mhurhangee/ep-ind-claims huggingface dataset:
A vacuum pump, in particular a turbomolecular pump, comprising a synchronous electric motor for driving a moving part of the vacuum pump, in particular for driving a pump rotor of the vacuum pump, wherein the electric motor has a rotor and a stator; wherein the stator has three winding strands (301, 303, 305) formed by a respective electrical conductor to generate a stator-side magnetic field which cooperates with a rotor-side magnetic field of the rotor for a rotating driving of the rotor, characterized in that an electrical terminal is provided which comprises at least six electrical contacts (403, 405, 407, 409, 411, 413) which are accessible from outside the vacuum pump and which lead into the interior of the vacuum pump; in that each of the two ends (U1, U2, V1, V2, W1, W2) of each winding strand (301, 303, 305) is connected to one of the electrical contacts (403, 405, 407, 409, 411, 413); and in that the winding strands (301, 303, 305) of the stator have a pitch such that harmonics of the stator-side magnetic field, in particular harmonics having ordinal numbers divisible by three, are at least substantially avoided.
A use of a passivation layer (1.1) for passivating a first side surface (4.1) of an adhesive roll, the passivation layer (1.1) being produced from at least one composition, the composition being dried and/or forming a tearable protective layer for the first side surface (4.1) of the adhesive roll after a chemical reaction, the passivation layer (1.1) being tearable in such a way that, after an adhesive strip has been unrolled, the remaining passivation layer (1.1) does not project from the side surfaces of the adhesive roll, the production method having the following steps: a) coating, with the composition, a first surface (2.1) of a production support for the passivation element, the coating being carried out in a thickness of between 0.02 mm and 1.5 mm by means of a spray, dip or doctor blade coating or in an offset printing, screen printing, gravure printing or transfer printing method; b) at least partially drying and/or curing the layer to form a passivation layer (1.1). a) coating, with the composition, a first surface (2.1) of a production support for the passivation element, the coating being carried out in a thickness of between 0.02 mm and 1.5 mm by means of a spray, dip or doctor blade coating or in an offset printing, screen printing, gravure printing or transfer printing method; b) at least partially drying and/or curing the layer to form a passivation layer (1.1).
A system, comprising: a first processing node associated with a first structural location of an aircraft platform, the first processing node comprising a first sensor, the first processing node to determine a first aeroelastic navigation state of the platform at the first structural location of the platform with respect to a first aeroelasticity reference; a second processing node associated with a second structural location of the platform different than the first structural location, the second processing node comprising a second sensor, the second processing node to determine a second aeroelastic navigation state of the platform at the second structural location of the platform with respect to the first aeroelasticity reference or a second aeroelasticity reference; a navigation reference node that uses the first and second aeroelastic navigation states to compute a center of gravity of the platform and determine a navigation state at the determined center of gravity of the platform; a storage device to store a platform navigation state comprising at least one of the first and second aeroelastic navigation states and the navigation state for the center of gravity for the platform. a first processing node associated with a first structural location of an aircraft platform, the first processing node comprising a first sensor, the first processing node to determine a first aeroelastic navigation state of the platform at the first structural location of the platform with respect to a first aeroelasticity reference; a second processing node associated with a second structural location of the platform different than the first structural location, the second processing node comprising a second sensor, the second processing node to determine a second aeroelastic navigation state of the platform at the second structural location of the platform with respect to the first aeroelasticity reference or a second aeroelasticity reference; a navigation reference node that uses the first and second aeroelastic navigation states to compute a center of gravity of the platform and determine a navigation state at the determined center of gravity of the platform; a storage device to store a platform navigation state comprising at least one of the first and second aeroelastic navigation states and the navigation state for the center of gravity for the platform.
