mhurhangee/patent-ind-claim-en huggingface dataset:
A system for controlling an aircraft in response to deployment of an ejection seat, the system comprising: a seat controller configured to be located on the ejection seat and configured to output a signal in response to initiation of an ejection sequence; an aircraft controller configured to receive the signal from the seat controller; and a first tangible, non-transitory memory configured to communicate with the aircraft controller, the first tangible, non-transitory memory having instructions stored thereon that, in response to execution by the aircraft controller, cause the aircraft controller to perform operations comprising: receiving, by the aircraft controller, the signal from the seat controller, receiving, by the aircraft controller, data signals from an operational data source, and sending, by the aircraft controller, a first set of command signals to a component of the aircraft. a seat controller configured to be located on the ejection seat and configured to output a signal in response to initiation of an ejection sequence; an aircraft controller configured to receive the signal from the seat controller; and a first tangible, non-transitory memory configured to communicate with the aircraft controller, the first tangible, non-transitory memory having instructions stored thereon that, in response to execution by the aircraft controller, cause the aircraft controller to perform operations comprising: receiving, by the aircraft controller, the signal from the seat controller, receiving, by the aircraft controller, data signals from an operational data source, and sending, by the aircraft controller, a first set of command signals to a component of the aircraft. receiving, by the aircraft controller, the signal from the seat controller, receiving, by the aircraft controller, data signals from an operational data source, and sending, by the aircraft controller, a first set of command signals to a component of the aircraft.
Suction pulser intended for a heating, ventilation and/or air-conditioning device of a motor vehicle, the pulser comprising a cylindrical or conical turbine that is able to be driven in rotation about the axis (A) of the said turbine , separation means that are suitable for delimiting a first air circulation duct allowing a first flow of air, intended to pass through a first axial part of the turbine , to flow, and a second air circulation duct allowing a second flow of air, intended to pass through a second axial part of the turbine , to flow, the said separation means comprising a tubular member mounted in line with a first end of the said turbine and delimiting an internal space forming at least one part of the first air circulation duct, the second air circulation duct extending outside the tubular member , air inlet means comprising a housing covering the first end of the turbine and the tubular member , the said air inlet means being able to direct a first flow of air into the first air circulation duct, and to direct a second flow of air into the second air circulation duct, the said housing comprising a filter that is intended to have the first and second flow of air pass through it, characterized in that the housing comprises two lateral zones respectively comprising a first orifice equipped with a first arresting means and a second orifice equipped with a second arresting means , the said arresting means being able to move between an open position that allows a flow of air to pass through the corresponding orifice and a closed position that prevents such a passage of the flow of air, the housing further comprising a median zone that comprises a third and a fourth orifice which are provided with at least one valve that serves to control the opening and/or the closing of the said third and fourth orifices so as to respectively allow the flow of air to pass through or prevent the flow of air from passing through the said third and fourth orifices , the first orifice and the second orifice being located facing the filter and the second air circulation duct, extending outside the tubular member , the third orifice and the fourth orifice being located facing the filter and the first air circulation duct, extending inside the tubular member .
A parking brake system for an aircraft , comprising: a first switch interface at a first location, comprising a first enable switch and a first activate switch , wherein the parking brake system is configured to switch a state of a brake in response to the first enable switch and the first activate switch being engaged at the same time; and a second switch interface at a second location, comprising a second enable switch and a second activate switch , wherein the parking brake system is configured to switch the state of the brake in response to the second enable switch and the second activate switch being engaged simultaneously; said system further comprising a shutoff valve configured to permit hydraulic fluid to pass in response to at least one of the first enable switch or the second enable switch being engaged, and a servo in fluid communication with the shutoff valve and configured to change the state of the brake between a park state and a not-park state in response to the first activate switch being engaged while the shutoff valve is configured to permit the hydraulic fluid to pass; wherein the shutoff valve 114 is downstream of the servo , wherein the servo is configured to alter the pressure in the brake when the shutoff valve is configured to allow flow to pass and the shutoff valve is configured to lock the hydraulic pressure in the brake in response to the shutoff valve shutting off flow, wherein the parking brake system is configured to retain, in a non-volatile memory, the state of the brake when the parking brake system remains inactive to conserve power. a first switch interface at a first location, comprising a first enable switch and a first activate switch , wherein the parking brake system is configured to switch a state of a brake in response to the first enable switch and the first activate switch being engaged at the same time; and a second switch interface at a second location, comprising a second enable switch and a second activate switch , wherein the parking brake system is configured to switch the state of the brake in response to the second enable switch and the second activate switch being engaged simultaneously; said system further comprising a shutoff valve configured to permit hydraulic fluid to pass in response to at least one of the first enable switch or the second enable switch being engaged, and a servo in fluid communication with the shutoff valve and configured to change the state of the brake between a park state and a not-park state in response to the first activate switch being engaged while the shutoff valve is configured to permit the hydraulic fluid to pass; wherein the shutoff valve 114 is downstream of the servo , wherein the servo is configured to alter the pressure in the brake when the shutoff valve is configured to allow flow to pass and the shutoff valve is configured to lock the hydraulic pressure in the brake in response to the shutoff valve shutting off flow, wherein the parking brake system is configured to retain, in a non-volatile memory, the state of the brake when the parking brake system remains inactive to conserve power.
