40results about How to "Solve uncontrollable problems" patented technology

The invention relates to a lower animal breeding device, particularly to a commercial damp dry solid lower animal breeding device, comprising a case shell frame having four-side outer wall, wherein drain air holes are arranged on the four-side outer wall of the shell frame; the integral shell frame is arranged on a concave cement base station having a drain interlayer; a soft inner bag is arranged in the shell frame; a breeding carrier is arranged in the soft inner bag; an inner bag bottom separating layer is arranged between the bottom of the soft inner bad and the breeding carrier, an inner bag separating layer is arranged between an inner wall of the soft inner bag and the breeding carrier. The invention has the effect of periodically effective waste discharge of six-side airing and five-side layering, keeps the solid breeding carrier in a good state.

The invention discloses a combined heat insulation light shielding cover structure for a star sensor. The structure comprises a cover body, a support seat and a light shielding ring. Each of the coverbody and the support seat is a hollow cylinder. The light shielding ring is a split type hollow circular ring. The light shielding ring used for heat dissipation and light elimination is installed onone end of the cover body. The support seat where a start sensor optical machine circuit box is assembled sleeves the other end of the cover body. According to the invention, by combining the cover body and the support seat, the structure of the star sensor light shielding cover is optimized; defects of complex structure, big weight, tedious assembly and disassembly and excessive heat transmission of the traditional star sensor are overcome; and by designing the light shielding ring, stray light and heat flows of spatial tracks are inhibited and difficulty that the traditional star sensor light shielding cover absorbs too much heat is overcome.

The invention aims at solving the problems that existing brake pad materials are unstable in frication performance, high in hardness, high in oscillation frequency, poor in automatic performance, uneven in frication and the like, and provides a novel modified prefabricated body carbon ceramic brake pad material and a manufacturingmethod thereof. The manufacturingmethod of the novel modified prefabricated body carbon ceramic brake pad material includes the steps ofusing a novel carbon fiber prefabricated body of a sandwich structure, preparing and processing fibers of a needled structure, manufacturing C / C porous bodies by adopting a slurry infiltration process, and introducing SiC-based, Si-based and B-based compounds into the carbon / ceramic porous prefabricated bodies;the puzzle that theresidual amount of Si is uncontrollable is effectively solved. According to the sandwich-shaped C / SiC brake material, stability of dry state frication performance is improved, the static friction coefficient is improved, and friction performance under a wet state condition does not attenuate.

The invention relates to a system for cultivating animals adapting to a culture pond and a method for cultivating the same. The cultivation system comprises the culture pond and a cultivating device arranged in the culture pond, wherein the cultivating device comprises an inner bracket on which an outer mesh bag provided with ventilating holes is supported and arranged, and the outer mesh bag is provided with an opening; and an air pipeline is arranged in the cultivating device, is provided with a plurality of inner air charging holes for the cultivating device, and is connected with an air breather. The invention also discloses the cultivation method for the cultivation system, which comprises the following steps: firstly, hanging the top of the cultivating device on a chief rope through a rope; secondly, hanging a heavy object which can adjust the ups and downs of the cultivating device on the bottom of the cultivating device; thirdly, semi-suspending the cultivating device in water; and fourthly, charging air in the cultivating device through the air pipeline of the air breather. In the cultivation process, when the water quality has abrupt changes, the cultivation system and the cultivation device can take the cultivated lower animals out of the pond quickly to avoid loss; and in the normal cultivation, the system and the device can keep the moderate air charge in a water pond so as to achieve that the cultivation conditions are controllable.

The invention discloses an aircraft lateral deviation correction system applied to a satellite signal unstable area. The system comprises a pseudo-satellite guidance resolving module, a microprocessormodule and a navigation ratio output module. The pseudo-satellite guidance resolving module is used for providing aircraft position and speed information at the current moment required for calculating overload required by lateral deviation for the microprocessor module when a satellite is lost; the navigation ratio output module is used for providing a navigation ratio changing in real time for the microprocessor module; the navigation ratio output module obtains a navigation ratio changing in real time according to the total range and the real-time lateral deviation distance when the aircraft is started and controlled and other information. Therefore, the guidance performance is improved, a target can enter the field of view range of the seeker when entering terminal guidance. In addition, since the navigation ratio is continuously changed at a small amplitude, large-amplitude vibration of the flight path cannot be caused, flight process is stable, and the final hit precision is high.