A tamper evident closure for a liquid container having a neck (2,344,442) with an opening defining a pourer orifice (3,343,443), said tamper evident closure extending in an axial direction (X-X) and comprising: a tubular member (101,301,401) comprising an upper portion (102,302,402) and a lower portion (103,303,403) with a lower edge (113,313,413) surrounding an open bottom end; and a plug member (123,308,423) coupled with said tubular member, configured to selectively close and open the pourer orifice of the liquid container, wherein the lower portion (103,303,403) of said tubular member comprises axial constraining means (110,310,410) configured to engage with corresponding axial constraining means of the container (5,305,405) in order to constrain said lower portion of the tubular member to the container in the axial direction (X-X) and thereby prevent its removal therefrom, and wherein said lower portion (103,303,403) of said tubular member (101,301,401) comprises at least one annular recess (115,315,415) that extends completely around the circumferential extent of the lower portion (103,303,403) of said tubular member and is positioned between said lower edge (113,313,413) and said axial constraining means (110,310,410), characterized in that said recess includes at least a portion with a reduced wall thickness (S2,S300,S400) whereby an axial thrust exceeding a predetermined value applied against said lower edge (113,313,413) in the direction of the upper portion (102,302,402) of said tubular member (101,301,401) will result in a visible deformation of the lower portion (103,303,403) at the recess (115,315,415). a tubular member (101,301,401) comprising an upper portion (102,302,402) and a lower portion (103,303,403) with a lower edge (113,313,413) surrounding an open bottom end; and a plug member (123,308,423) coupled with said tubular member, configured to selectively close and open the pourer orifice of the liquid container, wherein the lower portion (103,303,403) of said tubular member comprises axial constraining means (110,310,410) configured to engage with corresponding axial constraining means of the container (5,305,405) in order to constrain said lower portion of the tubular member to the container in the axial direction (X-X) and thereby prevent its removal therefrom, and wherein said lower portion (103,303,403) of said tubular member (101,301,401) comprises at least one annular recess (115,315,415) that extends completely around the circumferential extent of the lower portion (103,303,403) of said tubular member and is positioned between said lower edge (113,313,413) and said axial constraining means (110,310,410),
A method comprising: polling a subset of a plurality of remote terminals (112, 114, 116, 118) of a satellite communications network, and receiving a polling response from each of the polled remote terminals; determining a respective drift value for each polled remote terminal (112, 114, 116, 118), wherein each drift value is based on a difference between an initial timing reference and a subsequent timing reference as a result of a change of position of a satellite of the network, and computing a time delay value based on at least a subset of the determined drift values; monitoring by a hub a received data burst from each remote for an error, when the error crosses a threshold, and transmitting by the hub closed-loop timing feedback information to the plurality of remote terminals, correcting remote timing using the CLT feedback message from the said hub, wherein the CLT information is based on the timing of received data bursts relative to a timing aperture window; characterized by broadcasting by a hub a status flag contained as a field in a SuperFrame Numbering Packet, SFNP; and using by said hub the status flag to signal remotes the inroute timing mechanism that is currently used: - if this flag is TRUE, the system is using CLT mechanism and hub provides timing corrections to remotes, - if it is FALSE, the system is depending on a remote time offset T RO computation mechanism at the remotes. polling a subset of a plurality of remote terminals (112, 114, 116, 118) of a satellite communications network, and receiving a polling response from each of the polled remote terminals; determining a respective drift value for each polled remote terminal (112, 114, 116, 118), wherein each drift value is based on a difference between an initial timing reference and a subsequent timing reference as a result of a change of position of a satellite of the network, and computing a time delay value based on at least a subset of the determined drift values; monitoring by a hub a received data burst from each remote for an error, when the error crosses a threshold, and transmitting by the hub closed-loop timing feedback information to the plurality of remote terminals, correcting remote timing using the CLT feedback message from the said hub, wherein the CLT information is based on the timing of received data bursts relative to a timing aperture window; characterized by broadcasting by a hub a status flag contained as a field in a SuperFrame Numbering Packet, SFNP; and using by said hub the status flag to signal remotes the inroute timing mechanism that is currently used: - if this flag is TRUE, the system is using CLT mechanism and hub provides timing corrections to remotes, - if it is FALSE, the system is depending on a remote time offset T RO computation mechanism at the remotes. - if this flag is TRUE, the system is using CLT mechanism and hub provides timing corrections to remotes, - if it is FALSE, the system is depending on a remote time offset T RO computation mechanism at the remotes.