A food product obtained by compressing a pulverulent composition comprising an essentially, preferably exclusively, vegetable protein or protein mixture, said food product being flavored through the addition of at least one flavoring, said flavoring being chosen from the flavorings of dried fruits.
A piezoelectric element comprising: a first electrode ; a second electrode ; and a thin piezoelectric layer which is provided between the first electrode and the second electrode and is formed of a perovskite type compound oxide which contains potassium, sodium, and niobium, wherein, in the piezoelectric layer, in an X-ray diffraction pattern obtained by θ-2θ measurement, peaks derived respectively from a plane and a plane are in a range in which 2θ is from 45° to 47°, whereby, a peak position of the peak on a high angle side in the plane among the peaks satisfies 46.0° ≤ 2θ ≤ 46.5°; a difference between the 2θ peak on the high angle side in the plane and the 2θ peak on a low angle side in the plane is greater than 0.60°; characterized in that the piezoelectric layer comprises a plurality of piezoelectric films and in that the piezoelectric layer has a thickness of 50nm to 2000nm and wherein the piezoelectric layer is formed by a solution method. a first electrode ; a second electrode ; and a thin piezoelectric layer which is provided between the first electrode and the second electrode and is formed of a perovskite type compound oxide which contains potassium, sodium, and niobium, wherein, in the piezoelectric layer, in an X-ray diffraction pattern obtained by θ-2θ measurement, peaks derived respectively from a plane and a plane are in a range in which 2θ is from 45° to 47°, whereby, a peak position of the peak on a high angle side in the plane among the peaks satisfies 46.0° ≤ 2θ ≤ 46.5°; a difference between the 2θ peak on the high angle side in the plane and the 2θ peak on a low angle side in the plane is greater than 0.60°; characterized in that the piezoelectric layer comprises a plurality of piezoelectric films and in that the piezoelectric layer has a thickness of 50nm to 2000nm and wherein the piezoelectric layer is formed by a solution method.
A system for measuring the temperature of a superconducting device, comprising: a temperature component operable for determining an operating temperature of a superconducting resonator of the device, based on a frequency factor exhibited by the superconducting resonator; wherein the frequency factor comprises a frequency shift exhibited by the superconducting resonator due to a change in temperature between the operating temperature and a reference temperature; the temperature component further comprising: a simulation component operable for simulating operation of the superconducting resonator to determine an estimated frequency exhibited by the superconducting resonator at the reference temperature, wherein a kinetic inductance of the superconducting resonator is known at the reference temperature; and a measurement component operable for measuring an operating frequency exhibited by the superconducting resonator at the operating temperature, wherein the frequency shift is a function of the estimated frequency and the operating frequency. a temperature component operable for determining an operating temperature of a superconducting resonator of the device, based on a frequency factor exhibited by the superconducting resonator; wherein the frequency factor comprises a frequency shift exhibited by the superconducting resonator due to a change in temperature between the operating temperature and a reference temperature; the temperature component further comprising: a simulation component operable for simulating operation of the superconducting resonator to determine an estimated frequency exhibited by the superconducting resonator at the reference temperature, wherein a kinetic inductance of the superconducting resonator is known at the reference temperature; and a measurement component operable for measuring an operating frequency exhibited by the superconducting resonator at the operating temperature, wherein the frequency shift is a function of the estimated frequency and the operating frequency. a simulation component operable for simulating operation of the superconducting resonator to determine an estimated frequency exhibited by the superconducting resonator at the reference temperature, wherein a kinetic inductance of the superconducting resonator is known at the reference temperature; and a measurement component operable for measuring an operating frequency exhibited by the superconducting resonator at the operating temperature, wherein the frequency shift is a function of the estimated frequency and the operating frequency.