The invention discloses a composite extended-range aircraft capable of being applied to an unstable satellite signal area. A rocket range extending module, a bottom row range extending module, a rolling range extending module and a gliding range extending module are arranged in the aircraft at the same time. All the modules work cooperatively, work alternately in different flight stages accordingto a preset sequence and do not interfere with one another, and the range of the aircraft can be increased, so the final range of the aircraft is increased to the maximum extent. Besides, a processormodule and a quasi-satellite guidance resolving module are further arranged on the aircraft, and the quasi-satellite guidance resolving module is used for providing aircraft position and speed information at the current moment required by overload calculation for the processor module when the satellite is lost, so that the aircraft can still perform normal navigation guidance and cannot be out ofcontrol when the satellite is lost.

The invention discloses a satellite loss prevention remote guidance aircraft considering full-range coverage. The aircraft can strike a long-range target, a medium-range target and a short-range target, and is capable of avoiding out-of-control under the condition of staged satellite loss, thereby having important engineering significance. The remote guidance aircraft particularly comprises a decision making module and a central processing module, wherein the decision making module is used for selecting a guidance starting control module for executing work according to range information beforelaunching; and different guidance starting control modules can control different assembly modules to start to work, so that the corresponding assembly modules are controlled according to different ranges. The central processing module generates a rudder deviation instruction by receiving information transmitted by the assembly module and controls the aircraft to fly to a target, and a quasi-satellite guidance resolving sub-module capable of fitting a satellite signal during satellite loss is arranged in the satellite guidance module, so that the aircraft is ensured not to be out of control during satellite loss.

The invention relates to a lower animal breeding device, particularly to a commercial damp dry solid lower animal breeding device, comprising a case shell frame having four-side outer wall, wherein drain air holes are arranged on the four-side outer wall of the shell frame; the integral shell frame is arranged on a concave cement base station having a drain interlayer; a soft inner bag is arranged in the shell frame; a breeding carrier is arranged in the soft inner bag; an inner bag bottom separating layer is arranged between the bottom of the soft inner bad and the breeding carrier, an innerbag separating layer is arranged between an inner wall of the soft inner bag and the breeding carrier. The invention has the effect of periodically effective waste discharge of six-side airing and five-side layering, keeps the solid breeding carrier in a good state.

The invention relates to a prediction method of near alpha titanium alloy low-power coarse grain structure distribution. The prediction method comprises the following steps of S1 determining the structure of a material under a selected process condition; S2 carrying out statistical analysis on the microscopic structure of the core of the thermal compression test piece under the corresponding process, and carrying out statistical analysis on the grain size; S3 establishing a quantitative prediction model of the original grain size; and S4 on the basis of microscopic structure critical conditionD beta>=D0 formed by the low-power coarse crystals, realizing the visual prediction of near alpha-titanium alloy low-power coarse crystal distribution through secondary development and numerical simulation analysis of finite element software. The prediction method for the macroscopic structure distribution of the near alpha-titanium alloy can effectively reveal the microscopic structure change ofthe near alpha-titanium alloy forge piece after forging heat treatment, and particularly realizes visual prediction of the original grain coarsening and the macroscopic structure distribution causedby the original grain coarsening. The forming process is optimized, the low-power coarse grain area is reduced, and the prediction result is accurate.

The invention discloses a novel solid-state nano-pore structure, and relates to the technical field of micro-nano medical detection application. The novel solid-state nano-pore structure is applied toaccurately controlling a modification position of a biomolecule. The solid-state nano-pore structure includes a sandwich structure nano-pore array; the nano-pore array consists of a top layer, a middle layer and a bottom layer arranged sequentially; each of the top layer and the bottom layer is a protective layer of the nano-pore array; and the middle layer is a biomolecule modification positionlayer. The novel solid-state nano-pore structure is simple in structure; by using a difference of a binding force between a material in a nano-pore sandwich structure and a functional group of the biomolecule, the accurate control on the modulation position of the biomolecule is implemented, thus being beneficial to improving the detection accuracy of the biomolecule; and the novel solid-state nano-pore structure has a wide use prospect in the field of accurate medical detection.

