270results about How to "Safe separation" patented technology

Secure protection and distribution of a personal identification number (PIN) is achieved by using a first encryption process only for PIN data and a second encryption process for non-PIN data. The first encryption process uses asymmetric encryption, where a public key is used for encryption of PIN data and a private key, held only by an authorizing agent, is used to decrypt the PIN data. The second encryption process uses a key which is available to an authentication requestor, such as merchants. A party seeking authentication of PIN data must forward the encrypted PIN data to an authorizing agent along with account data necessary to validate the PIN data. The authentication requestor is provided with a signal which is indicative of the verification status of the PIN data without being privy to the contents of the PIN data.

Provided is a cutting method for a glass sheet, comprising radiating a laser beam to a cutting portion (C) of a glass sheet (G) having a thickness of 500 μm or less to fuse the glass sheet (G), wherein a narrowest gap between fused end surfaces (Ga1 and Gb1) of the glass sheet (G), which face each other in the cutting portion (C), is managed to satisfy a relationship of 0.1≦b/a≦2, where “a” is a thickness of the glass sheet (G) and “b” is the narrowest gap.

The present invention is a flight management system with precision merging that may determine a rejoin turn location based upon a heading to allow proper spacing between an aircraft and an identified target aircraft. The flight management system may monitor for deviation from assigned airspace, winds, turn radius and desired airport speed profile for the approach to further refine a turn-back location. Advantageously, a delay in landing of the target aircraft may not affect the landing approach of other aircraft. This may result in more accurate spacing between aircraft which are closer to the allowed separation minima and may provide an increase in capacity especially in high-density areas.

The invention relates to a sealed small low-impact release screw bolt. The bolt comprises an inner cylinder (1), a shear pin (2), a wedge block (3), a piston (4), a sealing ring (5), a double O-shaped ring sealed baffle (6) and an outer cylinder (7). The bolt is characterized by small size, sealing type, low impact, strong connection and no pollution. Before separated, the two polars of the connected body form strong connection; and when separated, the two polars of the connected body can be safely and fast separated and generate low impact disturbance, thus the bolt is a pyrotechnic connection separating device with good comprehensive performance, and can be directly used in the stage separating systems of the missile and other spacecrafts, also provide beneficial reference for the design of the similar separating mechanism, have good application prospect.

The invention relates to a solid material unpacking machine, in particular to a full automatic unpacking and unloading machine, which is characterized in that: all stages of mechanisms are connected through flanges; a bag breaking mechanism, a screening mechanism and a material output mechanism are arranged on a main body frame; the outer surface of the main body frame is connected with a surface panel in a splicing mode; the surface panel on the top of the main body frame is provided with a main dust removal outlet; and a channel formed from the feeding inlet end of a feeding mechanism to the outlet end of the material output mechanism and the outlet end of a waste bag output mechanism is a one-way communication channel. The full automatic unpacking and unloading machine has the advantages that the machine has high work efficiency, energy conservation, environmental protection, small volume, light weight and the like, can safely and stably separate solid materials from packages in automatic high-speed running, and convey the materials to downstream equipment, while the waste packages enter a waste bag recovery device for recovery, and the machine can particularly meet the requirements of unloading, separating and collecting toxic and corrosive powder, and particle materials.

Muzzleloader systems include a pre-packaged propellant charge and primer for providing efficient loading and unloading of the muzzleloader. The breech end accepts the propellant and means are provided to prevent breech loading of the projectile. A propellant cartridge conforms to a constriction portion to minimize ullage. A projectile is inserted in the muzzle end seats on the constriction portion. The propellant cartridge may be received in a removable breech plug. The constriction portion may be part of the breech plug or a separate component secured in the barrel by way of the breech plug. The cartridge may have a primer mechanism integrated into a proximal end. Projectiles have sliding components that have an axial elongate position and an axial shortened position and may be loaded with a ramrod having an engagement portion for each of the two pieces whereby the projectile doesn't prematurely collapse.

Methods and systems suitable for processing multiple trajectory modification requests received from multiple aircraft within an airspace. The methods include receiving multiple trajectory modification requests that are transmitted from multiple aircraft and request alterations of the altitudes, speeds and/or lateral routes thereof, sequentially performing conflict assessments on the multiple trajectory modification requests to determine if any of the multiple trajectory modification requests pose conflicts with the altitudes, speeds and lateral routes of any other of the multiple aircraft, placing in a computer memory data queue n trajectory modification requests of the multiple trajectory modification requests that are identified by the conflict assessments as posing conflicts, and periodically processing the queue to perform subsequent conflict assessments on the n trajectory modification requests to determine if any of the n trajectory modification requests still pose conflicts with the altitudes, speeds and lateral routes of any other of the multiple aircraft.

