56results about How to "Weight advantage" patented technology

A single-compartment combined-sphere broad-frequency submarine seismometer, which comprises a submersion coupling frame, a seismometer compartment, a function compartment and an unhooking mechanism. The submersion coupling frame, which is located at the bottom of the submarine seismometer, is provided with a rigid ring to accommodate the seismometer compartment and thereby allow the sealed seismometer compartment (48) inside said seismometer compartment to sit on the seabed directly. The seismometer compartment comprises a bell-shaped protective cover (49) and the sealed seismometer compartment (48). The bell-shaped protective cover (49) opens downwards. The upside of the sealed seismometer compartment (48) is suspended from the top inner surface of the bell-shaped protective cover (49) by multiple cables, and the underside of the sealed seismometer compartment (48) extends beneath the opening of the bell-shaped protective cover (49) to sit flush with the underside of the submersion-coupling frame. The unhooking mechanism is provided on the function compartment (36) and is connected fixedly with the rim of the submersion-coupling frame by a fusible tension steel wire (24), thus fixing the function compartment (36) and the seismometer compartment to the rigid ring at the center of the submersion coupling frame. The seismograph is installed in the sealed seismometer compartment (48) and is thus seated on the seabed directly, whereby the severe distortion of horizontal signals recorded by the submarine seismograph can be effectively overcome without the use of multilayer coupling structures.

The assembly and release apparatus and method utilizes a C-shaped clip defining a channel and a smaller slot extending along the channel, both open at at least one end, attachable to a first location on a garment. A pin of the apparatus is slidably receivable in the channel through the open end to assemble the C-shaped clip and the pin together. The pin has a tab or strip that extends through the slot, for attaching the pin to a second location on the garment. The apparatus includes at least one detent element associated with one of the C-shaped clip and the pin, cooperatively engageable with the other of the C-shaped clip and the pin for retaining the pin in the channel, and releasable in a predetermined manner to allow slidably removing the pin from the channel through the open end, to provide a quiet and rapid manner of operation.

The invention relates to an accelerator pedal module having a pedal (2) and a restoring device (4) for the pedal (2) as well as a full load indicator (20, 11). In the full load position of the pedal (2), the restoring device (4) can be latched to the full load indicator (11). Furthermore, the invention relates to an accelerator pedal module full load indicator.

The invention provides a chained static synchronous compensator with an active power adjusting capacity. The chained static synchronous compensator with the active power adjusting capacity comprises three phases of cascading chain links, connection reactors and breakers. Each phase of the cascading chain link comprises n cascading units which are connected in series at the alternating current side. One ends of the three phases of the cascading units are connected to form a neutral point of the static synchronous compensator, and the other ends of the three phases of the cascading units are connected into a three-phase grid through the corresponding connection reactors and the corresponding breakers. The invention further provides a corresponding cascading unit. An STATCOM and a BESS are combined, the capacity of controlling active power and reactive power at the same time is achieved, grid connection of medium voltage and high voltage is achieved in a manner of cascading multiple cascading units, a power switch device which is low in voltage resistance is used for achieving energy conversion of high voltage levels, modularization and redundancy design are easy to achieve, the function of balancing a battery is achieved, meanwhile, a bidirectional DC/DC converter is introduced at the direct current side, and ensuring the cycle life of the battery is facilitated.

The present invention relates to organoalkoxysilane compositions which comprise at least one organoalkoxysilane S, and at least one anhydrous surfactant T, where the weight fraction of all of the organoalkoxysilanes S is 33% by weight, based on the weight of the organoalkoxysilane composition, and where the ratio of the weight sum of all of the organoalkoxysilanes S to the weight sum of all of the anhydrous surfactants T (S:T) has a value of from 5:1 to 1:2.

A roof module of a motor vehicle, wherein the roof module is manufactured from a plastic and a roof box device is integrally formed with the roof module in one piece.

A crossmember for supporting and limiting torsional forces of an engine unit relative to a mounting frame, particularly a vehicle body, wherein the crossmember is provided with at least one area or one device for introducing torsional forces into the crossmember.

The invention discloses an aircraft communication system, relates to the technical field of laser communication, and mainly aims to achieve laser communication between aircrafts and satellites. The aircraft communication system disclosed by the invention comprises at least one piece of aircraft-satellite laser communication terminal equipment, an electric control box, a rectification cover and a bracket, wherein the bracket has a damping function; the aircraft-satellite laser communication terminal equipment communicates with a satellite communication system through a laser link; the electriccontrol box is used for supplying power to the aircraft-satellite laser communication terminal equipment and used for providing control instructions to information streams; the rectification cover isof a structure which is transparent at least partially and is arranged on the outer side of the aircraft-satellite laser communication terminal equipment in a covering manner. The aircraft communication system is mainly applied to data transmission of aircrafts.

