted cam such that it engages and flips a bi-stable toggle on the connecting rod. The clutch mechanism latches the eccentric at the eccentric rotation end point, whereupon the connecting rod acts as a rigid rod. The invention includes novel configurations of the lubricated journal bearing between the connecting rod and the eccentric that modify the squeeze film bearing effects and resulting friction. These configurations reduce the peak eccentric torque carried by the clutch mechanism while facilitating eccentric rotation at lower torque.

A containment vessel having a spiral plate heat exchanger, a central catalyst chamber packed with particulate catalyst, a central heater, a plenum providing conductive flow access for a hydrocarbon-air mixture to and from the containment vessel interior, and essential flow pathways interconnecting the plenum section, heat exchanger, catalyst chamber and central heater. The spiral plate heat exchanger, catalyst chamber, and heater assembly occupy successively smaller annular regions within the containment vessel.

An apparatus for ejecting a flying body such as a payload recovery container from a spacecraft includes a first ring to be releasably engaged with the flying body, a second ring to be secured to the spacecraft, and tension cables extending between and interconnecting the two rings. Cable winding devices mounted on at least one of the rings are spring-biased to wind-up the cables. The flying body is inserted through the open inner diameter of the second ring, and the first ring is separated from and rotated relative to the second ring, so that the cables extend helically along the outer circumference of the flying body. Holding and guide elements on the second ring hold and guide the flying body. When the holding elements are released, the cables are retracted by the cable winding devices, whereby the flying body is rotated and translationally ejected through the second ring.

The device employs a plurality of coefficients recorded in image data to detect whether edges are included per block, and determines as the blur level the proportion of edges, among the detected edges, in which the edge width is over a certain threshold. The device also determines, per block, coordinates composed of a first coefficient value representing frequency components in a first direction in the blocks and a second coefficient value representing frequency components in a second direction perpendicular to the first direction, and calculates the extent of bias in the distribution of the coordinates as the ellipticity. The device determines whether or not blurring has been produced by camera shake in an image based on the relationship between the blur level and ellipticity which have thus been determined.

An insert comprising a lightweight structure configured for filling the gaps between axially spaced C-shaped lamination stacks and circumferentially spaced non-magnetic cradles on a permanent magnet rotor. The insert is secured to a rib by a dovetail tongue that fits within a dovetail groove provided along the length of each rib. The insert engages the adjacent cradles and has a circumferential surface that has the same radius of curvature as the top surface of the cradles.

A secondary battery includes an electrode assembly; a collecting plate electrically coupled to the electrode assembly and having a short circuit hole; a short circuit member comprising a metal can, wherein the metal can is in the short circuit hole; a case accommodating the electrode assembly and the collecting plate and having an opening; and a cap assembly comprising a cap plate sealing the opening of the case.

The stimulated polariton scattering optical amplifier includes a first control optics assembly, a driver element, a second control optics assembly, a polariton active medium and egressing optics. The first control optics assembly receives an incoming laser beam and adjusts that incoming laser beam in accordance with first desired wavelength, polarization and beam propagation parameters. A driver element produces a driver laser beam. A second control optics assembly receives the driver laser beam and adjusts that driver laser beam in accordance with second desired wavelength, polarization and beam propagation parameters. A polariton active medium receives an output from the first control optics assembly and an output from the second control optics assembly. The polariton active medium provides a non-linear optical interaction between the outputs such that the incoming laser beam is amplified, producing an amplified polariton active medium output laser beam and a depleted driver laser beam. Egressing optics receives the amplified polariton active medium output laser beam and the depleted driver laser beam. The egressing optics controllably transmits the amplified polariton active medium output laser beam in accordance with third desired wavelength, polarization, and beam propagation parameters and prevents transmission of the depleted driver laser beam. The output of the egressing optics includes an amplified egressing optics output laser beam.

A method of treating hydroxide alkaline waste and by-products to render the material neutralized or reduced in pH from near 14 to a minimum lower limit of about 5.3 based on aluminum poly cation salts, rendering the waste or by-product stream suitable for ultimate disposal or reuse. The method comprises contacting together a mixture of moderate to high alkaline waste or by-product material with a pH in the range of 7.5-14, with sufficient water added or found within the alkaline material, with one or more poly cationic salts in the dry form taken from a group of salts containing tri-valent aluminum, tri-valent iron, di-valent calcium, di-valent magnesium, di-valent manganese, di-valent zinc, or any polyvalent cationic salt that is soluble in water to a minimum extent of 0.5 grams per 100 milliliters of water at near 0° Centigrade and 2 grams per 100 milliliters of water at near 100° Centigrade, in such a way to cause these materials to interact in a double replacement reaction to form a soluble salt reaction by-product and an insoluble hydroxide precipitate with water solubility characteristics, between 0° Centigrade and 100° Centigrade, equal to or exceeding that of CaS04*2H2O (gypsum) or approximately 0.20 grams per 100 milliliters of water. The added salts) may be dry or made up of a brine or dilute salt solution of the chosen salt or salts from the set of poly cation salts suitable to reduce hydroxide alkalinity in waste and by-product materials causing the pH to drop immediately upon thorough mixing of the poly cation salts and the waste / product materials, resulting in a treated waste / by-product stream / that is suitable for ultimate disposal or re-use.

The present invention comprises an apparatus and method for efficiently venting impurities from a heat recovery steam generator system by concentrating the impurities in a condensing deaerating vent line 40 and then venting a proportionately small amount of steam with a proportionately high concentration of impurities. The condensing deaerating vent line 40 is attached to a low pressure drum 10, and feed water 54 may be added to the upper portion of the condensing deaerating vent line 40 to improve condensation and conserve thermal energy.

An apparatus for ejecting a flying body (e.g. payload recovery container) from a spacecraft includes a first ring to be secured to the spacecraft, a cable winding device that is arranged on a second ring and that is releasably engageable with the flying body, and tension cables extending between the two rings. The cable winding device is spring-biased to wind-up the cables, which extend axis-parallel along the cylindrical outer shell of the flying body. Holding and guide elements on the first ring hold and guide the flying body. Catch elements on the cable winding device releasably engage receivers on the flying body. When the holding elements are released, the cables are retracted by the cable winding device, and the rotation of the cable winding device is transmitted to the flying body via the engaged catch elements and receivers. Thereby, the flying body is rotated and translationally ejected.

A dolly on which a grand piano can be mounted to facilitate movement thereof over a surface from one location to another, which includes a central hub shaped in the form of a miniature grand piano, two fixed length arms of equal length pivotally connected to the front of the hub at opposite corners thereof, and a fixed length rear arm having a longitudinal slot which is pivotally connected to the rear of the hub at selectively adjustable positions along the length of the slot to accommodate grand pianos having a range of different lengths.

An apparatus for ejecting a flying body (e.g. payload recovery container) from a spacecraft includes a first ring to be secured to the spacecraft, a cable winding device that is arranged on a second ring and that is releasably engageable with the flying body, and tension cables extending between the two rings. The cable winding device is spring-biased to wind-up the cables, which extend axis-parallel along the cylindrical outer shell of the flying body. Holding and guide elements on the first ring hold and guide the flying body. Catch elements on the cable winding device releasably engage receivers on the flying body. When the holding elements are released, the cables are retracted by the cable winding device, and the rotation of the cable winding device is transmitted to the flying body via the engaged catch elements and receivers. Thereby, the flying body is rotated and translationally ejected.