CN114044102A - Marine locater installation device - Google Patents

Marine locater installation device Download PDF

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Publication number
CN114044102A
CN114044102A CN202111083344.XA CN202111083344A CN114044102A CN 114044102 A CN114044102 A CN 114044102A CN 202111083344 A CN202111083344 A CN 202111083344A CN 114044102 A CN114044102 A CN 114044102A
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China
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type
positioning
gravity compensation
magnetic force
magnetic suspension
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CN202111083344.XA
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CN114044102B (en
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杜逢佳
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Jiangsu Yaoxin Information Technology Co ltd
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Jiangsu Yaoxin Information Technology Co ltd
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B49/00—Arrangements of nautical instruments or navigational aids
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01D—SEPARATION
    • B01D53/00—Separation of gases or vapours; Recovering vapours of volatile solvents from gases; Chemical or biological purification of waste gases, e.g. engine exhaust gases, smoke, fumes, flue gases, aerosols
    • B01D53/26—Drying gases or vapours
    • B01D53/261—Drying gases or vapours by adsorption
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01D—SEPARATION
    • B01D53/00—Separation of gases or vapours; Recovering vapours of volatile solvents from gases; Chemical or biological purification of waste gases, e.g. engine exhaust gases, smoke, fumes, flue gases, aerosols
    • B01D53/26—Drying gases or vapours
    • B01D53/265—Drying gases or vapours by refrigeration (condensation)
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/02—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
    • F16F15/03—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using magnetic or electromagnetic means

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Analytical Chemistry (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Oil, Petroleum & Natural Gas (AREA)
  • General Chemical & Material Sciences (AREA)
  • Thermal Sciences (AREA)
  • Acoustics & Sound (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Electromagnetism (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Combustion & Propulsion (AREA)
  • Ocean & Marine Engineering (AREA)
  • Magnetic Bearings And Hydrostatic Bearings (AREA)
  • Drying Of Gases (AREA)

Abstract

The invention discloses a mounting device for a marine locator, which comprises a main body, a multi-ring gyroscope type magnetic force micro-positioning type stabilizing device, a magnetic suspension gravity compensation type damping zero-damage type fixing device, a low-temperature drying type air flow guiding type air suction device, a liquid nitrogen desublimation frost-forming type capillary form contact type dehumidifying device and a multi-dimensional rotary type porous material rotational flow adsorption device. The invention belongs to the technical field of installation of marine positioning instruments, and particularly relates to a mounting device for a marine positioning instrument; the technical theory of weight compensation principle (combining a certain object with another object capable of providing force to compensate the weight of the object and realizing weight compensation through interaction with the environment) is creatively applied to the technical field of the installation of the marine locator.

Description

Marine locater installation device
Technical Field
The invention belongs to the technical field of installation of marine positioning instruments, and particularly relates to a mounting device for a marine positioning instrument.
Background
The marine locator mounting device mainly plays a role in fixing the locator, so that people can conveniently use the locator, and along with the continuous development of the navigation business in China, the requirements of people on the locator are higher and higher, so that the requirements of people on the fixing device are stricter and stricter; there is certain drawback in current fixing device when using, at first, traditional fixing device can only play single fixed action, stability can not be high, certain adverse effect has, secondly, because the locater is installed on the ship, because marine moisture is heavier, traditional fixing device can not play damp-proofing effect, certain adverse effect has, in addition, the locator belongs to precision equipment, the hull will lead to it to receive the damage if receiving violent vibrations, certain adverse effect has, certain influence has been brought to people's use, for this reason, we provide a marine locater installation device.
Disclosure of Invention
In order to solve the existing problems, the invention provides a mounting device of a marine locator, which creatively applies the technical theory of weight compensation principle (combining a certain object with another object capable of providing force to compensate the weight of the object and realizing weight compensation through the interaction with the environment) to the technical field of mounting of the marine locator without any clamp, because the locator belongs to precision equipment, a ship body can be damaged if being severely vibrated, has certain adverse effect and brings certain influence to the using process of people, the repulsion of a primary electromagnet fixed by a damping type magnetic suspension gravity compensation type primary electromagnetic winding is adjusted by electrifying the damping type magnetic suspension gravity compensation type primary electromagnetic winding, and the repulsion of a primary electromagnet fixed by a damping type magnetic suspension gravity compensation type secondary electromagnetic winding is adjusted by electrifying the damping type magnetic suspension gravity compensation type secondary electromagnetic winding The repulsion force of the secondary electromagnet is fixed in a formula mode, so that the transverse magnetic suspension gravity compensation type damping primary reinforcing plate is driven to move, the repulsion force of the damping type magnetic suspension gravity compensation type fixed secondary electromagnetic winding is adjusted by electrifying the damping type magnetic suspension gravity compensation type fixed secondary electromagnetic winding, so that the transverse magnetic suspension gravity compensation type damping secondary reinforcing plate is driven to move, the positioning instrument is fixed and protected, and the technical problem that the positioning instrument is easy to damage if a ship body vibrates violently is solved; for the stability concept of the positioning instrument, a dynamic characteristic principle (an object is automatically adjusted to enable the performance of the positioning instrument in each action and stage to be optimal or an object structure is divided into a plurality of components which can be changed and matched with each other or an immovable object can be moved and can be adapted) and a nesting principle (one object is embedded into a second object and then the two objects are embedded into a third object) technical theory are innovatively applied to the technical field of installation of the marine positioning instrument; the technical theory of physical or chemical parameter change principle (changing physical state of object, changing concentration or viscosity of object, changing flexibility of object, changing temperature or volume of object) and porous material principle (making object change into porous material or adding porous object, if the object has porous structure, using porous structure to introduce useful substance or function) is creatively applied to the technical field of installation of marine locator The damp capillary tube is used for carrying out desublimation and frost formation, and the dried air is discharged from the main body through the cyclone adsorption type multidimensional rotary three-level connecting tube, so that the problem that the traditional fixing device cannot play a damp-proof role is solved.
The technical scheme adopted by the invention is as follows: the invention relates to a mounting device of a marine locator, which comprises a main body, a multi-ring gyroscope type magnetic micro-positioning type stabilizing device, a magnetic suspension gravity compensation type damping zero-damage type fixing device, a low-temperature drying type air flow guiding type air suction device, a liquid nitrogen desublimation frost-forming type capillary form contact type dehumidifying device and a multidimensional type rotary type porous material rotational flow suction device, the multi-ring gyroscope type magnetic force micro-positioning type stabilizing device is arranged on the main body, the magnetic suspension gravity compensation type damping zero-damage type fixing device is arranged in the multi-ring gyroscope type magnetic force micro-positioning type stabilizing device, the low-temperature drying type air flow guiding type air suction device is arranged on the main body, the liquid nitrogen desublimation frost-forming type capillary contact type dehumidifying device is arranged in the main body, the multi-dimensional rotary porous material cyclone adsorption device is arranged in the liquid nitrogen desublimation frost-forming capillary contact type dehumidification device; the main body comprises a magnetic suspension gravity compensation type damping zero damage type fixed box and a liquid nitrogen desublimation frost-forming type capillary form contact type dehumidification adsorption hole, the magnetic suspension gravity compensation type damping zero damage type fixed box is arranged on the main body, and the liquid nitrogen desublimation frost-forming type capillary form contact type dehumidification adsorption hole is arranged on the magnetic suspension gravity compensation type damping zero damage type fixed box; the multi-ring gyroscope type magnetic force micro-positioning type stabilizing device comprises a multi-ring gyroscope type magnetic force micro-positioning type primary stabilizing ring, a multi-ring gyroscope type magnetic force micro-positioning type secondary stabilizing ring, a multi-ring gyroscope type magnetic force micro-positioning type tertiary stabilizing ring, a self-positioning type friction lossless type primary sliding groove, a self-positioning type friction lossless type primary pulley, a self-positioning type friction lossless type secondary pulley, a friction lossless type magnetic force micro-positioning type primary bearing, a friction lossless type magnetic force micro-positioning type secondary bearing, a friction lossless type magnetic force micro-positioning type tertiary bearing, a friction lossless type magnetic force micro-positioning type quaternary bearing, a multi-ring gyroscope type magnetic force micro-positioning type fixing frame, a magnetic force micro-positioning type multi-ring gyroscope type primary magnet, a magnetic force micro-positioning type multi-ring gyroscope type secondary magnet, a magnetic force micro-positioning type multi-ring gyroscope type tertiary magnet, a magnetic force micro-positioning type multi-ring gyroscope type quaternary magnet, a self-positioning type magnetic force micro-positioning type four-stage magnet, Magnetic force micro-positioning type multi-ring gyroscope type five-level magnet and magnetic force micro-positioning type multi-ring gyroscope type six-level magnet, the multi-ring gyroscope type magnetic force micro-positioning type one-level stable ring is arranged on a magnetic suspension gravity compensation type damping zero damage type fixed box, the self-positioning type friction lossless type one-level chute is arranged in the multi-ring gyroscope type magnetic force micro-positioning type one-level stable ring, one end of the self-positioning type friction lossless type one-level pulley is slidably arranged in the self-positioning type friction lossless type one-level chute, one end of the friction lossless type magnetic force micro-positioning type one-level bearing is arranged at the other end of the self-positioning type friction lossless type one-level pulley, one end of the self-positioning type friction lossless type two-level pulley is slidably arranged in the self-positioning type friction lossless type one-level chute, one end of the friction lossless type magnetic force micro-positioning type two-level bearing is arranged at the other end of the self-positioning type friction lossless type two-level pulley, the other end of the lossless magnetic force micro-positioning type first-level bearing of friction is arranged on the side wall of the multi-ring gyroscope magnetic force micro-positioning type second-level stabilizing ring, the other end of the lossless magnetic force micro-positioning type second-level bearing of friction is arranged on the other side wall of the multi-ring gyroscope magnetic force micro-positioning type second-level stabilizing ring, the upper end of the inner wall of the multi-ring gyroscope magnetic force micro-positioning type second-level stabilizing ring is arranged on one end of the lossless magnetic force micro-positioning type third-level bearing of friction, the lower end of the inner wall of the multi-ring gyroscope magnetic force micro-positioning type second-level stabilizing ring is arranged on the upper end of the outer side wall of the lossless magnetic force micro-positioning type third-level stabilizing ring, the lower end of the outer side wall of the multi-ring gyroscope magnetic force micro-positioning type fourth-level bearing of friction is arranged on the other end of the four-level magnetic force micro-positioning type fourth-level bearing of friction, on the inner wall of the tertiary stabilizing ring of the little location type of multi-ring gyroscope formula magnetic force is located to the little location type mount of multi-ring gyroscope formula magnetic force, the little location type multi-ring gyroscope formula secondary magnet of magnetic force is located on the lateral wall of the little location type mount of multi-ring gyroscope formula magnetic force, the little location type multi-ring gyroscope formula primary magnet of magnetic force is located on the magnetic levitation gravity compensation zero damage type fixed box inside wall, the little location type multi-ring gyroscope formula four-level magnet of magnetic force is located on another lateral wall of the little location type mount of multi-ring gyroscope formula magnetic force, the little location type multi-ring gyroscope formula tertiary magnet of magnetic force is located on another inside wall of the magnetic levitation gravity compensation zero damage type fixed box, the little location type multi-ring gyroscope formula six-level magnet of magnetic force is located the lower extreme of the little location type mount of multi-ring gyroscope formula magnetic force, the little location type multi-ring gyroscope formula five-level magnet of magnetic force is located the magnetic levitation gravity compensation zero damage type damping zero damage type fixed box inside wall of magnetic force When the motion amplitude of the ship body is small, the magnetic force micro-positioning type multi-ring gyroscope type six-level magnet and the magnetic force micro-positioning type multi-ring gyroscope type five-level magnet are mutually attracted to enable the positioning instrument to be vertically downward, the magnetic force micro-positioning type multi-ring gyroscope type primary magnet and the magnetic force micro-positioning type multi-ring gyroscope type secondary magnet are mutually attracted, the magnetic force micro-positioning type multi-ring gyroscope type tertiary magnet and the magnetic force micro-positioning type multi-ring gyroscope type four-level magnet are mutually attracted to enable the positioning instrument to be in a horizontal position, when the left-right shaking amplitude of the ship body is overlarge, the magnetic suspension gravity compensation type damping zero damage type fixing box drives the multi-ring gyroscope type magnetic force micro-positioning type primary stabilizing ring to shake left and right, the self-positioning type friction lossless primary sliding groove to shake left and right, the self-positioning type friction lossless primary pulley and the self-positioning type friction lossless secondary pulley rotate but the positions are unchanged, when the ship body shakes back and forth, the magnetic suspension gravity compensation type damping zero damage type fixing box drives the multi-ring gyroscope type magnetic force micro-positioning type primary stabilizing ring to shake back and forth, the multi-ring gyroscope type magnetic force micro-positioning type primary stabilizing ring shakes back and forth to drive the self-positioning type friction nondestructive type primary pulley and the self-positioning type friction nondestructive type secondary pulley to shake back and forth, the self-positioning type friction nondestructive type first-stage pulley shakes back and forth to drive the friction nondestructive type magnetic force micro-positioning type primary bearing to rotate, the self-positioning type friction nondestructive type secondary pulley shakes back and forth to drive the friction nondestructive type magnetic force micro-positioning type secondary bearing to rotate, the positions of the friction nondestructive type magnetic force micro-positioning type primary bearing and the friction nondestructive type magnetic force micro-positioning type secondary bearing are unchanged, when the ship body shakes in a reciprocating self-transmission manner, the magnetic suspension gravity compensation type damping zero damage type fixing box shakes to drive the multi-ring gyroscope type micro-magnetic force positioning type primary stabilizing ring to shake, the multi-ring gyroscope type magnetic force micro-positioning type first-stage stabilizing ring shakes to drive the friction lossless type magnetic force micro-positioning type first-stage bearing to shake, the friction lossless type magnetic force micro-positioning type first-stage bearing shakes to drive the multi-ring gyroscope type magnetic force micro-positioning type second-stage stabilizing ring to shake, the friction lossless type magnetic force micro-positioning type third-stage bearing and the friction lossless type magnetic force micro-positioning type fourth-stage bearing rotate, the positions of the friction lossless type magnetic force micro-positioning type third-stage bearing and the friction lossless type magnetic force micro-positioning type fourth-stage bearing are unchanged, and therefore the stability of the position finder is improved.