A system for enabling the safe landing of an aircraft during an in-flight emergency is provided. The system includes a plurality of onboard devices for releasably securing a plurality of wings to a fuselage, and a non-electric module for activating said onboard devices. Said onboard devices are released to separate said wings from the fuselage.

The present invention relates a method for preparation of ketoxime compound, comprising: feeding a ketone compound, hydrogen peroxide, water, and ammonia into a reactor for contact reaction under the conditions of oximation reaction of ketone and ammonia, in the presence of a titanium-silicon molecular sieve catalyst, wherein, the molar ratio of the hydrogen peroxide to the ketone compound is 0.1 or more and less than 1. The present invention also relates to method for preparation of alkoxy-amine hydrochloride, comprising the following steps: preparing ketoxime compound by using the method for preparation of ketoxime compound described above, preparing ketoxime ether compound from the ketoxime compound, and then feeding the ketoxime ether compound and hydrochloric acid solution respectively into a rectification tower continuously for catalytic distillation, and separating alkoxy-amine hydrochloride from the liquid of the tower bottom of the rectification tower. In the method for preparation of ketoxime compound provided in the present invention, the titanium-silicon molecular sieve catalyst has a long useful life; using the method for preparation of alkoxy-amine hydrochloride provided in the present invention, the target product can be obtained at high purity and high yield.

The invention discloses ground zero-gravity separation test equipment for a large spacecraft. The ground zero-gravity separation test equipment comprises a test bracket, pulley assemblies, a buffer mechanism, a locking mechanism, a connecting rope, a weight balancing and lifting mechanism, a tension recorder and a test sling, wherein the test bracket is a cubic frame structure; a pulley mechanism I is arranged on one side surface of a frame in a suspension manner; the test sling is connected to the lower end of the connecting rope, and the weight balancing and lifting mechanism is connected to the other end, going around a pulley mechanism II, of the connecting rope; the two pulley assemblies are respectively arranged on a top cross beam of the frame structure so as to support the connecting rope which goes around the pulley assemblies; the buffer mechanism comprises a buffer and a buffering stop block; and the connecting rope drives the buffering stop block to move together at a uniform speed until the buffering stop block impacts the buffer to enable the kinetic energy to be dissipated.

The present invention provides cellular phone in which a plurality of mounting parts for IC cards in which the country number of the contracting country and the own-station telephone number are stored are disposed, the cellular phone comprising position information storage means that store position of the cellular phone, selection means which make it possible to select the IC card in which the own-station telephone number that is used for calling is stored, first determination means which determine, on the basis of the country number stored in the selected IC card and the stored position information, whether or not calling is to be performed by adding header information for accessing the exchange of the contracting country of the IC card, and calling means which perform calling by adding the header information in cases where the first determination means determine that calling is to be performed by adding the header information.

The invention relates to a measurement transmitter for operation in a process plant. The enclosure of the measurement transmitter comprises two mutually separate containers (11, 12), where the transducer for converting the process-related, physical variable into an appropriate electrical variable is housed in the one container (11), and an electronic circuit (22) is arranged in the other container (12). The two containers (11, 12) have complimentary screw threads (51, 52) to each other, and are screwed together directly. The screw connection of the two containers (11, 12) comprises a transformer made up of two parts (31, 32), whose parts (31, 32) each comprise a winding (41, 42) connected to the circuitry (21, 22) of the respective container (11, 12).

The invention relates to a treatment method of coarse tin decoppered slag, which comprises the following steps: jetting industrial oxygen with the purity of 93-98.5% to the surface or inside of the coarse tin decoppered slag at the temperature of 850-1250 DEG C until the coarse tin decoppered slag is completely oxidized into copper oxide and tin tetroxide dust; leaching the copper oxide and tin tetroxide dust for 2-3 hours under atmospheric pressure and temperature under the condition of the initial acid of 70-120 g/L to obtain leached filtered slag, and carrying out reduction smelting to produce coarse tin; concentrating the leached filtrate to crystallize, and separating to produce chalcanthite product, or carrying out electrolysis to produce electrolytic copper; and returning the crystallization mother solution or electrolysis solution to the leaching process for solution preparation. The invention can separate tin and copper in the crude tin decoppered slag in a safe and efficient way, and does not generate waste water, waste gas or waste residue.