A method, comprising: acquiring, at a network entity, for each of a plurality of user equipment connected to a resource of a serving cooperation area a current connectivity ratio of each user equipment for the resource, wherein the resource is a set of physical resource blocks of the serving cooperation area that are needed for a requested data rate of the user equipment in one or more sub-bands, the current connectivity ratio is a group quality indicator ratio, GQIR, for the resource and the n-th group quality indicator ratio for user equipment connected to the resource is defined as: GQIR n = GQI n ∗ GQI n / GQI n + 1, wherein GQI(n) is a group quality indicator indicating channel quality for a group of connections for an n-th resource and all GQIs for all resources associated with any candidate for a serving cooperation area, CSCA, defined for said user equipment are sorted in a decreasing order with GQI >GQI >...>GQI, N being the number of resources and the serving cooperation area being a CSCA, selecting, at the network entity, among the plurality of user equipment connected to the resource of the serving cooperation area, first user equipment having a lowest current connectivity ratio, and determining whether the current connectivity ratio of the first user equipment for the resource is equal to or smaller than a stored connectivity ratio of the first user equipment for another resource available for the first user equipment. acquiring, at a network entity, for each of a plurality of user equipment connected to a resource of a serving cooperation area a current connectivity ratio of each user equipment for the resource, wherein the resource is a set of physical resource blocks of the serving cooperation area that are needed for a requested data rate of the user equipment in one or more sub-bands, the current connectivity ratio is a group quality indicator ratio, GQIR, for the resource and the n-th group quality indicator ratio for user equipment connected to the resource is defined as: GQIR n = GQI n ∗ GQI n / GQI n + 1, wherein GQI(n) is a group quality indicator indicating channel quality for a group of connections for an n-th resource and all GQIs for all resources associated with any candidate for a serving cooperation area, CSCA, defined for said user equipment are sorted in a decreasing order with GQI >GQI >...>GQI, N being the number of resources and the serving cooperation area being a CSCA, selecting, at the network entity, among the plurality of user equipment connected to the resource of the serving cooperation area, first user equipment having a lowest current connectivity ratio, and determining whether the current connectivity ratio of the first user equipment for the resource is equal to or smaller than a stored connectivity ratio of the first user equipment for another resource available for the first user equipment.
A composite waveguide, comprising: a central core configured to transmit a plurality of modes; and at least one side core helically wound about said central core and configured to be selectively coupled to at least a portion of said plurality of modes in said central core, such that said plurality of modes in said central core are selectively coupled to said at least one side core using a quasi-phase matching mechanism. a central core configured to transmit a plurality of modes; and at least one side core helically wound about said central core and configured to be selectively coupled to at least a portion of said plurality of modes in said central core, such that said plurality of modes in said central core are selectively coupled to said at least one side core using a quasi-phase matching mechanism.
A method for characterizing an incident wave pressure in a hearing test, the method comprising: introducing a sonic stimulus into an ear canal with a sound source transducer positioned in an ear canal; measuring at least a sound pressure level ( P m) in said ear canal with a receiving transducer in the ear canal, wherein the measured sound pressure level P m is related to a forward pressure according to P + = P m 1 + R; processing information associated with said sound pressure level; determining at least an acoustic reflectance including a real and imaginary part based on information associated with said sound pressure level; characterized by: determining an incident wave pressure parameter (P +) in said ear canal based on the measured sound pressure level P m according to: P + = P m 1 + R; and calibrating an audiometer using the incident wave pressure parameter ( P +); and, performing a hearing test to determine a hearing threshold level with respect to a threshold of said incident wave pressure. introducing a sonic stimulus into an ear canal with a sound source transducer positioned in an ear canal; measuring at least a sound pressure level ( P m) in said ear canal with a receiving transducer in the ear canal, wherein the measured sound pressure level P m is related to a forward pressure according to P + = P m 1 + R; processing information associated with said sound pressure level; determining at least an acoustic reflectance including a real and imaginary part based on information associated with said sound pressure level; characterized by: determining an incident wave pressure parameter (P +) in said ear canal based on the measured sound pressure level P m according to: P + = P m 1 + R; and calibrating an audiometer using the incident wave pressure parameter ( P +); and, determining an incident wave pressure parameter (P +) in said ear canal based on the measured sound pressure level P m according to: P + = P m 1 + R; and calibrating an audiometer using the incident wave pressure parameter ( P +); and, performing a hearing test to determine a hearing threshold level with respect to a threshold of said incident wave pressure.
Method for operating a motor vehicle which has a service brake system with a controllable pressure generator and a parking brake system which can be activated by means of extraneous force, wherein the parking brake system is formed essentially from an operator control element, an electronic control unit to which wheel speed values of wheel speed sensors (12, 13) are fed, at least one unit for generating a brake application force as well as having brake devices which can be applied by the unit on at least one axle, and wherein activation of the operator control element while the motor vehicle is travelling brings about actuation of the pressure generator in order to carry out an emergency braking process, while activation of the operator control element in the stationary state of the motor vehicle brings about actuation of the unit for initiating a parking brake process, and further measures for reducing the speed of the motor vehicle are carried out while an emergency braking process is being carried out, characterized in that in order to reduce the speed of the motor vehicle while an emergency braking process is being carried out the position of the accelerator pedal is ignored and a possible acceleration request of the vehicle driver by depressing the accelerator pedal is not carried out.