Further, the magnetic suspension gravity compensation type damping zero damage type fixing device comprises a magnetic suspension gravity compensation type damping zero damage type fixed primary sliding groove, a magnetic suspension gravity compensation type damping zero damage type fixed secondary sliding groove, a transverse magnetic suspension gravity compensation type damping primary additional plate, a transverse magnetic suspension gravity compensation type damping secondary additional plate, a friction lossless type transverse magnetic suspension gravity compensation type third-level pulley, a friction lossless type transverse magnetic suspension gravity compensation type fourth-level pulley, a damping type magnetic suspension gravity compensation type fixed primary electromagnet, a damping type magnetic suspension gravity type fixed secondary electromagnet, a damping type magnetic suspension gravity compensation type fixed primary electromagnetic winding, a damping type magnetic suspension gravity compensation type fixed third-level electromagnetic winding, a damping type magnetic suspension gravity compensation type fixed primary electromagnet, a damping type magnetic suspension gravity compensation type fixed third-level electromagnetic winding, The magnetic suspension gravity compensation type damping zero damage type fixed first-level extension pipe, the magnetic suspension gravity compensation type damping zero damage type fixed second-level extension pipe, the magnetic suspension gravity compensation type damping zero damage type fixed third-level extension pipe and the magnetic suspension gravity compensation type damping zero damage type fixed fourth-level extension pipe, the magnetic suspension gravity compensation type damping zero damage type fixed first-level sliding chute is arranged in the upper end wall of the multi-ring gyroscope type magnetic force micro-positioning type fixing frame, the magnetic suspension gravity compensation type damping zero damage type fixed second-level sliding chute is arranged in the lower end wall of the multi-ring gyroscope type magnetic force micro-positioning type fixing frame, one end of the friction nondestructive type transverse magnetic suspension gravity compensation type third-level pulley is slidably arranged in the magnetic suspension gravity compensation type damping zero damage type fixed first-level sliding chute, one end of the transverse magnetic suspension gravity compensation type damping first-level reinforcing plate is arranged at the other end of the friction nondestructive type transverse magnetic suspension gravity compensation type third-level pulley, one end of the friction lossless type transverse magnetic suspension gravity compensation type four-stage pulley is slidably arranged in a magnetic suspension gravity compensation type zero-damage fixed second-stage chute, the other end of the friction lossless type transverse magnetic suspension gravity compensation type four-stage pulley is arranged at the other end of a transverse magnetic suspension gravity compensation type damping first-stage additional plate, the damping type magnetic suspension gravity compensation type fixed first-stage electromagnetic winding is arranged on the inner wall of a multi-ring gyroscope type magnetic force micro-positioning type fixing frame, the damping type magnetic suspension gravity compensation type fixed second-stage electromagnetic winding is arranged on the inner wall of the multi-ring gyroscope type magnetic force micro-positioning type fixing frame, the damping type magnetic suspension gravity compensation type fixed first-stage electromagnet is arranged on the side wall of the transverse magnetic suspension gravity compensation type damping first-stage additional plate, the damping type magnetic suspension gravity compensation type fixed second-stage electromagnet is arranged on the side wall of the transverse magnetic suspension gravity compensation type damping first-stage additional plate, the fixed second grade telescopic tube of magnetic suspension gravity compensation type shock attenuation zero damage type is located the inner wall upper end of many ring gyroscope formula magnetic force micro-positioning type mount, the one end of the fixed first order telescopic tube of magnetic suspension gravity compensation type shock attenuation zero damage type slides and locates in the fixed second grade telescopic tube of magnetic suspension gravity compensation type shock attenuation zero damage type, the other end of the fixed first order telescopic tube of magnetic suspension gravity compensation type shock attenuation zero damage type is located to horizontal magnetic suspension gravity compensation type shock attenuation two-level addition board, the one end of the fixed fourth grade telescopic tube of magnetic suspension gravity compensation type shock attenuation zero damage type locates the inner wall upper end of the fixed many ring gyroscope formula magnetic force micro-positioning type mount, the one end of the fixed third grade telescopic tube of magnetic suspension gravity compensation type shock attenuation zero damage type slides and locates in the fixed fourth grade telescopic tube of magnetic suspension gravity compensation type shock attenuation zero damage type, the other end of the fixed third grade telescopic tube of magnetic suspension gravity compensation type shock attenuation zero damage type is located to horizontal magnetic suspension gravity compensation type shock attenuation zero damage type On the gravity compensation formula shock-proof type second grade addendum plate, the fixed tertiary electromagnetic winding of shock-proof type magnetic suspension gravity compensation formula is located the inner wall upper end of many ring gyroscope formula magnetic force micro-positioning type mount, the fixed tertiary electro-magnet of shock-proof type magnetic suspension gravity compensation formula is located on the horizontal magnetic suspension gravity compensation formula shock-proof type second grade addendum plate, start the zero damage type fixing device of magnetic suspension gravity compensation formula shock attenuation, adjust and the repulsion of the fixed primary electro-magnet of shock-proof type magnetic suspension gravity compensation formula through to the circular telegram of the fixed primary electromagnetic winding of shock-proof type magnetic suspension gravity compensation formula, adjust and the repulsion of the fixed secondary electro-magnet of shock-proof type magnetic suspension gravity compensation formula through to the circular telegram of the fixed secondary electromagnetic winding of shock-proof type magnetic suspension gravity compensation formula, thereby drive horizontal magnetic suspension gravity compensation formula shock-proof type first grade addendum plate motion, adjust and shock-proof type gravity compensation formula magnetic suspension gravity compensation formula through to the circular telegram of the fixed secondary electromagnetic winding of shock-proof type magnetic suspension gravity compensation formula Repulsion of the fixed tertiary electro-magnet of formula, thereby drive horizontal magnetic suspension gravity compensation formula shock attenuation type second grade and add the board motion, thereby fixed locater, the fixed one-level telescopic pipe of the zero damage type of magnetic suspension gravity compensation formula shock attenuation zero damage is mutually supported with the fixed second grade telescopic pipe of the zero damage type of magnetic suspension gravity compensation formula shock attenuation zero damage, the fixed three-level telescopic pipe of the zero damage type of magnetic suspension gravity compensation formula shock attenuation zero damage is mutually supported and is had the limiting displacement to horizontal magnetic suspension gravity compensation formula shock attenuation type second grade and add the board to the flexible pipe of the fixed level four of the zero damage type of magnetic suspension gravity compensation formula shock attenuation, when the hull striking produces violent vibrations, the locater can rely on the repulsion of magnetic suspension to carry out the shock attenuation buffering, thereby protect the locater.
Further, the low-temperature drying type air flow guiding type air suction device comprises a low-temperature drying type air flow guiding type air suction primary motor, a low-temperature drying type air flow guiding type air suction primary fan, an air flow guiding type low-temperature drying type primary gear, an air flow guiding type low-temperature drying type secondary gear, an air flow guiding type low-temperature drying type primary driving rod, a friction nondestructive type air flow guiding type five-stage bearing, a low-temperature drying type air flow guiding type air suction primary fixing piece, a low-temperature drying type air flow guiding type air suction primary fixing box and a low-temperature drying type air flow guiding type air suction primary air suction hole, wherein the low-temperature drying type air flow guiding type air suction primary fixing box is arranged in the magnetic suspension gravity compensation type damping zero damage type fixing box, and the low-temperature drying type air flow guiding type air suction primary air suction hole is arranged on the low-temperature drying type air flow guiding type air suction primary fixing box, the utility model discloses a low temperature drying formula air current guide type one-level mounting that induced drafts, including low temperature drying formula air current guide type one-level fixed case that induced drafts, on the inner wall of low temperature drying formula air current guide type one-level fixed case was located to low temperature drying formula air current guide type five-level bearing of friction lossless, low temperature drying formula air current guide type one-level motor that induced drafts was located on the lateral wall of low temperature drying formula air current guide type one-level fixed case, the output that low temperature drying formula air current guide type induced drafts the one-level motor is located to the one end of air current guide type one-level actuating lever, the other end of air current guide type low temperature drying formula one-level actuating lever is located on the five-level bearing of friction lossless type air current guide type, air current guide type low temperature drying formula one-level actuating lever rotates and locates on low temperature drying formula air current guide type one-level mounting that induced drafts, air current guide type one-level drive rod rotates and locates the one-level fixed case that induced drafts of low temperature drying formula air current guide type On the piece, the airflow guide type low-temperature drying type secondary gear is sleeved on the airflow guide type low-temperature drying type primary driving rod, the airflow guide type low-temperature drying type primary gear is sleeved on one end of the airflow guide type low-temperature drying type primary driving rod, the low-temperature drying type airflow guide type suction primary fan is arranged at the other end of the airflow guide type low-temperature drying type primary driving rod, and the airflow guide type low-temperature drying type primary gear and the airflow guide type low-temperature drying type secondary gear are connected in a meshing rotation mode.
