CN111577077A - Processing method of high-strength alloy for civil air defense door - Google Patents
Processing method of high-strength alloy for civil air defense door Download PDFInfo
- Publication number
- CN111577077A CN111577077A CN202010391516.9A CN202010391516A CN111577077A CN 111577077 A CN111577077 A CN 111577077A CN 202010391516 A CN202010391516 A CN 202010391516A CN 111577077 A CN111577077 A CN 111577077A
- Authority
- CN
- China
- Prior art keywords
- alloy
- core layer
- air defense
- civil air
- defense door
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Images
Classifications
-
- E—FIXED CONSTRUCTIONS
- E06—DOORS, WINDOWS, SHUTTERS, OR ROLLER BLINDS IN GENERAL; LADDERS
- E06B—FIXED OR MOVABLE CLOSURES FOR OPENINGS IN BUILDINGS, VEHICLES, FENCES OR LIKE ENCLOSURES IN GENERAL, e.g. DOORS, WINDOWS, BLINDS, GATES
- E06B5/00—Doors, windows, or like closures for special purposes; Border constructions therefor
- E06B5/10—Doors, windows, or like closures for special purposes; Border constructions therefor for protection against air-raid or other war-like action; for other protective purposes
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/04—Ferrous alloys, e.g. steel alloys containing manganese
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/06—Ferrous alloys, e.g. steel alloys containing aluminium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/28—Ferrous alloys, e.g. steel alloys containing chromium with titanium or zirconium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/38—Ferrous alloys, e.g. steel alloys containing chromium with more than 1.5% by weight of manganese
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C8/00—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
- C23C8/06—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases
- C23C8/08—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases only one element being applied
- C23C8/24—Nitriding
- C23C8/26—Nitriding of ferrous surfaces
-
- E—FIXED CONSTRUCTIONS
- E06—DOORS, WINDOWS, SHUTTERS, OR ROLLER BLINDS IN GENERAL; LADDERS
- E06B—FIXED OR MOVABLE CLOSURES FOR OPENINGS IN BUILDINGS, VEHICLES, FENCES OR LIKE ENCLOSURES IN GENERAL, e.g. DOORS, WINDOWS, BLINDS, GATES
- E06B3/00—Window sashes, door leaves, or like elements for closing wall or like openings; Layout of fixed or moving closures, e.g. windows in wall or like openings; Features of rigidly-mounted outer frames relating to the mounting of wing frames
- E06B3/30—Coverings, e.g. protecting against weather, for decorative purposes
-
- E—FIXED CONSTRUCTIONS
- E06—DOORS, WINDOWS, SHUTTERS, OR ROLLER BLINDS IN GENERAL; LADDERS
- E06B—FIXED OR MOVABLE CLOSURES FOR OPENINGS IN BUILDINGS, VEHICLES, FENCES OR LIKE ENCLOSURES IN GENERAL, e.g. DOORS, WINDOWS, BLINDS, GATES
- E06B3/00—Window sashes, door leaves, or like elements for closing wall or like openings; Layout of fixed or moving closures, e.g. windows in wall or like openings; Features of rigidly-mounted outer frames relating to the mounting of wing frames
- E06B3/70—Door leaves
-
- E—FIXED CONSTRUCTIONS
- E06—DOORS, WINDOWS, SHUTTERS, OR ROLLER BLINDS IN GENERAL; LADDERS
- E06B—FIXED OR MOVABLE CLOSURES FOR OPENINGS IN BUILDINGS, VEHICLES, FENCES OR LIKE ENCLOSURES IN GENERAL, e.g. DOORS, WINDOWS, BLINDS, GATES
- E06B3/00—Window sashes, door leaves, or like elements for closing wall or like openings; Layout of fixed or moving closures, e.g. windows in wall or like openings; Features of rigidly-mounted outer frames relating to the mounting of wing frames
- E06B3/70—Door leaves
- E06B3/7015—Door leaves characterised by the filling between two external panels
-
- E—FIXED CONSTRUCTIONS
- E06—DOORS, WINDOWS, SHUTTERS, OR ROLLER BLINDS IN GENERAL; LADDERS
- E06B—FIXED OR MOVABLE CLOSURES FOR OPENINGS IN BUILDINGS, VEHICLES, FENCES OR LIKE ENCLOSURES IN GENERAL, e.g. DOORS, WINDOWS, BLINDS, GATES
- E06B5/00—Doors, windows, or like closures for special purposes; Border constructions therefor
- E06B5/20—Doors, windows, or like closures for special purposes; Border constructions therefor for insulation against noise
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Securing Of Glass Panes Or The Like (AREA)
Abstract
The invention discloses a processing method of high-strength alloy for a civil air defense door, wherein the high-strength alloy is used as a civil air defense door alloy plate body of the civil air defense door, the civil air defense door alloy plate body comprises a first alloy plate and a second alloy plate which are provided with a spacing space and are in a parallel and level shape, the first alloy plate and the second alloy plate are integrally pressed and installed with a middle core layer alloy panel strip positioned in the middle of the spacing space through a cold assembly process, and simultaneously, a left end surface core layer alloy panel strip and a right end surface core layer alloy panel strip positioned on two sides of the spacing space are integrally pressed and installed through the cold assembly process, wherein, the middle core layer alloy panel strip and the left end surface core layer alloy panel strip and the right end surface core layer alloy panel strip respectively form a distance which is distributed in a bilateral symmetry way, rollers are respectively installed in the distances positioned at the upper end and the lower end, and the civil air defense door alloy; the invention can obviously improve the sound insulation effect and further improve the structural strength of the alloy plate body of the civil air defense door.
