213 results about "Angular sector" patented technology

The invention relates to a cooking vessel for cooking food under pressure, said vessel comprising: a cooking bowl (2), a lid (3), and locking means (5); and support means disposed between the lid (3) and the locking means (5); said cooking vessel being characterized in that: firstly, the lid (3) and the bowl (2) are shaped so that the lid (3) penetrates into the bowl (2) so as to form an “internal-mount” lid; and secondly, the support means subdivide the lid (3) into one or more fixed angular sectors (3F), and one or more free angular sectors, said support means and the lid (3) being dimensioned in a manner such as to enable the free sector(s) of the lid (3) to be deformed in controlled manner under the effect of the pressure prevailing in the bowl (2). A cooking vessel for cooking food under pressure.

This system accompanies the alarms of TAWS type and in particular the alarms of “Avoid terrain” type indicating to the pilot that he has passed the limit point of success of a standard vertical avoidance maneuver, indications (32, 33) of free-travel distances in azimuth sectors suited to a clearance maneuver and one or more recommended relief avoidance maneuvers (A, B), both lateral and vertical. For the determination of the limit point, it monitors the penetration of a model of the terrain being flown over into a first protection volume (1) linked to the aircraft and configured in such a way as to model a standard vertical avoidance maneuver trajectory executed without notable delay. For the determination of the azimuth sectors open to a clearance maneuver, it analyzes the penetrations of the model of terrain being flown over in a second protection volume with large azimuth aperture, linked to the aircraft and configured in such a way as to contain the limit point protection volume (1). To evaluate the free-travel distances, it searches for limit points of effectiveness of a standard vertical avoidance maneuver, on arbitrary distancing trajectories in the azimuth sectors open to the clearance maneuvers. Based on the determination of these free-travel distances, the system determines the limit instant of manual initiation by the pilot or automatic initiation of an avoidance trajectory and determines the optimum route alteration to be initiated prior to the avoidance maneuver.

A method and apparatus is provided for automatically classifying a defect on the surface of a semiconductor wafer into one of, e.g., seven core classes: a missing pattern on the surface, an extra pattern on the surface, a deformed pattern on the surface, a particle on the surface, a particle embedded in the surface, a particle and a deformed pattern on the surface, or craters and microscratches on the surface. The defect may also be further classified into a subclass of arbitrarily defined defects defined by the user or preprogrammed in the apparatus. Embodiments include using a scanning electron microscope (SEM) capable of collecting electrons emitted from a plurality of angular sectors to obtain an image of the defect and a reference image containing topographical and location information, then analyzing this information to classify the defect. As the defects are classified, counts are maintained of the number of occurrences of each type of defect, and an alarm is raised if the defect count in a particular class exceeds a predetermined level. Thus, defects are accurately and reliably classified and monitored to enable early detection and cure of processing problems.

A base station for a cellular telecommunications network is arranged to support a plurality of angular sectors. Each sector has a single dual column antenna, or two single column antennas, and each column is dual polarized such that each element in each column has a correspondingly polarized element in the other column. Thus the two pairs of correspondingly polarized elements form a phased array pair which is steerable together to form a narrow compound sector beam and steerable apart to form a wide compound sector beam.

A method for defining an isolation area around an object of interest in a cell culture vessel, the method comprising the steps of: obtaining one or more images of the cell culture vessel using one or more of a plurality of illumination sources, each illumination source being capable of illuminating the vessel from a different direction; selecting an image or combination of images for further processing; applying a circular object detection transformation to identify one or more objects of interest being substantially circular objects in the cell culture vessel, which circular objects of interest are representative of isolated colonies in the cell culture vessel and determining the center of an object of interest; applying a binarizing step to obtain a binarized image of the object of interest and other objects, wherein the center of the binarized image corresponds to the center of the object of interest; iteratively forming concentric circles with increasing radius, wherein the concentric circles are centered on the center of the binarized image; identifying coronas, wherein a corona is delimited by two circles having successive radius values; for each corona: determining the presence and the location of any other object located in the corona to determine the presence and the location of other objects; determining a clearance angle defining an angular sector free of other objects around the object of interest to define the isolation area around the object of interest.