Further, the liquid nitrogen desublimation frost-forming type capillary form contact type dehumidification device comprises a liquid nitrogen desublimation frost-forming type capillary form contact type dehumidification capillary net, a liquid nitrogen desublimation frost-forming type capillary form contact type dehumidification capillary blade, a liquid nitrogen desublimation frost-forming type capillary form contact type dehumidification capillary, a capillary form contact type dehumidification liquid nitrogen desublimation frost-forming type liquid nitrogen tank, a capillary form contact type dehumidification liquid nitrogen desublimation frost-forming type circulating pump, a capillary form contact type dehumidification liquid nitrogen desublimation frost-forming type primary connecting pipe and a capillary form contact type dehumidification liquid nitrogen desublimation frost-forming type secondary connecting pipe, wherein the liquid nitrogen desublimation frost-forming type capillary form contact type dehumidification capillary net is arranged in the low-temperature dry type air flow guiding type primary air suction primary fixing box, and the liquid nitrogen desublimation frost-forming type capillary form contact type dehumidification capillary blade is arranged on the liquid nitrogen desublimation frost-forming type capillary form contact type dehumidification capillary net in a penetrating manner, the liquid nitrogen desublimation frosting type capillary form contact type dehumidifying capillary tube is communicated with and arranged on liquid nitrogen desublimation frosting type capillary form contact type dehumidifying capillary blades, the capillary form contact type dehumidifying liquid nitrogen desublimation frosting type liquid nitrogen tank is arranged on one side of the low-temperature drying type air flow guide type air suction primary fixed box, one end of the capillary form contact type dehumidifying liquid nitrogen desublimation frosting type primary connecting tube is communicated with and arranged at the input end of the liquid nitrogen desublimation frosting type capillary form dehumidifying capillary network, the other end of the capillary form contact type dehumidifying liquid nitrogen desublimation frosting type primary connecting tube is communicated with and arranged at the output end of the capillary form contact type dehumidifying liquid nitrogen desublimation frosting type liquid nitrogen tank, the capillary form contact type dehumidifying liquid nitrogen desublimation frosting type circulating pump is arranged on the capillary form contact type dehumidifying liquid nitrogen desublimation frosting type primary connecting tube, one end of the capillary form contact type dehumidifying liquid nitrogen desublimation frosting type secondary connecting tube is communicated with and arranged at the output end of the liquid nitrogen desublimation frosting type dehumidifying liquid nitrogen desublimation frosting type capillary form contact type capillary form dehumidifying liquid nitrogen frosting type capillary network The other end of the capillary form contact type dehumidification liquid nitrogen desublimation frost-forming type secondary connecting pipe is communicated with the input end of the capillary form contact type dehumidification liquid nitrogen desublimation frost-forming type liquid nitrogen tank.
Further, the multi-dimensional rotary type porous material cyclone adsorption device comprises a multi-dimensional rotary type porous material cyclone adsorption first-stage bearing, a multi-dimensional rotary type porous material cyclone adsorption second-stage bearing, a multi-dimensional rotary type porous material cyclone adsorption third-stage gear, a multi-dimensional rotary type porous material cyclone adsorption fourth-stage gear, a porous material cyclone adsorption multi-dimensional rotary type first-stage adsorption pipe, a porous material cyclone adsorption multi-dimensional rotary type first-stage adsorption hole, a porous material cyclone adsorption multi-dimensional rotary type first-stage air pump, a cyclone adsorption multi-dimensional rotary type third-stage connecting pipe, a cyclone adsorption multi-dimensional rotary type second-stage motor and a multi-dimensional rotary type porous material cyclone adsorption fixing piece, wherein the multi-dimensional rotary type porous material cyclone adsorption fixing piece is arranged in a low-temperature drying type air flow guiding type suction first-stage fixing box, the multi-dimensional rotary type porous material cyclone adsorption primary bearing is arranged on the multi-dimensional rotary type porous material cyclone adsorption fixing piece, one end of the porous material cyclone adsorption type multi-dimensional rotary type primary adsorption pipe is arranged on the multi-dimensional rotary type porous material cyclone adsorption primary bearing, the porous material cyclone adsorption type multi-dimensional rotary type primary adsorption hole is arranged on the porous material cyclone adsorption type multi-dimensional rotary type primary adsorption pipe, the multi-dimensional rotary type porous material cyclone adsorption four-stage gear is sleeved on the shaft of the porous material cyclone adsorption type multi-dimensional rotary type primary adsorption pipe, the multi-dimensional rotary type porous material cyclone adsorption secondary bearing is communicated with the lower end of the porous material cyclone adsorption type multi-dimensional rotary type primary adsorption pipe, one end of the cyclone adsorption type multi-dimensional rotary type three-stage connecting pipe is communicated with the multi-dimensional rotary type porous material cyclone adsorption secondary bearing, the rotational flow adsorption type multi-dimensional rotary three-stage connecting pipe is arranged on the inner side wall of the magnetic suspension gravity compensation type damping zero-damage type fixed box, the porous material rotational flow adsorption type multi-dimensional rotary one-stage air pump is arranged on the rotational flow adsorption type multi-dimensional rotary three-stage connecting pipe, the other end of the rotational flow adsorption type multi-dimensional rotary three-stage connecting pipe is arranged outside the magnetic suspension gravity compensation type damping zero-damage type fixed box, the rotational flow adsorption type multi-dimensional rotary two-stage motor is arranged on the inner side of the magnetic suspension gravity compensation type damping zero-damage type fixed box, the multi-dimensional rotary porous material rotational flow adsorption three-stage gear is arranged at the output end of the rotational flow adsorption type multi-dimensional rotary two-stage motor, and the multi-dimensional rotary porous material rotational flow adsorption three-stage gear and the multi-dimensional rotary porous material rotational flow adsorption four-stage gear are in meshed rotation connection, when the sea humidity is too high, the low-temperature drying type air flow guiding type air suction device is started, the output end of a low-temperature drying type air flow guiding type air suction primary motor rotates to drive an air flow guiding type low-temperature drying type primary driving rod to rotate, the air flow guiding type low-temperature drying type primary driving rod rotates to drive an air flow guiding type low-temperature drying type secondary gear to rotate, the air flow guiding type low-temperature drying type secondary gear rotates to drive an air flow guiding type low-temperature drying type primary gear to rotate, the air flow guiding type low-temperature drying type primary gear rotates to drive an air flow guiding type low-temperature drying type primary driving rod to rotate, the air suction liquid nitrogen is condensed into a frost type capillary form contact type dehumidifying device, the liquid nitrogen is condensed into frost type capillary form contact type dehumidifying capillary net, The liquid nitrogen desublimation frost-forming capillary form contact type dehumidification capillary blade and the liquid nitrogen desublimation frost-forming capillary form contact type dehumidification capillary are filled with flowing liquid nitrogen, the multidimensional rotary porous material rotational flow adsorption device is started, the output end of the rotational flow adsorption type multidimensional rotary secondary motor rotates to drive the multidimensional rotary porous material rotational flow adsorption tertiary gear to rotate, the multidimensional rotary porous material rotational flow adsorption tertiary gear rotates to drive the multidimensional rotary porous material rotational flow adsorption quaternary gear to rotate, the multidimensional rotary porous material rotational flow adsorption quaternary gear rotates to drive the porous material rotational flow adsorption type multidimensional rotary primary adsorption tube to rotate, the porous material rotational flow adsorption type multidimensional rotary primary air pump is started to adsorb moist air through the porous material rotational flow adsorption type multidimensional rotary primary adsorption hole and then passes through the liquid nitrogen desublimation frost-forming capillary form contact type dehumidification capillary net first, the liquid nitrogen desublimation frost-forming capillary form contact type dehumidifying capillary blade and the liquid nitrogen desublimation frost-forming capillary form contact type dehumidifying capillary perform desublimation frost-forming, and the dried air is discharged out of the main body through the rotational flow adsorption type multidimensional rotary type three-level connecting pipe.
Furthermore, the multi-ring gyroscope type magnetic force micro-positioning type fixing frame is externally connected with a power supply.
Further, a flow channel is arranged in the liquid nitrogen desublimation frost-forming capillary form contact type dehumidification capillary net, a flow channel is arranged in the liquid nitrogen desublimation frost-forming capillary form contact type dehumidification capillary blade, and a flow channel is arranged in the liquid nitrogen desublimation frost-forming capillary form contact type dehumidification capillary pipe.
The invention with the structure has the following beneficial effects: the invention provides a mounting device of a marine locator, which creatively applies the technical theory of a weight compensation principle (combining a certain object with another object capable of providing power to compensate the weight of the object and realizing the weight compensation through the interaction with the environment) to the technical field of mounting of the marine locator under the condition of no fixture fixation The transverse magnetic suspension gravity compensation type damping primary reinforcing plate is driven to move, the repulsion force between the damping type magnetic suspension gravity compensation type fixed secondary electromagnetic winding and the damping type magnetic suspension gravity compensation type fixed tertiary electromagnet is adjusted by electrifying the damping type magnetic suspension gravity compensation type fixed secondary electromagnetic winding, so that the transverse magnetic suspension gravity compensation type damping secondary reinforcing plate is driven to move, the positioning instrument is fixed and protected, and the technical problem that the positioning instrument is easy to damage if a ship body vibrates violently is solved; for the stability concept of the locator, the technical theory of dynamic characteristic principle (automatically adjusting the object to enable the object to have optimal performance in each action and stage or dividing the structure of the object into a plurality of components which can be changed and matched mutually or enabling the object which is not moved to be movable and self-adaptive) and nesting principle (embedding one object into a second object and then embedding the two objects into a third object) is innovatively applied to the technical field of the installation of the locator for the ship; the technical theory of physical or chemical parameter change principle (changing physical state of object, changing concentration or viscosity of object, changing flexibility of object, changing temperature or volume of object) and porous material principle (making object become porous material or adding porous object, if the object has porous structure, using porous structure to introduce useful substance or function) is creatively applied to the technical field of installation of marine locator The damp capillary tube is desublimated and frosted, and the dried air is discharged out of the main body through the cyclone adsorption type multidimensional rotary three-level connecting tube, so that the problem that the traditional fixing device cannot play a damp-proof role is solved.
Drawings
The accompanying drawings, which are included to provide a further understanding of the invention and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention and together with the description serve to explain the invention without limiting the invention.