This invention relates to a low disturbance conversion supply, in which, a three-phase AC input is sent to a trigger control and rectified circuit of a thyristor, the control signal of which is generated by a computer control circuit, its rectified output is sent to a bridge output circuit, the output signal of which is sent to a short circuit box and sent to an output sampling and testing circuit, which sends the sampled signal for testing then sends the tested signal to a computer control circuit, At the same time, the system voltage is also sent to a computer control circuit via the system voltage input and measurement circuit, which generates an input control signal needed by a synchronous and blanking signal generation circuit.

The invention discloses a stop block on an automobile door, which consists of a stop arm (1) and a stop box body assembly which consists of a stop box cover (3) and a stop box (2); and one end of the stop arm (1) is provided with a stand (8) which is connected with the stop arm (1) through a rivet (7). The stop block is characterized in that the interior of the stop box assembly is provided with a plastic stand (5) and a rubber spring (4) which are evenly arranged at the two sides of the stop arm (1). With such technical proposal, the stop block has the advantages of simple structure and process, more advantageous in the quantity, weight and cost of spare parts than the traditional structure, and higher product reliability.

A system for the collection of observations is described which has particular application in the clinical research and aerospace industries. The system has a planning station, for preparing a work package of observations to be collected; a download station for downloading the work package to at least one primary capture tool, the primary capture tool being used to collect observations according to the work package autonomously; and an upload station, for uploading the observations from the at least one primary capture tool. The invention also concerns a method for collecting observations, as well as a graphical interface therefor. The invention make use of an atomic database, which obviates the need to reprogram the database when it is to be used for a different set of observations to be collected.

The invention discloses a ground station communication system, relates to the technical field of laser communication and mainly aims to achieve laser communication between the ground and a satellite.An aircraft communication system disclosed by the invention comprises at least one ground station laser communication terminal, wherein the ground station laser communication terminal communicates with the satellite; the ground station laser communication terminal comprises at least one ground station-satellite laser communication terminal device and communicates with the satellite through a laserlink based on the ground station-satellite laser communication terminal device; the ground station laser communication terminal further comprises a data communication interface and is connected witha public Internet network through the data interface. By adopting the system, communication can be carried out through the link between the ground station and the satellite, data of an aircraft in laser link connection with the satellite can be downloaded to the ground, and bidirectional communication of the aircraft with the ground can be achieved.

The invention provides an integrated point of interface (POI). The integrated POI comprises an upper cover having a first combining function, a cavity body that has a bridge circuit coupling function and is arranged below the upper cover, and a bottom cover that has a second combining function and is connected with the bottom of the cavity body. The integrated POI provided by the invention has the characteristics of small size and high space utilization rate.

An ignition system and a method for controlling an ignition system for a spark-ignited internal combustion engine are described, having a primary voltage generator for generating an ignition spark and a boost converter for maintaining an ignition spark. The method includes sending a signal from an engine control unit to the ignition system, in order to determine a predetermined ignition timing for triggering an ignition spark, sending an additional signal from the engine control unit to the ignition system, in order to determine a predetermined additional ignition timing for triggering an additional ignition spark, and sending a control signal for influencing the operating mode of the boost converter from the engine control unit to the ignition system between the signal and the additional signal.

A chassis for a rail vehicle, in particular with inboard wheel sets, with at least one transmission, at least one transversely mounted drive motor and at least one chassis frame, wherein the chassis frame includes at least one crossmember and at least a first longitudinal carrier and a second longitudinal carrier, where at least a first elastic bearing, a second elastic bearing and a third elastic bearing are arranged between the drive motor and the chassis frame, and where in each case one of the elastic bearings is arranged on at least one of the longitudinal carriers in order to provide advantageous construction conditions.

The invention relates to a device for reinforcing a supporting sub-frame for motor vehicles which is made up of two longitudinal spars (30) and at least one transverse spar (32, 34), wherein by means of radially projecting fixed mountings (36, 38) the links (14, 16, 20, 22) of wheel suspensions on both sides are articulated on the longitudinal spars (30) by means of rubber/metal sleeve bearings, and wherein at least in an articulation region of a link (14) the longitudinal spars (30) have a curvature of in particular approximately 90 DEG with a longitudinally extending section (30b) and a transversely extending section (30c). According to the invention the mountings (36, 38) are formed as two brackets, of which one is supported on the longitudinally extending section (30b) of the longitudinal spars (30) and the other is supported on the transversely extending section (30c).

The invention discloses a communication system, relates to the technical field of aviation and spaceflight, and mainly aims to increase the network transmission rate of an aircraft. The main technicalscheme is as follows: the communication system comprises a satellite communication system and an aircraft communication system; the satellite communication system comprises multiple satellites; eachsatellite carries an inter-satellite laser communication terminal device for inter-satellite communication, a to-air laser communication terminal device for communication between the satellite and theaircraft, and a to-ground laser communication terminal device for communication between the satellite and a ground station; the multiple communication satellites are in communication connection through a laser link based on the inter-satellite laser communication terminal device; and the aircraft communication system comprises a predetermined number of aircraft-satellite laser communication terminal devices for communication with the satellite, and performs communication connection with the satellite communication system through the laser link based on the aircraft-satellite laser communication terminal devices. The communication system disclosed by the invention is mainly used for air data transmission of the aircraft.