The ingress to and egress from an access restricted compartment, such as the cockpit in an aircraft, is controlled by a revolving gate (1) rotatably mounted in a stationary gate frame (2). The revolving gate (1) has a single gate opening (11) and is rotatable about its central longitudinal axis through predetermined or preselected angular sectors to bring the gate opening (11) either into alignment with any one opening (21) of at least two frame openings (21) at a time, to provide ingress or egress, or to cause said single gate opening (11) to face a wall (2A) of said stationary gate frame (2) or a closed door (51) in said stationary gate frame (2) to close the gate (1). In the closed position of the gate (1) escape from the gate (1) is prevented by locking the gate in its closed position by at least one arresting bolt that is electrically controllable, preferably from the cockpit. The atmosphere in the revolving gate (1) is controllable, preferably also from the cockpit, for incapacitating any unauthorized intruder.

Clutch mechanism for locks, which is composed of an interior axis (1), an exterior axis (2), a static body (3), a radial pin (4), a radial catch (5) and a radial actuator (6); said interior (1) and exterior (2) axes and body (3) compose a coaxial assembly where the exterior axis (2) penetrates the interior axis (1) and both are installed with a rotational adjustment in the static body (3), the set of radial pin (4) and radial catch (5) is installed between the actuator (6) and a radial spring (7) which acts between the catch (5) and the base of the housing (2a) of the exterior axis (2); whose pin (4) and catch (5) are dimensioned in such a way that each will be able to be moved between the circumferences of the exterior diameter of the axis (2) and the interior diameter of the axis (1); the radial actuator (6) is composed of a curved plate (6a) and by, at least, one rod (6b), whose plate (6a) is located in an annular depression (8) between the interior axis (1) and static body (3), extending in a circumferential arc containing the angular sector corresponding to the operative rotational transit of the interior axis (1).

For a bearing mounted between two concentric races rotating relative to each other, and forming an annular gap that accommodates the bearing and is closed by seals, at least one grease tube is provided between the periphery of one of the two races and the annular gap, and is connected to a corresponding grease reservoir. At least one main grease tube opens into the annular gap in an angular sector where an overpressure occurs, a corresponding main grease reservoir is adapted to collect grease flowing from the annular gap through the main grease tube due to the overpressure that may occur within the annular gap in the angular sector.

A supersonic externally pressurized inlet comprising a generally scoop-shaped supersonic pressurized portion for diffusing a supersonic free jet. The supersonic pressurization portion includes a main wall having a leading edge and a throat downstream of the leading edge; and sides joined to opposed side edges of the main wall to form a generally scoop-shaped member. The sides preferably protrude far enough into the supersonic flow to encompass the initial oblique shock attached to the leading edge of the main wall. The main wall has an inner surface generally formed as an inclined sector of the surface of revolution, the inner surface of the main wall cooperating with the inner surfaces of the sides to form a three-dimensional external pressurized surface. The supersonic external pressurization inlet also includes a subsonic diffuser section arranged to receive airflow from the supersonic pressurization section and diffuse the airflow to subsonic conditions. The variable geometry inlet includes an outer ramp hinged about its forward edge and forming part of the inner surface of the spoon diffuser, the pivotal movement of the outer ramp being used to vary the throat size of the inlet. The subsonic diffuser includes an inner ramp hinged around its trailing edge to maintain a smooth transition from the outer ramp.

Embodiments of the invention relate to beamforming antennas such as can be used in space division multiplexing systems. Space division multiplexing can be used to increase data capacity in wireless networks by enabling different base stations to transmit signals within the same frequency band. Each antenna beam can potentially be used to establish a communication link within an area of wireless coverage, and other communication links established on other antenna beams then represent interference to that user. In order to reduce interference, narrow beamwidths are desirable. These are typically achieved by increasing the aperture of the antenna in the azimuth plane, and in arrangements that require finely divided angular sectors, a greater number of antennas will be required to give three hundred and sixty degree coverage. As a result, there is potentially a large increase in the total surface area of antennas which is undesirable, as it leads to increased wind loading of an antenna tower. Embodiments of the invention provide an arrangement in which data are transmitted from a first transmitter to a first receiver using a first antenna beam, and data are transmitted from a second transmitter to a second receiver using a second antenna beam. The first antenna beam is formed by splitting the signal from the first transmitter into two parts with a first phase relationship between the parts, each part being connected to an antenna. A second antenna beam is formed by splitting the signal from the second transmitter into two parts with a second phase relationship between the parts, each part being connected to one of the two antennas. An advantage of embodiments of the invention is that data can be transmitted from different transmitters at the same frequency without interference, while presenting a smaller antenna aperture than is required with conventional systems.