FIG. 1 is a front view of a positioning device for a ship according to the present invention;
FIG. 2 is a front sectional view of a positioning device for a ship according to the present invention;
FIG. 3 is an enlarged view of a portion A of FIG. 2;
FIG. 4 is a schematic view of the low-temperature drying type air flow guiding type air suction device according to the present invention;
FIG. 5 is a schematic structural view of the low-temperature drying type air flow guide type air suction primary fixing box in FIG. 4;
FIG. 6 is a schematic structural view of the capillary-type contact dehumidification device in FIG. 4 for condensing and frosting liquid nitrogen;
fig. 7 is a schematic structural view of the multi-dimensional rotary type porous material cyclone adsorption apparatus shown in fig. 2.
Wherein, 1, a main body, 2, a multi-ring gyroscope type magnetic force micro-positioning type stabilizing device, 3, a magnetic suspension gravity compensation type damping zero-damage type fixing device, 4, a low-temperature drying type air flow guiding type air suction device, 5, a liquid nitrogen desublimation type capillary form contact type dehumidifying device, 6, a multi-dimensional rotary type porous material cyclone adsorption device, 7, a multi-ring gyroscope type magnetic force micro-positioning type primary stabilizing ring, 8, a multi-ring gyroscope type magnetic force micro-positioning type secondary stabilizing ring, 9, a multi-ring gyroscope type magnetic force micro-positioning type tertiary stabilizing ring, 10, a self-positioning type friction lossless type primary sliding groove, 11, a self-positioning type friction lossless type primary pulley, 12, a self-positioning type friction lossless type secondary pulley, 13, a friction lossless type magnetic force micro-positioning type primary bearing, 14, a friction lossless type magnetic force micro-positioning type secondary bearing, 15, A friction lossless magnetic force micro-positioning type tertiary bearing, 16, a friction lossless magnetic force micro-positioning type quaternary bearing, 17, a multi-ring gyroscope type magnetic force micro-positioning type fixing frame, 18, a magnetic force micro-positioning type multi-ring gyroscope type primary magnet, 19, a magnetic force micro-positioning type multi-ring gyroscope type secondary magnet, 20, a magnetic force micro-positioning type multi-ring gyroscope type tertiary magnet, 21, a magnetic force micro-positioning type multi-ring gyroscope type quaternary magnet, 22, a magnetic force micro-positioning type multi-ring gyroscope type five-stage magnet, 23, a magnetic force micro-positioning type multi-ring gyroscope type six-stage magnet, 24, a magnetic suspension gravity compensation type damping zero-damage type fixed primary slide groove, 25, a magnetic suspension gravity compensation type damping zero-damage type fixed secondary slide groove, 26, a transverse magnetic suspension gravity compensation type damping primary addition plate, 27, a transverse magnetic suspension gravity compensation type damping secondary addition plate, 28. a friction lossless type horizontal magnetic suspension gravity compensation type three-level pulley, 29, a friction lossless type horizontal magnetic suspension gravity compensation type four-level pulley, 30, a damping type magnetic suspension gravity compensation type fixed first-level electromagnet, 31, a damping type magnetic suspension gravity compensation type fixed second-level electromagnet, 32, a damping type magnetic suspension gravity compensation type fixed first-level electromagnetic winding, 33, a damping type magnetic suspension gravity compensation type fixed second-level electromagnetic winding, 34, a damping type magnetic suspension gravity compensation type fixed third-level electromagnet, 35, a damping type magnetic suspension gravity compensation type fixed third-level electromagnetic winding, 36, a magnetic suspension gravity compensation type damping zero damage type fixed first-level telescopic pipe, 37, a magnetic suspension gravity compensation type damping zero damage type fixed second-level telescopic pipe, 38, a magnetic suspension gravity compensation type damping zero damage type fixed third-level telescopic pipe, 39, a magnetic suspension gravity compensation type damping zero damage type fixed four-level telescopic pipe, 40. a low-temperature drying type air flow guiding type air suction primary motor, 41, a low-temperature drying type air flow guiding type air suction primary fan, 42, an air flow guiding type low-temperature drying type primary gear, 43, an air flow guiding type low-temperature drying type secondary gear, 44, an air flow guiding type low-temperature drying type primary driving rod, 45, an air flow guiding type low-temperature drying type primary driving rod, 46, a friction nondestructive type air flow guiding type five-stage bearing, 47, a low-temperature drying type air flow guiding type air suction primary fixing piece, 48, a low-temperature drying type air flow guiding type air suction primary fixing box, 49, a low-temperature drying type air flow guiding type air suction primary suction hole, 50, a liquid nitrogen desublimation type frost-forming capillary form contact type dehumidification capillary net, 51, a liquid nitrogen desublimation type frost-forming capillary form contact type dehumidification capillary blade, 52, and a liquid nitrogen desublimation type capillary form contact type dehumidification capillary, 53. capillary form contact type dehumidification liquid nitrogen desublimation frost-forming type liquid nitrogen tank, 54 capillary form contact type dehumidification liquid nitrogen desublimation frost-forming type circulating pump, 55 capillary form contact type dehumidification liquid nitrogen desublimation frost-forming type primary connecting pipe, 56 capillary form contact type dehumidification liquid nitrogen desublimation frost-forming type secondary connecting pipe, 57, multidimensional rotary type porous material cyclone adsorption primary bearing, 58, multidimensional rotary type porous material cyclone adsorption secondary bearing, 59, multidimensional rotary type porous material cyclone adsorption tertiary gear, 60, multidimensional rotary type porous material cyclone adsorption quaternary gear, 61, porous material cyclone adsorption type multidimensional rotary type primary adsorption pipe, 62, porous material cyclone adsorption type multidimensional rotary type primary adsorption hole, 63, porous material cyclone adsorption type multidimensional rotary type primary air pump, 64, cyclone adsorption type multidimensional rotary type tertiary connecting pipe, 65. A cyclone adsorption type multi-dimensional rotary secondary motor comprises a 66 multi-dimensional rotary porous material cyclone adsorption fixing part, a 67 magnetic suspension gravity compensation type damping zero-damage type fixing box and 68 liquid nitrogen desublimation frost-forming capillary contact type dehumidification adsorption holes.
Detailed Description
The technical solutions of the present invention will be further described in detail with reference to specific embodiments, and the technical features or connection relationships described in the present invention are not described in detail in the prior art. The present invention will be described in further detail with reference to the accompanying drawings.
In the description of the present invention, it is to be understood that the terms "upper", "lower", "front", "rear", "left", "right", "top", "bottom", "inner", "outer", and the like, indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, are merely for convenience in describing the present invention and simplifying the description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed in a particular orientation, and be operated, and thus, should not be construed as limiting the present invention.
As shown in fig. 1-4, the invention provides a mounting device of a marine locator, which comprises a main body 1, a multi-ring gyroscope type magnetic micro-positioning type stabilizing device 2, a magnetic suspension gravity compensation type damping zero-damage type fixing device 3, the device comprises a low-temperature drying type air flow guiding type air suction device 4, a liquid nitrogen desublimation frost-forming type capillary form contact type dehumidifying device 5 and a multidimensional type rotary porous material rotational flow adsorption device 6, wherein a multi-ring gyroscope type magnetic micro-positioning type stabilizing device 2 is arranged on a main body 1, a magnetic suspension gravity compensation type damping zero-damage type fixing device 3 is arranged in the multi-ring gyroscope type magnetic micro-positioning type stabilizing device 2, the low-temperature drying type air flow guiding type air suction device 4 is arranged on the main body 1, the liquid nitrogen desublimation frost-forming type capillary form contact type dehumidifying device 5 is arranged in the main body 1, and the multidimensional type rotary porous material rotational flow adsorption device 6 is arranged in the liquid nitrogen desublimation frost-forming type capillary form contact type dehumidifying device 5; the main body 1 comprises a magnetic suspension gravity compensation type damping zero damage type fixing box 67 and a liquid nitrogen desublimation frost-forming type capillary form contact type moisture removal adsorption hole 68, the magnetic suspension gravity compensation type damping zero damage type fixing box 67 is arranged on the main body 1, and the liquid nitrogen desublimation frost-forming type capillary form contact type moisture removal adsorption hole 68 is arranged on the magnetic suspension gravity compensation type damping zero damage type fixing box 67; the multi-ring gyroscope type magnetic force micro-positioning type stabilizing device 2 comprises a multi-ring gyroscope type magnetic force micro-positioning type primary stabilizing ring 7, a multi-ring gyroscope type magnetic force micro-positioning type secondary stabilizing ring 8, a multi-ring gyroscope type magnetic force micro-positioning type tertiary stabilizing ring 9, a self-positioning type friction lossless type primary sliding groove 10, a self-positioning type friction lossless type primary pulley 11, a self-positioning type friction lossless type secondary pulley 12, a friction lossless type magnetic force micro-positioning type primary bearing 13, a friction lossless type magnetic force micro-positioning type secondary bearing 14, a friction lossless type magnetic force micro-positioning type tertiary bearing 15, a friction lossless type magnetic force micro-positioning type quaternary bearing 16, a multi-ring gyroscope type magnetic force micro-positioning type fixing frame 17, a magnetic force micro-positioning type multi-ring gyroscope type primary magnet 18, a magnetic force micro-positioning type multi-ring gyroscope type secondary magnet 19, a micro-positioning type multi-ring gyroscope type tertiary magnet 20, a self-positioning type friction lossless type secondary bearing 11, a self-positioning type magnetic force micro-positioning type secondary bearing 13, a self-positioning type magnetic force micro-stage bearing 16, a self-positioning type magnetic force micro-stage bearing 17, a magnetic force micro-positioning type magnetic force micro-stage bearing 13, a magnetic force micro-positioning type magnetic force micro-stage bearing 12, a magnetic force micro-positioning type magnetic force micro-stage bearing 12, a magnetic force micro-positioning type magnetic force micro-stage bearing 13, a magnetic force positioning, A magnetic force micro-positioning type multi-ring gyroscope type four-stage magnet 21, a magnetic force micro-positioning type multi-ring gyroscope type five-stage magnet 22 and a magnetic force micro-positioning type multi-ring gyroscope type six-stage magnet 23, the multi-ring gyroscope type magnetic force micro-positioning type first-stage stabilizing ring 7 is arranged on the magnetic suspension gravity compensation zero-damage type fixing box 67, the self-positioning type friction lossless type first-stage sliding groove 10 is arranged in the multi-ring gyroscope type magnetic force micro-positioning type first-stage stabilizing ring 7, one end of the self-positioning type friction lossless type first-stage pulley 11 is slidingly arranged in the self-positioning type friction lossless type first-stage sliding groove 10, one end of the friction lossless type magnetic force micro-positioning type first-stage bearing 13 is arranged at the other end of the self-positioning type friction lossless type first-stage pulley 11, one end of the self-positioning type friction lossless type second-stage pulley 12 is slidingly arranged in the self-positioning type friction lossless type first-stage sliding groove 10, one end of the friction lossless type second-positioning type magnetic force micro-positioning type second-stage bearing 14 is arranged at the other end of the self-positioning type friction type second stage pulley 12 The side wall of the multi-ring gyroscope type magnetic force micro-positioning type secondary stabilizing ring 8 is arranged at the other end of the friction nondestructive type magnetic force micro-positioning type primary bearing 13, the other side wall of the multi-ring gyroscope type magnetic force micro-positioning type secondary stabilizing ring 8 is arranged at the other end of the friction nondestructive type magnetic force micro-positioning type secondary bearing 14, one end of the friction nondestructive type magnetic force micro-positioning type tertiary bearing 15 is arranged at the upper end of the inner wall of the multi-ring gyroscope type magnetic force micro-positioning type secondary stabilizing ring 8, the upper end of the outer side wall of the multi-ring gyroscope type magnetic force micro-positioning type tertiary stabilizing ring 9 is arranged at the other end of the friction nondestructive type magnetic force micro-positioning type tertiary bearing 15, one end of the friction nondestructive type magnetic force micro-positioning type quaternary bearing 16 is arranged at the lower end of the inner wall of the multi-ring gyroscope type magnetic force micro-positioning type secondary stabilizing ring 8, the other end of the friction nondestructive type magnetic force micro-positioning type quaternary bearing 16 is arranged at the lower end of the outer side wall of the multi-ring gyroscope type magnetic force micro-positioning type tertiary stabilizing ring 9, on the inner wall of the tertiary stabilizing ring 9 of the little location type of multi-ring gyroscope formula magnetic force is located to the little location type mount 17 of multi-ring gyroscope formula magnetic force, little location type multi-ring gyroscope formula secondary magnet 19 of magnetic force locates on the lateral wall of the little location type mount 17 of multi-ring gyroscope formula magnetic force, little location type multi-ring gyroscope formula primary magnet 18 of magnetic force locates on the magnetic levitation gravity compensation type shock attenuation zero damage type fixed box 67 inside wall, little location type multi-ring gyroscope formula fourth grade magnet 21 of magnetic force locates on another lateral wall of the little location type mount 17 of multi-ring gyroscope formula magnetic force, little location type multi-ring gyroscope formula tertiary magnet 20 of magnetic force locates on another inside wall of the magnetic levitation gravity compensation type shock attenuation zero damage type fixed box 67, little location type multi-ring gyroscope formula sixth grade magnet 23 of magnetic force locates the lower extreme of the little location type mount 17 of multi-ring gyroscope formula magnetic force, little location type five grade magnet 22 of magnetic force locates on the magnetic levitation gravity compensation type shock attenuation zero damage type fixed box 67 The lower end of the inner wall of the mold fixing box 67.