A motor winding enamelled wire, an iron core separation device and a separation method are characterized in that a horizontal working platform is arranged; a pair of gripping tongs used for gripping the winding iron core are fixedly arranged on the working platform; a cutting machine is arranged at one side of the gripping tongs, a grinding wheel on the cutting machine is positioned at the right end of the winding enamelled wire and the edge of the grinding wheel is parallel to the end face of the winding enamelled wire; an air cylinder is arranged at the left side of the winding iron core along the axis direction of the winding iron core; and the front end of a flexible cylinder rod in the air cylinder is connected with a hook that can be embedded at the left end of the winding enamelled wire through an inhaul cable. The device is simple in structure, low in manufacturing cost, is applicable to a wide range of motors, and simple and convenient in operation. The method is safe and reliable in separation process, does not damage silicon-steel sheet, and is highly efficient, energy-saving and environment-friendly in separation operation.

An internal combustion engine has a reciprocating piston moving in a cylinder. A crank shaft is mounted in the interior of the crankcase. A connecting rod connects the piston to the crankshaft. The crankcase has a venting device for pressure compensation of the interior of the crankcase. The venting device has a venting line having a channel extending in a rotary component of the engine.

A muzzle-loader bullet system includes a pre-packaged propellant charge and primer for providing efficient loading and unloading of the muzzleloader. The muzzleloader accepts in the breech end the propellant containment vessel that abuts against a constriction portion with a reduced diameter portion. The propellant containment vessel having an end portion with a tapered surface that conforms to the constriction portion surface. A projectile is inserted in the muzzle end and seats against the constriction portion. The propellant containment vessel may be received in a removable breech plug. The constriction portion may be part of the breech plug or a separate component secured in the barrel by way of the breech plug. The containment vessel further comprises a primer mechanism that may be integrated into the proximal end of the containment vessel.

A system of separating a membrane from underlying tissue. The system includes a separation member operable to separate the membrane from the tissue and a cutting element in communication with the separation member. The cutting element is also operable to dissect the membrane without harming the underlying tissue.

A female element quick coupling for releasably joining two pipes conveying a fluid under pressure and which receives a male coupling wherein the female element includes a latch movable relative to a body of the female element between a first position, in which it retains the male portion in a leaktight coupling position, and a second position, in which it retains the male portion in a position for purging a downstream pipe. The female element further includes a control member mounted to slide in an open bore in the body for causing the latch to move at least towards the second position. This female element includes a gasket for closing a gap defined between an outer face of the member and an inside face of the bore especially at high purging pressures.

The application provides a model separation device for a 3D printer, wherein the 3D printer is capable of printing a solid-state model. The model separation device comprises a fixed bearing plate used for bearing the model and provided with a plurality of through holes, and a movable extrusion plate arranged in parallel relative to the bearing plate, wherein a plurality of extrusion components are arranged between the plate body of the extrusion plate and the bearing plate, and the extrusion plate and the extrusion components are configured as follows: the extrusion components are capable of gradually stretching out from the through holes with the movement of the plate body of the extrusion plate towards a direction approaching to the bearing plate. According to the model separation device for the 3D printer provided by the application, the purpose of rapidly, safely and accurately separating the printing model is achieved by virtue of the principle of generating an axial force by thread rotation by reasonably designing structures among the various components. Meanwhile, the working efficiency is increased, and the integrity and beauty of the printing model are ensured.

The invention relates to a method for optimizing the display of data relating to the risks associated with obstacles. The method includes extracting from an obstacle database, a list of obstacles included in the geographic zone defined by the range, the orientation and the position of the aircraft. Obstacle related information and warning lists are received. The obstacle list is regrouped by applying to the obstacles criteria relating to the proximity of the obstacles relative to the aircraft; to the proximity of the obstacles to one another; and to their warning level. The symbology adapted to the obstacle display is generated. In particular, the invention applies to optimizing the display of warnings relating to the risks of collision with point-like or linear obstacles.

The invention discloses a protective method for a solid-state disk encryption key. The protective method comprises the following steps: a user passes a management procedure authentication password; a solid-state disk safety module calculates a hash value for the authentication password and stores the hash value into a solid-state disk for authenticating a user password in a daily using process; the safety module encrypts the encryption key by using the authentication password; the solid-state disk stores a ciphertext of the encryption key. According to the technical scheme adopted by the invention, the authentication password hash value is stored in the solid-state disk and encryption protection is performed on the encryption key by using the authentication password, so that the safe separation of the protected encryption key and the protected data is achieved while the user's identity is effectively authenticated, and the safety of the encryption key is improved.