Description
Technical Field
The invention relates to the field of manufacturing of civil air defense doors, in particular to a processing method of a high-strength alloy for a civil air defense door.
Background
The civil air defense door is a door at the entrance and exit of the civil protection project, the classification of the civil air defense door is more distinct, and the civil air defense door comprises a common single-leaf protective airtight door and a common double-leaf protective airtight door, and the door is shaped earliest and is widely selected. The entrance and exit device has the characteristics of simple structure, reliable operation and convenient maintenance, and is suitable for the entrances and exits of various civil air defense projects. People's air defense door weight is very heavy, and the conventionality all adopts run from opposite directions rotation or singly to open the rotation mode, needs the manual work to open, opens the door and closes the door and hit the people easily, not only has the potential safety hazard, and sealed effect when closing is equally relatively poor.
The applicant therefore wishes to seek technical solutions that improve on the above technical problem.
Disclosure of Invention
In view of the above, the present invention is directed to a method for processing a high strength alloy for a civil air defense door, which can significantly improve a sound insulation effect and further improve the structural strength of an alloy plate body of the civil air defense door.
The technical scheme adopted by the invention is as follows:
a safe and efficient civil air defense door alloy structure comprises a door frame fixedly installed on a wall body, wherein one side opening of the door frame is sealed through the wall body, the other side opening of the door frame is selectively opened and closed through a civil air defense door alloy plate, slide rails are respectively arranged in upper and lower frames of the door frame, the civil air defense door alloy plate can be relatively slidably installed in the slide rails to selectively open and close, the civil air defense door alloy plate comprises a civil air defense door alloy plate body, the upper end and the lower end of the civil air defense door alloy plate body are respectively slidably installed in the slide rails corresponding to the upper and lower frames through rollers, meanwhile, a sliding driving assembly is arranged at the bottom of the civil air defense door alloy plate body, the sliding driving assembly comprises a driving installation plate fixedly installed at the bottom of the civil air defense door alloy plate body, a driving gear and a driven gear which are connected in a meshing manner are respectively installed on the, driven gear is connected with the spur rack meshing of installing in people's air defense door alloy plate body bottom under driving motor's drive effect, people's air defense door alloy plate body is in slide rail slides and realizes the selectivity and open and close.
Preferably, the driving gear has an outer diameter smaller than an outer diameter of the driven gear.
Preferably, the upper end and the lower extreme of people's air defense door alloy plate body are equipped with respectively and are interval distribution's first gyro wheel and second gyro wheel, first gyro wheel and second gyro wheel are installed through the roller shaft respectively on the people's air defense door alloy plate body.
Preferably, the slide rail on the lower frame and the spur rack are distributed in parallel, and the spur rack is located outside relative to the slide rail.
Preferably, the driving motor is a servo motor, and is connected with an operation panel installed on the wall board in a wired manner or is wirelessly connected with an external operation remote controller, so as to realize the opening and closing of the servo motor.
Preferably, the driving motor is mounted on the driving mounting plate, and an output shaft of the driving motor is fixedly connected with the driving gear.
Preferably, the driven gear can be sleeved on a gear shaft in a relatively rotating mode through a flange bearing, and the gear shaft is fixedly installed on the driving installation plate and is locked through a nut.
In consideration of the fact that the existing civil air defense door is poor in durability, prone to rusting and not wear-resistant, and further the protection effect is affected negatively, the service life of the civil air defense door can be affected, in order to improve the strength of the civil air defense door, the invention provides a high-strength alloy for the civil air defense door, which adopts an alloy steel plate as a raw material steel plate, wherein the alloy steel plate comprises the following components:
1-2.5 wt% aluminum;
0.08-0.15 wt% carbon;
1-2 wt% manganese;
0.08-0.2 wt% titanium;
0.2-0.6 wt% chromium;
the balance of iron;
and carrying out a nitriding treatment process on the alloy steel plate, and forming a durable nitriding protective layer on the surface of the alloy steel plate.