As shown in FIGS. 2-3, the magnetic suspension gravity compensation type damping zero damage type fixing device 3 includes a magnetic suspension gravity compensation type damping zero damage type fixed primary chute 24, a magnetic suspension gravity compensation type damping zero damage type fixed secondary chute 25, a transverse magnetic suspension gravity compensation type damping primary additional plate 26, a transverse magnetic suspension gravity compensation type damping secondary additional plate 27, a friction non-destructive type transverse magnetic suspension gravity compensation type tertiary pulley 28, a friction non-destructive type transverse magnetic suspension gravity compensation type quaternary pulley 29, a damping type magnetic suspension gravity compensation type fixed primary electromagnet 30, a damping type magnetic suspension gravity compensation type fixed secondary electromagnet 31, a damping type magnetic suspension gravity compensation type fixed primary electromagnetic winding 32, a damping type magnetic suspension gravity compensation type fixed secondary electromagnetic winding 33, a damping type magnetic suspension gravity compensation type fixed tertiary electromagnet 34, A damping type magnetic suspension gravity compensation type fixed three-level electromagnetic winding 35, a magnetic suspension gravity compensation type damping zero damage type fixed first-level extension pipe 36, a magnetic suspension gravity compensation type damping zero damage type fixed second-level extension pipe 37, a magnetic suspension gravity compensation type damping zero damage type fixed third-level extension pipe 38 and a magnetic suspension gravity compensation type damping zero damage type fixed fourth-level extension pipe 39, a magnetic suspension gravity compensation type damping zero damage type fixed first-level sliding chute 24 is arranged in the upper end wall of the multi-ring gyroscope type magnetic micro-positioning type fixed frame 17, a magnetic suspension gravity compensation type damping zero damage type fixed second-level sliding chute 25 is arranged in the lower end wall of the multi-ring gyroscope type magnetic micro-positioning type fixed frame 17, one end of a friction non-destructive type transverse magnetic suspension gravity compensation type three-level sliding pulley 28 is slidably arranged in the magnetic suspension gravity compensation type damping zero damage type fixed first-level sliding chute 24, one end of a transverse magnetic suspension gravity compensation type damping type primary additional plate 26 is arranged at the other end of a friction lossless type transverse magnetic suspension gravity compensation type tertiary pulley 28, one end of a friction lossless type transverse magnetic suspension gravity compensation type quaternary pulley 29 is arranged in a magnetic suspension gravity compensation zero damage type fixed secondary chute 25 in a sliding manner, the other end of the friction lossless type transverse magnetic suspension gravity compensation type quaternary pulley 29 is arranged at the other end of the transverse magnetic suspension gravity compensation type damping type primary additional plate 26, a damping type magnetic suspension gravity compensation type fixed primary electromagnetic winding 32 is arranged on the inner wall of a multi-ring gyroscope type magnetic force micro-positioning type fixing frame 17, a damping type magnetic suspension gravity compensation type fixed secondary electromagnetic winding 33 is arranged on the inner wall of the multi-ring gyroscope type magnetic force micro-positioning type fixing frame 17, a damping type magnetic suspension gravity compensation type fixed primary electromagnet 30 is arranged on the side wall of the transverse magnetic suspension gravity compensation type damping type primary additional plate 26, the damping type magnetic suspension gravity compensation type fixed secondary electromagnet 31 is arranged on the side wall of the transverse magnetic suspension gravity compensation type damping type primary additional plate 26, the magnetic suspension gravity compensation type damping zero damage type fixed secondary expansion pipe 37 is arranged on the upper end of the inner wall of the multi-ring gyroscope type magnetic force micro-positioning type fixing frame 17, one end of the magnetic suspension gravity compensation type damping zero damage type fixed primary expansion pipe 36 is arranged in the magnetic suspension gravity compensation type damping zero damage type fixed secondary expansion pipe 37 in a sliding manner, the transverse magnetic suspension gravity compensation type damping secondary additional plate 27 is arranged at the other end of the magnetic suspension gravity compensation type damping zero damage type fixed primary expansion pipe 36, one end of the magnetic suspension gravity compensation type damping zero damage type fixed four-stage expansion pipe 39 is arranged on the upper end of the inner wall of the gyroscope type magnetic force micro-positioning type fixing frame 17, one end of the magnetic suspension gravity compensation type damping zero damage type fixed three-stage expansion pipe 38 is arranged in a sliding manner In the flexible pipe 39 of fixed level four, the fixed tertiary flexible pipe 38 of horizontal magnetic levitation gravity compensation formula shock attenuation zero damage type is located to the other end of the fixed tertiary flexible pipe 38 of magnetic levitation gravity compensation formula on the board 27 is added to horizontal magnetic levitation gravity compensation formula shock attenuation type second grade, and the fixed tertiary electromagnetic winding 35 of shock attenuation type magnetic levitation gravity compensation formula is located the inner wall upper end of the little location type mount 17 of polycyclic gyroscope formula magnetic force, and the fixed tertiary electro-magnet 34 of shock attenuation type magnetic levitation gravity compensation formula is located on the board 27 is added to horizontal magnetic levitation gravity compensation formula shock attenuation type second grade.
As shown in fig. 4-5, the low-temperature drying type air flow guiding type air suction device 4 includes a low-temperature drying type air flow guiding type air suction primary motor 40, a low-temperature drying type air flow guiding type air suction primary fan 41, an air flow guiding type low-temperature drying type primary gear 42, an air flow guiding type low-temperature drying type secondary gear 43, an air flow guiding type low-temperature drying type primary driving rod 44, an air flow guiding type low-temperature drying type primary driving rod 45, a friction lossless type air flow guiding type five-stage bearing 46, a low-temperature drying type air flow guiding type air suction primary fixing piece 47, a low-temperature drying type air flow guiding type air suction primary fixing box 48 and a low-temperature drying type air flow guiding type air suction primary air suction hole 49, the low-temperature drying type air flow guiding type air suction primary fixing box 48 is arranged in a magnetic suspension gravity compensation type zero damage damping type fixing box 67, the low-temperature drying type air flow guiding type air suction primary air suction hole 49 is arranged on the low-temperature drying type air flow guiding type air suction primary fixing box 48, the low-temperature drying type air flow guiding type air suction first-stage fixing piece 47 is arranged in a low-temperature drying type air flow guiding type air suction first-stage fixing box 48, a friction lossless type air flow guiding type five-stage bearing 46 is arranged on the inner wall of the low-temperature drying type air flow guiding type air suction first-stage fixing box 48, a low-temperature drying type air flow guiding type air suction first-stage motor 40 is arranged on the outer side wall of the low-temperature drying type air flow guiding type air suction first-stage fixing box 48, one end of an air flow guiding type low-temperature drying type first-stage driving rod 44 is arranged at the output end of the low-temperature drying type air flow guiding type air suction first-stage motor 40, the other end of the air flow guiding type low-temperature drying type first-stage driving rod 44 is arranged on the friction lossless type air flow guiding type five-stage bearing 46, the air flow guiding type low-temperature drying type first-stage driving rod 44 is rotatably arranged on the low-temperature drying type air flow guiding type air suction first-stage fixing piece 47, and the air flow guiding type low-temperature drying type first-stage driving rod 45 is rotatably arranged on the low-temperature drying type air flow guiding type air suction first-stage fixing piece 48 At 47, the airflow guiding type low temperature drying type secondary gear 43 is sleeved on the airflow guiding type low temperature drying type primary driving rod 44, the airflow guiding type low temperature drying type primary gear 42 is sleeved on one end of the airflow guiding type low temperature drying type primary driving rod 45, the low temperature drying type airflow guiding type suction primary fan 41 is arranged at the other end of the airflow guiding type low temperature drying type primary driving rod 45, and the airflow guiding type low temperature drying type primary gear 42 and the airflow guiding type low temperature drying type secondary gear 43 are connected in a meshing rotation manner.
As shown in FIGS. 4 and 6, the liquid nitrogen-desublimation-frost-forming capillary form contact type dehumidification device 5 includes a liquid nitrogen-desublimation-frost-forming capillary form contact type dehumidification capillary net 50, a liquid nitrogen-desublimation-frost-forming capillary form contact type dehumidification capillary blade 51, a liquid nitrogen-desublimation-frost-forming capillary form contact type dehumidification capillary 52, a capillary form contact type dehumidification liquid nitrogen-desublimation-frost-forming liquid nitrogen tank 53, a capillary form contact type dehumidification liquid nitrogen-desublimation-frost-forming circulation pump 54, a capillary form contact type dehumidification liquid nitrogen-desublimation-frost-forming primary connection pipe 55, and a capillary form contact type dehumidification liquid nitrogen-desublimation-frost-forming secondary connection pipe 56, the liquid nitrogen-desublimation-frost-forming capillary form contact type dehumidification capillary net 50 is disposed in the low-temperature drying type air flow-guiding primary air-suction fixing box 48, the liquid nitrogen-desublimation-frost-forming capillary form contact type dehumidification capillary blade 51 is penetratively disposed on the liquid nitrogen-desublimation-frost-formation type capillary form contact type dehumidification capillary net 50, a liquid nitrogen-desublimating-type capillary form contact-type dehumidifying capillary 52 is arranged on a liquid nitrogen-desublimating-type capillary form contact-type dehumidifying capillary blade 51 in a penetrating manner, a capillary form contact-type dehumidifying liquid nitrogen-desublimating-type liquid nitrogen tank 53 is arranged on one side of the low-temperature drying type air-draft primary fixing box 48, one end of a capillary form contact-type dehumidifying liquid nitrogen-desublimating-type primary connecting pipe 55 is arranged at the input end of the liquid nitrogen-desublimating-type capillary form contact-type dehumidifying capillary net 50 in a penetrating manner, the other end of the capillary form contact-type dehumidifying liquid nitrogen-desublimating-type primary connecting pipe 55 is arranged at the output end of the capillary form contact-type dehumidifying liquid nitrogen-desublimating-type liquid nitrogen tank 53 in a penetrating manner, a capillary form contact-type dehumidifying liquid nitrogen-desublimating-frosting-type circulating pump 54 is arranged on the capillary form contact-type dehumidifying liquid nitrogen-desublimating-frosting-type primary connecting pipe 55, and one end of the capillary form contact-type dehumidifying liquid nitrogen-desublimating-type secondary connecting pipe 56 is arranged at the output end of the liquid nitrogen-desublimating-type defrosting-type The other end of the capillary form contact type dehumidification liquid nitrogen desublimation frost-forming type secondary connecting pipe 56 is communicated with the input end of the capillary form contact type dehumidification liquid nitrogen desublimation frost-forming type liquid nitrogen tank 53.