A method comprising: by a computing device, determining a received power at a receiving antenna mounted to an antenna measurement system from a transmitting antenna mounted to a device under test, DUT, in motion relative to the antenna measurement system , wherein the method is characterised in that the antenna measurement system is mounted to an N-copter aerial vehicle and comprises a gimbal and signal absorbing foam surrounding the receiving antenna; by the computing device, determining one or more first orientation parameters of the antenna measurement system ; by the computing device, determining one or more second orientation parameters of the DUT ; by the computing device, determining an antenna pattern of the transmitting antenna based on the received power, the first orientation parameters, and the second orientation parameters, wherein the determining is performed while the N-copter aerial vehicle hovers at a stationary lo-cation while the DUT moves in relation to the N-copter aerial vehicle and the receiving antenna receives the received power from the transmitting antenna while the DUT is moving in relation to the N-copter aerial vehicle. by a computing device, determining a received power at a receiving antenna mounted to an antenna measurement system from a transmitting antenna mounted to a device under test, DUT, in motion relative to the antenna measurement system , wherein the method is characterised in that the antenna measurement system is mounted to an N-copter aerial vehicle and comprises a gimbal and signal absorbing foam surrounding the receiving antenna; by the computing device, determining one or more first orientation parameters of the antenna measurement system ; by the computing device, determining one or more second orientation parameters of the DUT ; by the computing device, determining an antenna pattern of the transmitting antenna based on the received power, the first orientation parameters, and the second orientation parameters, wherein the determining is performed while the N-copter aerial vehicle hovers at a stationary lo-cation while the DUT moves in relation to the N-copter aerial vehicle and the receiving antenna receives the received power from the transmitting antenna while the DUT is moving in relation to the N-copter aerial vehicle.
, Clamping spring for a screwless connection terminal for connecting a conductor , wherein the clamping spring has a clamping limb , a contact limb , and a tensioning limb , the tensioning limb being connected to the clamping limb and the contact limb, and the clamping limb and the contact limb being designed as intersecting limbs, wherein the clamping limb has a clamping opening through which the contact limb extends, such that the contact limb is in contact with an edge of the clamping opening remote from the tensioning limb in a pretensioned manner and an exposed wire end of a conductor can be clamped with the contact limb onto a contact surface of a contact element of a screwless connection terminal, wherein the clamping limb has a clamping extension having a clamping surface , characterized in that said clamping extension , starting from the free end of the clamping limb remote from the tensioning limb , initially being formed so as to extend away from the tensioning limb , being then formed so as to extend back in the direction of the tensioning limb in a substantially curved form, and finally being oriented in the direction of the contact limb . wherein the clamping spring has a clamping limb , a contact limb , and a tensioning limb , the tensioning limb being connected to the clamping limb and the contact limb, and the clamping limb and the contact limb being designed as intersecting limbs, wherein the clamping limb has a clamping opening through which the contact limb extends, such that the contact limb is in contact with an edge of the clamping opening remote from the tensioning limb in a pretensioned manner and an exposed wire end of a conductor can be clamped with the contact limb onto a contact surface of a contact element of a screwless connection terminal, wherein the clamping limb has a clamping extension having a clamping surface , characterized in that said clamping extension , starting from the free end of the clamping limb remote from the tensioning limb , initially being formed so as to extend away from the tensioning limb , being then formed so as to extend back in the direction of the tensioning limb in a substantially curved form, and finally being oriented in the direction of the contact limb .
A three-dimensional modeling material for forming a three-dimensional model using thermal energy, the three-dimensional modeling material comprising an olefin-based polymer and an organometallic complex, wherein the organometallic complex contains a central metal, a ligand coordinated to the central metal, and a compatible group having a structure in which four or more carbon atoms bonded to the ligand are linearly arranged, and the central metal has one or more vacant orbitals, characterised in that the compatible group is an aliphatic chain having 4 or more carbon atoms and having no substituent. the three-dimensional modeling material comprising an olefin-based polymer and an organometallic complex, wherein the organometallic complex contains a central metal, a ligand coordinated to the central metal, and a compatible group having a structure in which four or more carbon atoms bonded to the ligand are linearly arranged, and the central metal has one or more vacant orbitals, characterised in that the compatible group is an aliphatic chain having 4 or more carbon atoms and having no substituent.