The invention discloses an aircraft side deviation correction system applied to an area where satellite signals are unstable. The system includes a quasi-satellite guidance calculation module, a microprocessor module and a navigation ratio output module. The quasi-satellite guidance calculation module is used for When the star is lost, the microprocessor module is provided with the aircraft position and speed information required by the overload at the present moment for calculating the side deviation; the navigation ratio of the real-time change is provided for the microprocessor module by the navigation ratio output module, and the navigation ratio output is The module obtains the real-time changing navigation ratio according to the total range, real-time lateral distance and other information when the aircraft is controlled, so as to improve its guidance performance and ensure that the target enters the field of view of the seeker when it enters the terminal guidance. In addition, since the navigation ratio changes continuously in a small range, it will not cause large vibrations in the flight path, ensuring a stable flight process and high final hit accuracy.

A slag cooling device applicable to dry slag discharge machines provided by the invention comprises a cooling device (8) and a control system (10). According to the slag cooling device applicable to dry slag discharge machines, low-temperature purified flue gas after desulfurization by a flue gas desulfurization device replaces natural wind as a cooling medium of slag and a dry slag discharge machine, and the amount of low-temperature purified flue gas feeding into the dry slag discharge machine is adjusted automatically according to the temperatures of a main heater and a reheater of a boiler, the temperature of slag, and the pressures in the lower part of a dry bottom hopper and inside the dry slag discharge machine. Therefore, the situation in which a large amount of unorganized natural wind enters the hearth to affect normal combustion organizations is avoided, and the economic performance of unit operation is improved while cooling of slag and the dry slag discharge machine is realized.

The invention discloses an audio conference security system and a security method using the echo cancellation function. The system is composed of a control system and a venue system. The power amplifier is composed of; the venue system is composed of speakers, earphones and microphones. The processor has two sound cards and is equipped with audio conference security software; the first sound card has the function of echo cancellation. The software is composed of noise playback module, audio processing module and pure voice output module. The method is that the audio conference security software plays noise, collects noisy voice and transmits it to the No. 1 sound card for echo cancellation and denoising, and the audio processing module removes residual noise from the voice signal after echo cancellation and denoising. The invention solves the problem that the anti-eavesdropping device has single eavesdropping means and the sound wave propagation range is uncontrollable, and can effectively ensure that the content of the meeting is not eavesdropped and the communication is not affected.

The invention discloses an audio conference safety secrecy system and method. The audio conference safety secrecy system is composed of a control system and a meeting place system. The control system is composed of a processor, a multi-path headset distributor, a conference system master controller and a multi-path audio power amplifier. The meeting place system is composed of loudspeaker boxes, headsets and microphones. The processor is provided with two sound cards and audio conference security secrecy software. The software is composed of a noise playing module, a noisy voice collection module, an audio processing module and a pure voice output module. The audio conference safety secrecy method includes the steps that the audio conference security secrecy software plays noise, collects and processes the noisy voice and sequentially transmits pure voice signals to the second sound card, the multi-path headset distributor and the headsets, and conventioneers hear information of the meeting place through the headsets. The audio conference safety secrecy system and method solve the problems that the telephone tapping means adopted by anti-eavesdrop equipment is singular, and the sound wave spreading range is uncontrollable, and it can be effectively guaranteed that the conference content is not eavesdropped, and normal communication of the conventioneers is not affected.

The invention discloses a compound range-extending aircraft that can be applied to areas where satellite signals are unstable. The aircraft is simultaneously equipped with a rocket range-extending module, a bottom row extending-range module, a rolling-range extending module and a gliding range-extending module. Each module They work together, and work alternately in different flight stages according to a predetermined order, without interfering with each other, which can improve the range of the aircraft, so that the final range of the aircraft can be improved to the greatest extent; in addition, a processor is also set on the aircraft module and the quasi-satellite guidance calculation module, the quasi-satellite guidance calculation module is used to provide the processor module with the aircraft position and speed information at the current moment required for calculating the overload required when the star is lost, so that the aircraft It can still navigate and guide normally without losing control.