As shown in fig. 2, 4 and 7, the multi-dimensional rotary porous material cyclone adsorption device 6 comprises a multi-dimensional rotary porous material cyclone adsorption first-stage bearing 57, a multi-dimensional rotary porous material cyclone adsorption second-stage bearing 58, a multi-dimensional rotary porous material cyclone adsorption third-stage gear 59, a multi-dimensional rotary porous material cyclone adsorption fourth-stage gear 60, a porous material cyclone adsorption multi-dimensional rotary first-stage adsorption tube 61, a porous material cyclone adsorption multi-dimensional rotary first-stage adsorption hole 62, a porous material cyclone adsorption multi-dimensional rotary first-stage air pump 63, a cyclone adsorption multi-dimensional rotary third-stage connecting tube 64, a cyclone adsorption multi-dimensional rotary second-stage motor 65 and a multi-dimensional rotary porous material cyclone adsorption fixing member 66, wherein the multi-dimensional rotary porous material cyclone adsorption fixing member 66 is arranged in a low-temperature drying type air flow guiding first-stage air suction fixing box 48, a multidimensional rotary porous material cyclone adsorption primary bearing 57 is arranged on a multidimensional rotary porous material cyclone adsorption fixing part 66, one end of a porous material cyclone adsorption multidimensional rotary porous material cyclone adsorption primary adsorption tube 61 is arranged on the multidimensional rotary porous material cyclone adsorption primary bearing 57, a porous material cyclone adsorption multidimensional rotary primary adsorption hole 62 is arranged on the porous material cyclone adsorption multidimensional rotary primary adsorption tube 61, a multidimensional rotary porous material cyclone adsorption four-stage gear 60 is sleeved on the shaft of the porous material cyclone adsorption multidimensional rotary primary adsorption tube 61, a multidimensional rotary porous material cyclone adsorption secondary bearing 58 is arranged at the lower end of the porous material cyclone adsorption multidimensional rotary porous material cyclone adsorption type rotary primary adsorption tube 61, one end of a cyclone adsorption multidimensional rotary three-stage connecting tube 64 is arranged on the multidimensional rotary porous material cyclone adsorption secondary bearing 58, the rotational flow adsorption type multi-dimensional rotary three-stage connecting pipe 64 is arranged on the inner side wall of the magnetic suspension gravity compensation type damping zero-damage type fixed box 67, the porous material rotational flow adsorption type multi-dimensional rotary one-stage air pump 63 is arranged on the rotational flow adsorption type multi-dimensional rotary three-stage connecting pipe 64, the other end of the rotational flow adsorption type multi-dimensional rotary three-stage connecting pipe 64 is arranged on the outer side of the magnetic suspension gravity compensation type damping zero-damage type fixed box 67, the rotational flow adsorption type multi-dimensional rotary two-stage motor 65 is arranged on the inner side of the magnetic suspension gravity compensation type damping zero-damage type fixed box 67, the multi-dimensional rotary porous material rotational flow adsorption three-stage gear 59 is arranged at the output end of the rotational flow adsorption type multi-dimensional rotary two-stage motor 65, and the multi-dimensional rotary porous material rotational flow adsorption three-stage gear 59 and the multi-dimensional rotary porous material rotational flow adsorption four-stage gear 60 are connected in a meshing rotation mode.
As shown in fig. 3, 4 and 6, the multi-ring gyroscope type magnetic micro-positioning fixing frame 17 is externally connected with a power supply.
The liquid nitrogen desublimation frost-forming capillary form contact type dehumidification capillary net 50 is internally provided with a flow passage, the liquid nitrogen desublimation frost-forming capillary form contact type dehumidification capillary blade 51 is internally provided with a flow passage, and the liquid nitrogen desublimation frost-forming capillary form contact type dehumidification capillary 52 is internally provided with a flow passage.
When the device is used, firstly, the locator is placed on the magnetic suspension gravity compensation type damping zero-damage fixing device 3, as an improvement, in view of the fact that the ship sailing speed is slower than that of an automobile, the reporting frequency of the locator is adjusted to be 1 time every 15 minutes, the reporting frequency of position data is reasonably controlled to greatly relieve the storage pressure of a server, meanwhile, the ships sailing in inland rivers and Yangtze rivers have the situations of bridge-crossing gate-crossing queuing, goods loading and unloading queuing waiting and the like, so that the movement sensing sensitivity of the locator is reduced to 5 kilometers per hour, the device is prevented from being incapable of sensing and automatically sleeping under the condition of low-speed movement, the actual situation of a ship transportation scene is adapted, a 24V voltage interface for power connection of the locator is connected with a positive electrode and a negative electrode, and a customized 24V-to-12V voltage reducer are connected, and then the locator is connected to a 12V locator power supply interface for power supply, starting the magnetic suspension gravity compensation type damping zero damage type fixing device 3, adjusting the repulsion force of the damping type magnetic suspension gravity compensation type fixed primary electromagnet 30 by electrifying the damping type magnetic suspension gravity compensation type fixed primary electromagnetic winding 32, adjusting the repulsion force of the damping type magnetic suspension gravity compensation type fixed secondary electromagnet 31 by electrifying the damping type magnetic suspension gravity compensation type fixed secondary electromagnetic winding 33, thereby driving the transverse magnetic suspension gravity compensation type damping primary additional plate 26 to move, adjusting the repulsion force of the damping type magnetic suspension gravity compensation type fixed secondary electromagnetic winding 33 and the damping type magnetic suspension gravity compensation type fixed tertiary electromagnet 34 by electrifying the damping type magnetic suspension gravity compensation type fixed secondary electromagnetic winding 33, thereby driving the transverse magnetic suspension gravity compensation type damping secondary additional plate 27 to move, thereby fixing the positioning instrument, fixing the magnetic suspension gravity compensation type damping zero damage type fixed primary telescopic pipe 36 and the magnetic suspension gravity compensation type damping zero damage type fixed secondary telescopic pipe 37 in phase The mutually matched magnetic suspension gravity compensation type damping zero damage type fixed three-level extension pipe 38 and the magnetic suspension gravity compensation type damping zero damage type fixed four-level extension pipe 39 are mutually matched to have a limiting effect on the transverse magnetic suspension gravity compensation type damping two-level additional plate 27, when a ship body is impacted to generate severe vibration, the positioner can perform damping and buffering by virtue of repulsive force of magnetic suspension so as to protect the positioner, when the motion amplitude of the ship body is tiny, the magnetic micro-positioning type multi-ring gyroscope type six-level magnet 23 and the magnetic micro-positioning type multi-ring gyroscope type five-level magnet 22 are mutually attracted to ensure that the positioner vertically faces downwards, the magnetic micro-positioning type multi-ring gyroscope type first-level magnet 18 and the magnetic micro-positioning type multi-ring gyroscope type two-level magnet 19 are mutually attracted, the magnetic micro-positioning type multi-ring gyroscope type three-level magnet 20 and the magnetic micro-positioning type multi-ring gyroscope type four-level magnet 21 are mutually attracted, the positioning instrument is in a horizontal position, when the left-right shaking amplitude of the ship body is overlarge, the magnetic suspension gravity compensation type damping zero damage type fixing box 67 drives the multi-ring gyroscope type magnetic force micro-positioning type primary stabilizing ring 7 to shake left and right, the self-positioning type friction damage-free type primary chute 10 shakes left and right, the self-positioning type friction damage-free type primary pulley 11 and the self-positioning type friction damage-free type secondary pulley 12 rotate but the positions are unchanged, when the ship body shakes forwards and backwards, the magnetic suspension gravity compensation type damping zero damage type fixing box 67 drives the multi-ring gyroscope type magnetic force micro-positioning type primary stabilizing ring 7 to shake forwards and backwards, the multi-ring gyroscope type magnetic force micro-positioning type primary stabilizing ring 7 shakes forwards and backwards to drive the self-positioning type friction damage-free type primary pulley 11 and the self-positioning type friction damage-free type secondary pulley 12 to shake forwards and backwards, the self-positioning type friction damage-free type primary pulley 11 shakes forwards and backwards to drive the friction damage-free type magnetic force micro-positioning type primary bearing 13 to rotate, self-positioning type friction lossless type secondary pulley 12 shakes back and forth to drive friction lossless type magnetic force micro-positioning type secondary bearing 14 to rotate, the positions of friction lossless type magnetic force micro-positioning type primary bearing 13 and friction lossless type magnetic force micro-positioning type secondary bearing 14 are not changed, when the ship body shakes in a reciprocating and self-transmission manner, magnetic suspension gravity compensation type damping zero-damage type fixing box 67 shakes to drive multi-ring gyroscope type magnetic force micro-positioning type primary stabilizing ring 7 to shake, multi-ring gyroscope type magnetic force micro-positioning type primary stabilizing ring 7 shakes to drive friction lossless type magnetic force micro-positioning type primary bearing 13 to shake, friction lossless type magnetic force micro-positioning type primary bearing 13 shakes to drive multi-ring gyroscope type magnetic force micro-positioning type secondary stabilizing ring 8 to shake, friction lossless type magnetic force micro-positioning type tertiary bearing 15 and friction lossless type magnetic force micro-positioning type four-stage bearing 16 rotate When the position is unchanged, when the sea humidity is too high, the low-temperature drying type air flow guiding type air suction device 4 is started, the output end of the low-temperature drying type air flow guiding type air suction primary motor 40 rotates to drive the air flow guiding type low-temperature drying type primary driving rod 44 to rotate, the air flow guiding type low-temperature drying type primary driving rod 44 rotates to drive the air flow guiding type low-temperature drying type secondary gear 43 to rotate, the air flow guiding type low-temperature drying type secondary gear 43 rotates to drive the air flow guiding type low-temperature drying type primary gear 42 to rotate, the air flow guiding type low-temperature drying type primary gear 42 rotates to drive the air flow guiding type low-temperature drying type primary driving rod 45 to rotate, the air flow guiding type low-temperature drying type primary driving rod 45 rotates to drive the low-temperature drying type air flow guiding type air suction primary fan 41 to rotate, and air is sucked into the liquid nitrogen and condensed into the frost type capillary form contact type moisture removal device 5, the liquid nitrogen desublimation frost-forming capillary form contact type dehumidification capillary net 50, the liquid nitrogen desublimation frost-forming capillary form contact type dehumidification capillary blade 51 and the liquid nitrogen desublimation frost-forming capillary form contact type dehumidification capillary tube 52 are filled with flowing liquid nitrogen, the multidimensional rotary type porous material cyclone adsorption device 6 is started, the output end of the cyclone adsorption type multidimensional rotary type two-stage motor 65 rotates to drive the multidimensional rotary type porous material cyclone adsorption three-stage gear 59 to rotate, the multidimensional rotary type porous material cyclone adsorption three-stage gear 59 rotates to drive the multidimensional rotary type porous material cyclone adsorption four-stage gear 60 to rotate, the multidimensional rotary type porous material cyclone adsorption four-stage gear 60 rotates to drive the porous material cyclone adsorption type multidimensional rotary type one-stage adsorption tube 61 to rotate, the porous material cyclone adsorption type multidimensional rotary type one-stage air pump 63 starts to adsorb moist air through the porous material cyclone adsorption type multidimensional rotary type one-stage adsorption hole 62 first and then through the porous material cyclone adsorption type one-stage adsorption hole 62 The liquid nitrogen desublimation and frost formation type capillary form contact type moisture removal capillary net 50, the liquid nitrogen desublimation and frost formation type capillary form contact type moisture removal capillary blade 51 and the liquid nitrogen desublimation and frost formation type capillary form contact type moisture removal capillary 52 are desublimed and frosted, the dried air is discharged out of the main body 1 through the rotational flow adsorption type multidimensional rotary three-level connecting pipe 64, the collected dust is mixed in the water for centralized treatment, the whole working process is completed, and the steps are repeated when the air is used next time.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
The present invention and its embodiments have been described above, and the description is not intended to be limiting, and the drawings are only one embodiment of the present invention, and the actual structure is not limited thereto. In summary, those skilled in the art should appreciate that they can readily use the disclosed conception and specific embodiments as a basis for designing or modifying other structures for carrying out the same purposes of the present invention without departing from the spirit and scope of the invention as defined by the appended claims.