A turbine (40) for a turbocharger (10) has a turbine housing (41) defining a generally annular chamber (43) surrounding a turbine wheel (44), the chamber receiving exhaust gas for driving the turbine wheel. The chamber has dividing walls (46) that divide the chamber into a plurality of angular sectors (43a,43b), each fed with exhaust gas separately from the other sector(s). (52,53) located radially inwardly of the sectors for guiding flow into the turbine wheel include at least dividing vanes (52) that form extensions of the dividing walls (46) so as to extend the sector-division of the exhaust gas flow path all the way to the trailing edges of the dividing vanes. An axially slidable piston (48) is disposed radially inwardly of the sectors, and radially overlaps with the dividing vanes (52). The vanes either are mounted on fixed structure and are received in slots (49) in the piston, or are mounted on the piston and received in slots in fixed structure.

A stator suitable for high-pressure compressors in gas turbine engines includes two points of ventilation at different temperatures. It is recommended that the upstream section of the stator be constructed with a casing and a shroud, both of which are unbroken around a circumference and made of a material with a low degree of thermal expansion. Downstream the shroud is, however, constructed using angular sectors in a material with a higher degree of thermal expansion.

Methods for processing ultrasonic signal data to evaluate subsurface properties and tool orientation. Acoustic signals are transmitted into a plurality of azimuthal borehole positions. Formation echo signal transit time distributions are then determined in a plurality of azimuthal sectors for the acoustic signals. Front face echo signal transit times are also measured and farther-mode and closer-mode transit times are determined for the distribution of formation echo signals. Farther and closer tool standoffs are determined for the azimuthal sectors and a borehole diameter is determined from a summation including standoffs in opposing sectors. The standoffs are also used to determine a preferential tool position.

A method for determining duty-cycles of respective pulse width modulated (PWM), space vector modulated (SVM) control signals of an inverter, may include storing values of the duty-cycles as a function of a position of the multi-phase electric load in a look-up table. The method also may include determining a phasor angle representing applied sinusoidal voltages. The method also may include determining the duty-cycles as a function of the angle, and storing, in the look-up table, values of two pre-established waveforms relative to at least one duty-cycle as a function of the angle in at least two 60° degree angular sectors, by at least, identifying which of six 60° angular sectors the angle belongs, calculating a difference between the angle and an angular sector lower bound, and generating values as a function of the identified angular sector of the difference and the two pre-established waveforms stored in the look-up table.

A logging-while-drilling density sensor includes a gamma ray source and at least two NaI detectors spaced apart from the source for determining measurements indicative of the formation density. A magnetometer on the drill collar measures the relative azimuth of the NaI detectors. Measurements made by the detectors are partitioned into bins defined by azimuth. A compensated bulk density is determined for selected ones of said azimuthal sectors that meet a threshold test related to a minimum difference of measurements or a minimum correction. The method of the invention may also be used with neutron porosity logging devices.

An inductive sensor includes a primary winding, two secondary windings and a moveable target, the primary winding being centered about a central axis and carrying a high-frequency alternating current which can induce a voltage in secondary windings, the secondary windings also being centered about the central axis and made up of a number k of substantially identical loops, which are successively crossed and arranged opposite the primary winding. In this case, the target is made up of a part having p=1 angular sector with an angular opening. The opening of the angular sector of the target is less than that of a loop of secondary winding with a deviation calculated such as to eliminate the fourth harmonic of the linearity deviation Fourier decomposition, between the measured angular value and real angular value for the position of the target over the measurement course.

A phased array antenna is designed for scanning a narrow beam over an angular sector that is wide in one plane, and narrow in another, while using a minimum number of phase steering controls. High directivity elements occupy a rectangularly shaped area which is large in one direction relative to a second direction, the elements being staggered in position with neighboring elements to suppress near-in grating lobes. The elements are independent and identical to one another so that conventional array beamforming techniques may be utilized.

The ingress to and egress from an access restricted compartment, such as the cockpit in an aircraft, is controlled by a revolving gate (1) rotatably mounted in a stationary gate frame (2). The revolving gate (1) has a single gate opening (11) and is rotatable about its central longitudinal axis through predetermined or preselected angular sectors to bring the gate opening (11) either into alignment with any one opening (21) of at least two frame openings (21) at a time, to provide ingress or egress, or to cause said single gate opening (11) to face a wall (2A) of said stationary gate frame (2) or a closed door (51) in said stationary gate frame (2) to close the gate (1). In the closed position of the gate (1) escape from the gate (1) is prevented by locking the gate in its closed position by at least one arresting bolt that is electrically controllable. The atmosphere in the revolving gate (1) is also controllable for incapacitating any unauthorized intruder.