A wrought aluminum alloy product consisting of: from 2.75 wt. % to 5.0 wt. % Cu; from 0.2 wt. % to 0.8 wt. % Mg; wherein the ratio of copper-to-magnesium ratio (Cu/Mg) in the aluminum alloy is in the range of from 8.0 to 17; from 0.1 wt. % to 1.05 wt. % Li; from 0.30 wt. % to 2.0 wt. % Ag; from 0.50 wt. % to 1.5 wt. % Zn; up to 1.0 wt. % Mn; optional from 0.01 wt.-% to 0.15 wt.-% Ti, wherein Ti may be present as a grain refiner in combination with B or C in an amount ranging from 0.0003 wt.-% to 0.005 wt.-%; optional grain structure control elements from 0.01 wt.% to 0.25 wt.%, wherein the grain structure control elements include one or more elements of the group of Zr, Sc, Cr, V, and Hf; and optional deoxidizers chosen from the group of Ca, Sr and Be, wherein, when Ca is included, it may be present in an amount of from 0.001 to 0.05 wt.-%, wherein Sr may be included in an amount of from 0.001 to 0.05 wt.-% as a substitute in whole or in part for Ca, and wherein Be may be present in an amount of up to 20 ppm; the balance being aluminum and impurities. from 2.75 wt. % to 5.0 wt. % Cu; from 0.2 wt. % to 0.8 wt. % Mg; wherein the ratio of copper-to-magnesium ratio (Cu/Mg) in the aluminum alloy is in the range of from 8.0 to 17; from 0.1 wt. % to 1.05 wt. % Li; from 0.30 wt. % to 2.0 wt. % Ag; from 0.50 wt. % to 1.5 wt. % Zn; up to 1.0 wt. % Mn; optional from 0.01 wt.-% to 0.15 wt.-% Ti, wherein Ti may be present as a grain refiner in combination with B or C in an amount ranging from 0.0003 wt.-% to 0.005 wt.-%; optional grain structure control elements from 0.01 wt.% to 0.25 wt.%, wherein the grain structure control elements include one or more elements of the group of Zr, Sc, Cr, V, and Hf; and optional deoxidizers chosen from the group of Ca, Sr and Be, wherein, when Ca is included, it may be present in an amount of from 0.001 to 0.05 wt.-%, wherein Sr may be included in an amount of from 0.001 to 0.05 wt.-% as a substitute in whole or in part for Ca, and wherein Be may be present in an amount of up to 20 ppm; the balance being aluminum and impurities.
A solid ammonia storage and delivery material wherein said solid material is a chemical complex in the form of an ionic salt of the general formula: M a (NH 3) n X z, wherein M is one or more cations selected from alkali metals such as Li, Na, K or Cs, alkaline earth metals such as Mg, Ca or Sr, aluminium and transition metals such as V, Cr, Mn, Fe, Co, Ni, Cu or Zn or combinations thereof such as NaAl, KAI, K 2 Zn, CsCu or K 2 Fe, X is one or more anions selected from fluoride, chloride, bromide, iodide, nitrate, thiocyanate, sulphate, molybdate and phosphate ions, a is the number of cations per salt molecule, z is the number of anions per salt molecule, and n is the coordination number of 2 to 12, wherein said storage and delivery material which is saturated completely or not completely has an ammonia content of 20-60 wt%, wherein said storage and delivery material is compacted to a density above 75% of the theoretical skeleton density defined as the density of an ideal single crystal with no internal voids and is in the form of a block or tablet or a pellet of a desired shape.
A method for making a vehicle, including a body comprising carbon fibres, where the body is wound up on a mandrel with threads wetted in glue, where the threads contain carbon fibres, where the threads wound around the mandrel are subsequently cured, where, after the curing, the body is drawn off the mandrel, where the front end and rear end of the body are closed with closure elements, characterised in that during the winding process, one or more layers of light weight ceramic and/or other armouring materials are laid in which thereby become integrated in the basic body and that mounting agents are put on the mandrel, whereafter mounting means are fitted, where mounting agents and means are cleaned from threads and glue after the winding process, where the body is subsequently surface treated.
One- or multilayered film, wherein the film (1;2;11) comprises two outer layers (4,5) and at least one inner layer that contains at least one thermoplastic olefin homo or co-polymer selected from the group consisting of poly ethylene, in particular LDPE or HDPE, polypropylene, polybutylene, polyisobutylene or mixtures of at least two of the said polymers and at least one polyester, characterized in that the at least one polyester in the inner layer is amorphous, in particular in the form of amorphous polyethylene terephthalate (A-PET), and that in one or both of the outer layers (4,5) either polyester alone or a mixture of polyester and polyolefin is present.