Claims (7)

1. The utility model provides a marine locater installation device which characterized in that: the device comprises a main body, a multi-ring gyroscope type magnetic force micro-positioning type stabilizing device, a magnetic suspension gravity compensation type damping zero-damage type fixing device, a low-temperature drying type air draft device, a liquid nitrogen desublimation frost-forming type capillary form contact type dehumidifying device and a multi-dimensional rotary type porous material rotational flow adsorption device, wherein the multi-ring gyroscope type magnetic force micro-positioning type stabilizing device is arranged on the main body; the main body comprises a magnetic suspension gravity compensation type damping zero damage type fixed box and a liquid nitrogen desublimation frost-forming type capillary form contact type dehumidification adsorption hole, the magnetic suspension gravity compensation type damping zero damage type fixed box is arranged on the main body, and the liquid nitrogen desublimation frost-forming type capillary form contact type dehumidification adsorption hole is arranged on the magnetic suspension gravity compensation type damping zero damage type fixed box; the multi-ring gyroscope type magnetic force micro-positioning type stabilizing device comprises a multi-ring gyroscope type magnetic force micro-positioning type primary stabilizing ring, a multi-ring gyroscope type magnetic force micro-positioning type secondary stabilizing ring, a multi-ring gyroscope type magnetic force micro-positioning type tertiary stabilizing ring, a self-positioning type friction lossless primary sliding groove, a self-positioning type friction lossless primary pulley, a self-positioning type friction lossless secondary pulley, a friction lossless type magnetic force micro-positioning type primary bearing, a friction lossless type magnetic force micro-positioning type secondary bearing, a friction lossless type magnetic force micro-positioning type tertiary bearing, a friction lossless type magnetic force micro-positioning type quaternary bearing, a multi-ring gyroscope type magnetic force micro-positioning type fixing frame, a magnetic force micro-positioning type multi-ring gyroscope type primary magnet, a magnetic force micro-positioning type multi-ring gyroscope type secondary magnet, a magnetic force micro-positioning type multi-ring gyroscope type tertiary magnet, a magnetic force micro-positioning type multi-ring gyroscope type quaternary magnet, a magnetic force micro-positioning type fixing frame, a magnetic force micro-ring gyroscope type magnetic force micro-positioning type primary magnet, a magnetic force micro-ring gyroscope type magnetic force micro-positioning type magnetic bearing, a magnetic force micro-positioning type magnetic force micro-ring-positioning type magnetic force micro-ring, Magnetic force micro-positioning type multi-ring gyroscope type five-level magnet and magnetic force micro-positioning type multi-ring gyroscope type six-level magnet, wherein the multi-ring gyroscope type magnetic force micro-positioning type one-level stable ring is arranged on a magnetic suspension gravity compensation type damping zero damage type fixed box, the self-positioning type friction lossless type one-level chute is arranged in the multi-ring gyroscope type magnetic force micro-positioning type one-level stable ring, one end of the self-positioning type friction lossless type one-level pulley is arranged in the self-positioning type friction lossless type one-level chute in a sliding manner, one end of the friction lossless type magnetic force micro-positioning type one-level bearing is arranged at the other end of the self-positioning type friction lossless type one-level pulley, one end of the self-positioning type friction lossless type two-level pulley is arranged in the self-positioning type friction lossless type one-level chute in a sliding manner, one end of the friction lossless type magnetic force micro-positioning type two-level bearing is arranged at the other end of the self-positioning type friction lossless type two-level pulley, the other end of the lossless magnetic force micro-positioning type first-level bearing of friction is arranged on the side wall of the multi-ring gyroscope type magnetic force micro-positioning type second-level stabilizing ring, the other end of the lossless magnetic force micro-positioning type second-level bearing of friction is arranged on the other side wall of the multi-ring gyroscope type magnetic force micro-positioning type second-level stabilizing ring, one end of the lossless magnetic force micro-positioning type third-level bearing of friction is arranged on the upper end of the inner wall of the multi-ring gyroscope type magnetic force micro-positioning type second-level stabilizing ring, the upper end of the outer side wall of the lossless magnetic force micro-positioning type third-level stabilizing ring is arranged on the other end of the lossless magnetic force micro-positioning type third-level bearing of friction, one end of the lossless magnetic force micro-positioning type fourth-level bearing of friction is arranged on the lower end of the inner wall of the multi-ring gyroscope type magnetic force micro-positioning type second-level stabilizing ring, and the other end of the lossless magnetic force micro-positioning type fourth-level bearing of friction is arranged on the outer side wall of the multi-level gyro type magnetic force micro-level stabilizing ring, on the inner wall of the tertiary stabilizing ring of multi-ring gyroscope type magnetic force micro-positioning type was located to multi-ring gyroscope type magnetic force micro-positioning type mount, magnetic force micro-positioning type multi-ring gyroscope type secondary magnet was located on the lateral wall of multi-ring gyroscope type magnetic force micro-positioning type mount, magnetic force micro-positioning type multi-ring gyroscope type primary magnet was located on the magnetic suspension gravity compensation type zero damage type fixed box inside wall, magnetic force micro-positioning type multi-ring gyroscope type four-level magnet was located on another lateral wall of multi-ring gyroscope type magnetic force micro-positioning type mount, magnetic force micro-positioning type multi-ring gyroscope type tertiary magnet was located on another inside wall of magnetic suspension gravity compensation type zero damage type fixed box, magnetic force micro-positioning type multi-ring gyroscope type six-level magnet was located the lower extreme of multi-ring gyroscope type magnetic force micro-positioning type mount, magnetic force micro-positioning type multi-ring gyroscope type five-level magnet was located the magnetic suspension gravity compensation type zero damage type fixed box inside wall The lower end of the wall.
2. The apparatus according to claim 1, wherein: the magnetic suspension gravity compensation type damping zero damage type fixing device comprises a magnetic suspension gravity compensation type damping zero damage type fixed first-level sliding chute, a magnetic suspension gravity compensation type damping zero damage type fixed second-level sliding chute, a transverse magnetic suspension gravity compensation type damping first-level additional plate, a transverse magnetic suspension gravity compensation type damping second-level additional plate, a friction-lossless type transverse magnetic suspension gravity compensation type third-level pulley, a friction-lossless type transverse magnetic suspension gravity compensation type fourth-level pulley, a damping type magnetic suspension gravity compensation type fixed first-level electromagnet, a damping type magnetic suspension gravity compensation type fixed second-level electromagnet, a damping type magnetic suspension gravity compensation type fixed first-level electromagnetic winding, a damping type magnetic suspension gravity compensation type fixed second-level electromagnetic winding, a damping type magnetic suspension gravity compensation type fixed third-level electromagnet, a damping type magnetic suspension gravity compensation type fixed third-level electromagnetic winding, The magnetic suspension gravity compensation type damping zero damage fixed primary telescopic pipe, the magnetic suspension gravity compensation type damping zero damage fixed secondary telescopic pipe, the magnetic suspension gravity compensation type damping zero damage fixed tertiary telescopic pipe and the magnetic suspension gravity compensation type damping zero damage fixed quaternary telescopic pipe, the magnetic suspension gravity compensation type damping zero damage fixed primary chute is arranged in the upper end wall of the multi-ring gyroscope type magnetic force micro-positioning type fixing frame, the magnetic suspension gravity compensation type damping zero damage fixed secondary chute is arranged in the lower end wall of the multi-ring gyroscope type magnetic force micro-positioning type fixing frame, one end of the non-destructive friction type transverse magnetic suspension gravity compensation type tertiary pulley is slidably arranged in the magnetic suspension gravity compensation type damping zero damage fixed primary chute, one end of the transverse magnetic suspension gravity compensation type damping primary reinforcing plate is arranged at the other end of the frictional non-destructive type transverse magnetic suspension gravity compensation type tertiary pulley, one end of the friction lossless type transverse magnetic suspension gravity compensation type four-stage pulley is slidably arranged in a magnetic suspension gravity compensation type zero-damage fixed second-stage sliding chute, the other end of the friction lossless type transverse magnetic suspension gravity compensation type four-stage pulley is arranged at the other end of a transverse magnetic suspension gravity compensation type damping type first-stage additional plate, the damping type magnetic suspension gravity compensation type fixed first-stage electromagnetic winding is arranged on the inner wall of the multi-ring gyroscope type magnetic force micro-positioning type fixing frame, the damping type magnetic suspension gravity compensation type fixed second-stage electromagnetic winding is arranged on the inner wall of the multi-ring gyroscope type magnetic force micro-positioning type fixing frame, the damping type magnetic suspension gravity compensation type fixed first-stage electromagnet is arranged on the side wall of the transverse magnetic suspension gravity compensation type damping type first-stage additional plate, the damping type magnetic suspension gravity compensation type fixed second-stage electromagnet is arranged on the side wall of the transverse magnetic suspension gravity compensation type damping type first-stage additional plate, the inner wall upper end of the fixed two-stage telescopic pipe of the magnetic suspension gravity compensation type damping zero damage type is arranged on the multi-ring gyroscope type magnetic force micro-positioning type fixing frame, one end of the fixed one-stage telescopic pipe of the magnetic suspension gravity compensation type damping zero damage type is slidably arranged in the fixed two-stage telescopic pipe of the magnetic suspension gravity compensation type damping zero damage type, one end of the fixed four-stage telescopic pipe of the magnetic suspension gravity compensation type damping zero damage type is transversely provided with the magnetic suspension gravity compensation type damping two-stage additional plate and is arranged at the other end of the fixed one-stage telescopic pipe of the magnetic suspension gravity compensation type damping zero damage type, one end of the fixed four-stage telescopic pipe of the magnetic suspension gravity compensation type damping zero damage type is slidably arranged in the fixed four-stage telescopic pipe of the magnetic suspension gravity compensation type damping zero damage type, the other end of the fixed three-stage telescopic pipe of the magnetic suspension gravity compensation type damping zero damage type is arranged at the upper end of the transverse magnetic suspension gravity compensation type damping gravity micro-positioning type fixing frame On the type second grade adds the board, the fixed tertiary electromagnetic winding of shock-proof type magnetic suspension gravity compensation formula is located the inner wall upper end of many ring gyroscope formula magnetic force micro-positioning type mount, the fixed tertiary electro-magnet of shock-proof type magnetic suspension gravity compensation formula is located on horizontal magnetic suspension gravity compensation formula shock-proof type second grade adds the board.