There is provided a method, including obtaining, by a network apparatus, antenna sensing information with respect to signals received by a base station operating under a shared access-system which allows a licensee system to apply at least a part of an shared access spectrum which is currently unused by an incumbent system; detecting, on the basis of the antenna sensing information, that at least one device of the incumbent system is communicating on the shared access spectrum in the coverage area of the base station; identifying the angular sector in which the device of the incumbent system is located with respect to the base station; and dynamically isolating the identified angular sector from usage by the licensee system.

In the method, a support is provided that presents a base for an annular wiper, and a wiper is built up that presents height that varies around its circumference, by forming a plurality of projecting portions by performing following successive steps: a laser source connected to an optical head focused on a point on the top surface of the base is activated, as is a source of powder connected to the spray nozzle, thereby forming a localized melt at said point, into which the powder is injected, thus forming a localized region of extra thickness; and the optical head and the nozzle are aimed at another point adjacent to said region of extra thickness and the method returns to the preceding step until the layer of material is completed in the angular sector in question.

The object of the invention is a process for detecting latent flatness defects in a band product (2) applied under tensile load to an angular sector (A) of measuring roll (1) comprising a plurality of detection zones (4) spaced apart each comprising a transmission sensor (3), at each rotation, of a measurement signal having a value under load (i) which is compared, at each rotation, with a reference value, in order to assess, in each longitudinal zone of the band (2), information representative of the tensile load applied in this zone. According to the invention, two values in empty condition (i1, i2) of the signal transmitted by each sensor (3) are measured, respectively before and after the corresponding detection zone passes through the angular application sector (A) of the band and the reference value (i0) to which is compared, at each rotation, the value under load (i) of the signal transmitted by each sensor is obtained by combination of said values in empty condition, respectively preceding (i1) and subsequent (i2).

A method for determining a total mechanical load of a wind turbine is provided. A present load signal indicative of a present load of a wind turbine base structure is obtained, wherein the present load acts in a present angular direction. A first present load and a second present load are derived based upon the present load signal and the present angular direction, wherein the first present load is associated with a first angular sector of the turbine and the second present load is associated with a second angular sector of the turbine. Further, a total mechanical load is derived based upon the first present load and the second present load.

A circular needling table for needling a textile structure made from an annular fiber preform, the table including: a horizontal annular platen for having the annular fiber preform placed thereon; drive means for driving the fiber preform in rotation about the axis of the platen; a needling device having a needling head extending over an angular sector of the platen and driven in vertical motion relative to the platen; and guide means for guiding the fiber preform under the needling head.

The invention provides a circular needling table (10) for needling a textile structure made from an annular fiber preform, wherein the table comprises: a horizontal annular platen (14) for having the annular fiber preform (12) placed thereon; drive means for driving the fiber preform in rotation about the axis (16) of the platen; a needling device (22) having a needling head (24) extending over an angular sector of the platen and driven in vertical motion relative to the platen; and guide means (38a, 38b) for guiding the fiber preform under the needling head.

A stator angular sector for a turbine engine compressor including: an outer shroud and an inner shroud, and at least one vane extending radially between the shrouds. The outer shroud includes first and second mounting mechanisms for mounting the stator angular sector on a casing of the engine, which mechanisms are oriented parallel to the axis in opposite directions and connected together by an intermediate portion. The outer shroud includes at least one axial end portion extending from the intermediate portion with which at least one damper-forming insert is configured to come into contact, such that beyond a given value for amplitude of vibration of the end portion, the damper insert and the end portion are configured to move relative to each other to vary total moving mass moving with the end portion, thereby modifying vibratory behavior of the end portion.

A device for winding automatic watches, including an electrical energy source and a receptacle support including a surface configured to receive in abutment a back cover of a watch, the device configured to generate a magnetic and / or electrostatic field or eddy currents, in a fixed position underneath the bearing surface and generate, on a substantially annular angular sector, a magnetic and or electrostatic field that varies as a function of time and whose direction is orthogonal to the bearing surface, or generating eddy currents that vary as a function of time. The device can be provided for a watch including an automatic winding mechanism with an oscillating weight including a first ferromagnetic inner part and a second heavy metal peripheral part, and possibly with a paramagnetic conductive disc coaxial to the oscillating weight.

The invention relates to a system for guiding a drone during the approach phase to a platform, in particular a naval platform, with a view to landing same, characterised in that the platform is provided with equipment indicating the angle of descent, emitting an array of optical guide beams onto an angular sector predetermined from the horizontal, and in that the drone is provided with a camera (6) for acquiring the beam and which is connected to an image analysis means (7) and a means (8) for computing command orders sent to an automatic flight means (9) of the drone, in order to prompt the drone to follow the guide beams.