Thermoplastic polymer composition (P) comprising: (A) 88 to 99.9 wt.-%, preferably 93 to 99.9 wt.-% and in particular 95 to 99.7 wt.-% of at least one styrene-based copolymer, wherein the at least one styrene-based copolymer is selected from poly(α-methylstyrene-co-acrylonitrile) (AMSAN), poly(styrene-co-methyl methacrylate) (SMMA) and mixtures thereof; (B) 0.1 to 5 wt.-%, preferably 0.1 to 4 wt.-%, and in particular 0.2 to 3 wt.-% of at least one modified organopolysiloxane compound; (C) 0 to 10 wt.-%, preferably 0.1 to 6.9 wt.-%, and in particular 0.5 to 2.8 wt.-%, of at least one colorant, dye or pigment; and (D) 0 to 3 wt.-%, preferably 0.1 to 3 wt.-%, and in particular 0.5 to 2.8 wt.-%, of at least one further additive; wherein the constituents (A) to (D) sum up to 100 wt.-% of the thermoplastic polymer composition (P). (A) 88 to 99.9 wt.-%, preferably 93 to 99.9 wt.-% and in particular 95 to 99.7 wt.-% of at least one styrene-based copolymer, wherein the at least one styrene-based copolymer is selected from poly(α-methylstyrene-co-acrylonitrile) (AMSAN), poly(styrene-co-methyl methacrylate) (SMMA) and mixtures thereof; (B) 0.1 to 5 wt.-%, preferably 0.1 to 4 wt.-%, and in particular 0.2 to 3 wt.-% of at least one modified organopolysiloxane compound; (C) 0 to 10 wt.-%, preferably 0.1 to 6.9 wt.-%, and in particular 0.5 to 2.8 wt.-%, of at least one colorant, dye or pigment; and (D) 0 to 3 wt.-%, preferably 0.1 to 3 wt.-%, and in particular 0.5 to 2.8 wt.-%, of at least one further additive;
An electrical device comprising: voltage carrying components, a solid insulation system configured to electrically insulate the voltage carrying components, and a moisture sensor configured to detect moisture in the solid insulation system , wherein the moisture sensor comprises: a capacitor having: - a first electrode , - a second electrode , and - a dielectric material arranged between the first electrode and the second electrode , wherein the solid insulation system forms the dielectric material , the capacitance of the capacitor providing an indication of a moisture level in the dielectric material ; characterized in that the device further comprises a shield member electrically connected to the first electrode , and a spacer configured to distance the shield member from the first electrode to facilitate moisture migration, wherein the first electrode has a meshed structure configured to facilitate moisture migration to and from the dielectric material . voltage carrying components, a solid insulation system configured to electrically insulate the voltage carrying components, and a moisture sensor configured to detect moisture in the solid insulation system , wherein the moisture sensor comprises: a capacitor having: - a first electrode , - a second electrode , and - a dielectric material arranged between the first electrode and the second electrode , wherein the solid insulation system forms the dielectric material , the capacitance of the capacitor providing an indication of a moisture level in the dielectric material ; a capacitor having: - a first electrode , - a second electrode , and - a dielectric material arranged between the first electrode and the second electrode , wherein the solid insulation system forms the dielectric material , the capacitance of the capacitor providing an indication of a moisture level in the dielectric material ; - a first electrode , - a second electrode , and - a dielectric material arranged between the first electrode and the second electrode , wherein the solid insulation system forms the dielectric material , the capacitance of the capacitor providing an indication of a moisture level in the dielectric material ; a shield member electrically connected to the first electrode , and a spacer configured to distance the shield member from the first electrode to facilitate moisture migration, wherein the first electrode has a meshed structure configured to facilitate moisture migration to and from the dielectric material .
A biological fluid collection system adapted to receive a sample , the biological fluid collection system comprising: a mixer having a first mixer end and a second mixer end ; a sample stabilizer disposed within the mixer ; a syringe assembly having a collection chamber , the syringe assembly removably connectable with the second mixer end , the syringe assembly creates a vacuum that draws the sample through the mixer and into the collection chamber ; and a closure removably connectable with the first mixer end , the biological fluid collection system being characterized in that the closure comprises: a cap having a first cap end , a second cap end , and defining a cap channel therein, the cap having a pierceable self-sealing stopper within a portion of the cap channel and a cap connection portion at the second cap end ; and an adapter having a first adapter end , a second adapter end , and defining an adapter channel therein, the adapter having an adapter connection portion at the first adapter end , the cap connection portion removably connectable with the adapter connection portion . a mixer having a first mixer end and a second mixer end ; a sample stabilizer disposed within the mixer ; a syringe assembly having a collection chamber , the syringe assembly removably connectable with the second mixer end , the syringe assembly creates a vacuum that draws the sample through the mixer and into the collection chamber ; and a closure removably connectable with the first mixer end , the biological fluid collection system being characterized in that the closure comprises: a cap having a first cap end , a second cap end , and defining a cap channel therein, the cap having a pierceable self-sealing stopper within a portion of the cap channel and a cap connection portion at the second cap end ; and an adapter having a first adapter end , a second adapter end , and defining an adapter channel therein, the adapter having an adapter connection portion at the first adapter end , the cap connection portion removably connectable with the adapter connection portion . a cap having a first cap end , a second cap end , and defining a cap channel therein, the cap having a pierceable self-sealing stopper within a portion of the cap channel and a cap connection portion at the second cap end ; and an adapter having a first adapter end , a second adapter end , and defining an adapter channel therein, the adapter having an adapter connection portion at the first adapter end , the cap connection portion removably connectable with the adapter connection portion .