3. The apparatus according to claim 2, wherein: the low-temperature drying type air flow guiding type air suction device comprises a low-temperature drying type air flow guiding type air suction primary motor, a low-temperature drying type air flow guiding type air suction primary fan, an air flow guiding type low-temperature drying type primary gear, an air flow guiding type low-temperature drying type secondary gear, an air flow guiding type low-temperature drying type primary driving rod, a friction nondestructive type air flow guiding type five-stage bearing, a low-temperature drying type air flow guiding type air suction primary fixing box and a low-temperature drying type air flow guiding type air suction primary air suction hole, wherein the low-temperature drying type air flow guiding type air suction primary fixing box is arranged in the magnetic suspension weight compensation type damping zero damage type fixing box, and the low-temperature drying type air flow guiding type air suction primary air suction hole is arranged on the low-temperature drying type air flow guiding type air suction primary fixing box, the low-temperature drying type air flow guiding type air suction first-level fixing piece is arranged in the low-temperature drying type air flow guiding type air suction first-level fixing box, the friction lossless type air flow guiding type five-level bearing is arranged on the inner wall of the low-temperature drying type air flow guiding type air suction first-level fixing box, the low-temperature drying type air flow guiding type air suction first-level motor is arranged on the outer side wall of the low-temperature drying type air flow guiding type air suction first-level fixing box, one end of an air flow guiding type low-temperature drying type first-level driving rod is arranged at the output end of the low-temperature drying type air flow guiding type air suction first-level motor, the other end of the air flow guiding type low-temperature drying type first-level driving rod is arranged on the friction lossless type air flow guiding type five-level bearing, the air flow guiding type low-temperature drying type first-level driving rod is rotatably arranged on the low-temperature drying type air flow guiding type air suction first-level fixing piece, and the air flow guiding type low-temperature drying type low-level driving rod is rotatably arranged on the low-temperature drying type air suction first-level fixing piece, the air flow guiding type low-temperature drying type secondary gear is sleeved on the air flow guiding type low-temperature drying type primary driving rod, the air flow guiding type low-temperature drying type primary gear is sleeved on one end of the air flow guiding type low-temperature drying type primary driving rod, the low-temperature drying type air suction primary fan is arranged at the other end of the air flow guiding type low-temperature drying type primary driving rod, and the air flow guiding type low-temperature drying type secondary gears of the air flow guiding type low-temperature drying type primary gears are connected in a meshing rotation mode.
4. A positioning instrument mounting arrangement for a ship according to claim 3, wherein: the liquid nitrogen desublimation frost-forming type capillary form contact type dehumidification device comprises a liquid nitrogen desublimation frost-forming type capillary form contact type dehumidification capillary net, a liquid nitrogen desublimation frost-forming type capillary form contact type dehumidification capillary blade, a liquid nitrogen desublimation frost-forming type capillary form contact type dehumidification capillary tube, a capillary form contact type dehumidification liquid nitrogen desublimation frost-forming type liquid nitrogen tank, a capillary form contact type dehumidification liquid nitrogen desublimation frost-forming type circulating pump, a capillary form contact type dehumidification liquid nitrogen desublimation frost-forming type primary connecting pipe and a capillary form contact type dehumidification frost-forming type secondary connecting pipe, wherein the liquid nitrogen desublimation frost-forming type capillary form contact type dehumidification capillary net is arranged in a low-temperature drying type air flow guiding type primary air suction fixing box, the liquid nitrogen desublimation frost-forming type capillary form contact type dehumidification capillary blade is communicated with the liquid nitrogen desublimation frost-forming type capillary form contact type dehumidification capillary net, and the liquid nitrogen desublimation capillary form contact type dehumidification capillary pipe is communicated with the frost-forming type capillary form capillary net On the capillary leaf of thin form contact type dehumidification, capillary form contact type dehumidification liquid nitrogen desublimation frost-forming formula liquid nitrogen jar locates one side of low temperature drying formula air current guide type induced draft primary fixing case, the one end of capillary form contact type dehumidification liquid nitrogen desublimation frost-forming formula primary connecting pipe link up and locate liquid nitrogen desublimation frost-forming formula capillary form contact type dehumidification capillary net input, the other end of capillary form contact type dehumidification liquid nitrogen desublimation frost-forming formula primary connecting pipe link up and locate the output of capillary form contact type dehumidification liquid nitrogen desublimation frost-forming formula liquid nitrogen jar, capillary form contact type dehumidification liquid nitrogen desublimation frost-forming formula circulating pump locates on capillary form contact type dehumidification liquid nitrogen desublimation frost-forming formula primary connecting pipe, one end of capillary form contact type dehumidification liquid nitrogen desublimation frost-forming formula secondary connecting pipe link up and locates the output of liquid nitrogen desublimation frost-forming formula capillary form contact type dehumidification net, the other end of the capillary form contact type dehumidification liquid nitrogen desublimation frost-forming type secondary connecting pipe is communicated with the input end of the capillary form contact type dehumidification liquid nitrogen desublimation frost-forming type liquid nitrogen tank.
5. The apparatus according to claim 4, wherein: the multi-dimensional rotary type porous material cyclone adsorption device comprises a multi-dimensional rotary type porous material cyclone adsorption first-stage bearing, a multi-dimensional rotary type porous material cyclone adsorption second-stage bearing, a multi-dimensional rotary type porous material cyclone adsorption third-stage gear, a multi-dimensional rotary type porous material cyclone adsorption fourth-stage gear, a porous material cyclone adsorption multi-dimensional rotary type first-stage adsorption pipe, a porous material cyclone adsorption multi-dimensional rotary type first-stage adsorption hole, a porous material cyclone adsorption multi-dimensional rotary type first-stage air pump, a cyclone adsorption multi-dimensional rotary type third-stage connecting pipe, a cyclone adsorption multi-dimensional rotary type second-stage motor and a multi-dimensional rotary type porous material cyclone adsorption fixing piece, wherein the multi-dimensional rotary type porous material cyclone adsorption fixing piece is arranged in a low-temperature drying type air flow guiding type air suction first-stage fixing box, the multi-dimensional rotary type porous material cyclone adsorption first-stage bearing is arranged on the multi-dimensional rotary type porous material cyclone adsorption fixing piece, one end of the porous material rotational flow adsorption type multidimensional rotary primary adsorption pipe is arranged on a multidimensional rotary porous material rotational flow adsorption primary bearing, the porous material rotational flow adsorption type multidimensional rotary primary adsorption hole is arranged on the porous material rotational flow adsorption type multidimensional rotary primary adsorption pipe, the multidimensional rotary porous material rotational flow adsorption four-stage gear is sleeved on the shaft of the porous material rotational flow adsorption type multidimensional rotary primary adsorption pipe, the multidimensional rotary porous material rotational flow adsorption secondary bearing is arranged at the lower end of the porous material rotational flow adsorption type multidimensional rotary primary adsorption pipe in a penetrating way, one end of the rotational flow adsorption type multidimensional rotary three-stage connecting pipe is arranged on the multidimensional rotary porous material rotational flow adsorption secondary bearing in a penetrating way, the rotational flow adsorption type multidimensional rotary three-stage connecting pipe is arranged on the inner side wall of the magnetic suspension gravity compensation type damping zero damage type fixing box, the utility model discloses a three-dimensional rotary-type air pump of porous material whirl absorption formula multidimension formula, including rotary-flow absorption formula multidimension rotary-type tertiary connecting pipe, the fixed case outside of magnetic suspension gravity compensation formula shock attenuation zero damage type is located to the other end of rotary-flow absorption formula multidimension rotary-type tertiary connecting pipe, rotary-flow absorption formula multidimension rotary-type secondary motor is located on the inboard of magnetic suspension gravity compensation formula shock attenuation zero damage type fixed case, the output of rotary-flow absorption formula multidimension rotary-type secondary motor is located to rotary-type porous material whirl absorption tertiary gear of multidimension, rotary-type porous material whirl absorption tertiary gear of multidimension and rotary-type porous material whirl absorption level four gears link to each other for the meshing rotation.
6. The apparatus according to claim 5, wherein: the multi-ring gyroscope type magnetic force micro-positioning type fixing frame is externally connected with a power supply.
7. The marine locator mounting device according to claim 6, wherein: the liquid nitrogen desublimation frost-forming type capillary form contact type dehumidification capillary is internally provided with a flow passage, the liquid nitrogen desublimation frost-forming type capillary form contact type dehumidification capillary blade is internally provided with a flow passage, and the liquid nitrogen desublimation frost-forming type capillary form contact type dehumidification capillary is internally provided with a flow passage.
CN202111083344.XA 2021-09-16 2021-09-16 Marine locater installation device Active CN114044102B (en)

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JPH09229135A (en) * 1996-02-21 1997-09-02 Yoshiro Oguro Magnetic floating type vibration resistant device
CN203402375U (en) * 2013-08-15 2014-01-22 浙江省舟山市英特讯信息科技有限公司 Integrated safety navigator of ship
CN203402374U (en) * 2013-08-15 2014-01-22 浙江省舟山市英特讯信息科技有限公司 Ship navigator host machine
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CN109238290A (en) * 2018-09-25 2019-01-18 东莞市圣荣自动化科技有限公司 A kind of ship safety navigator installing structure
CN109941405A (en) * 2019-05-08 2019-06-28 江苏海事职业技术学院 A kind of fixation bracket of autical instrument
CN209833945U (en) * 2019-04-04 2019-12-24 中海油信息科技有限公司 Deck fixing device for mounting marine ship operation mobile differential positioning instrument

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH09229135A (en) * 1996-02-21 1997-09-02 Yoshiro Oguro Magnetic floating type vibration resistant device
CN203402375U (en) * 2013-08-15 2014-01-22 浙江省舟山市英特讯信息科技有限公司 Integrated safety navigator of ship
CN203402374U (en) * 2013-08-15 2014-01-22 浙江省舟山市英特讯信息科技有限公司 Ship navigator host machine
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CN209833945U (en) * 2019-04-04 2019-12-24 中海油信息科技有限公司 Deck fixing device for mounting marine ship operation mobile differential positioning instrument
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