Preferably, the thickness of the durable nitriding protective layer ranges from 10 microns to 30 microns, and the thickness of the alloy steel plate ranges from 1 mm to 5 mm.
Preferably, the nitriding treatment process adopts a gas nitriding process, and the gas nitriding process comprises the following operation steps:
A10) carrying out surface physical treatment or chemical treatment on the alloy steel plate, and removing oil stains on the surface of the alloy steel plate;
A20) placing the alloy steel plate after the surface treatment in a nitriding furnace, and injecting ammonia gas into the nitriding furnace, wherein the ammonia gas is subjected to thermal decomposition at the nitriding temperature to obtain a nitrogen monomer, and the nitrogen monomer permeates into the surface of the alloy steel plate to form a durable nitriding protective layer on the surface of the alloy steel plate;
A30) and cooling and taking out to obtain the high-strength alloy for the civil air defense door.
Preferably, the nitriding temperature is 560-.
Preferably, the people's air defense door alloy plate body of high strength alloy conduct people's air defense door for the people's air defense door, the upper end and the lower extreme of people's air defense door alloy plate body are respectively through gyro wheel slidable mounting in the slide rail rather than corresponding, simultaneously people's air defense door alloy plate body bottom is equipped with the slip drive subassembly, wherein, the slip drive subassembly includes fixed mounting and is in the drive mounting panel of people's air defense door alloy plate body bottom, install driving gear and the driven gear that the meshing is connected on the drive mounting panel respectively, the driving gear is connected with the driving motor drive, driven gear is connected with the spur rack meshing of installing in people's air defense door alloy plate body bottom under driving motor's the drive effect, people's air defense door alloy plate body is in slide in the slide rail and realize the.
Preferably, the driving motor is mounted on the driving mounting plate, and an output shaft of the driving motor is fixedly connected with the driving gear; the driven gear can be sleeved on a gear shaft in a relatively rotating mode through a flange bearing, the gear shaft is fixedly installed on the driving installation plate, and meanwhile the driven gear is locked through a nut.
The invention provides a processing method of high-strength alloy for a civil air defense door, the high-strength alloy is used as a civil air defense door alloy plate body of the civil air defense door, the civil air defense door alloy plate body comprises a first alloy plate and a second alloy plate which are provided with a spacing space and are in a flush state, the first alloy plate and the second alloy plate are integrally pressed and mounted with a middle core layer alloy panel positioned in the middle of the spacing space through a cold assembly process, meanwhile, the left end surface core layer alloy inlaid strip and the right end surface core layer alloy inlaid strip which are positioned at the two sides of the spacing space are integrally pressed and installed through a cold assembling process, wherein, the middle core layer alloy inlaid strips respectively form intervals which are distributed in bilateral symmetry with the left end surface core layer alloy inlaid strips and the right end surface core layer alloy inlaid strips, and the upper end and the lower end of the frame are respectively provided with a roller, and the alloy plate body of the civil air defense door is connected with a sliding rail on the door frame in a sliding installation manner through the rollers.
Preferably, the upper and lower end faces of the middle core layer alloy panel, the left end face core layer alloy panel and the right end face core layer alloy panel are opposite to each other, the first alloy plate extends outwards respectively to form a first sealing reinforcing boss clamped with the door frame, and the right end faces of the left end face core layer alloy panel and the right end face core layer alloy panel extend outwards to form a second sealing reinforcing boss clamped with the door frame.
Preferably, the first alloy plate and the second alloy plate are respectively provided with roller mounting holes which are correspondingly matched, mounting shafts are fixedly inserted in the roller mounting holes, and the rollers are mounted on the mounting shafts in a relatively rotatable manner.
Preferably, the cold assembly process comprises freezing the middle core alloy panel, the left end core alloy panel and the right end core alloy panel by using a freezer, wherein the temperature of the freezer is not more than-20 ℃.
Preferably, the cold assembling process comprises the following operation steps:
s10), setting the temperature of the refrigerator at-35 ℃ to-25 ℃;
s20), placing the middle core layer alloy panel to be frozen, the left end surface core layer alloy panel and the right end surface core layer alloy panel in a freezer, wherein the freezing time is not less than 20 minutes, and the freezing effect of the middle core layer alloy panel, the left end surface core layer alloy panel and the right end surface core layer alloy panel is ensured;
s30), taking out the middle core layer alloy panel from the refrigerator and pressing the alloy panel into the middle of the spacing space, and then taking out the left end surface core layer alloy panel and the right end surface core layer from the refrigerator in sequence and laminating the alloy panel and the right end surface core layer into two sides of the spacing space;
s40), and after the middle core layer alloy inlaid strip, the left end surface core layer alloy inlaid strip and the right end surface core layer alloy inlaid strip return to the room temperature, finishing the cold assembly process.
Preferably, be equipped with the slide rail in the last lower frame of door frame respectively, people's air defense door alloy plate body pass through the gyro wheel with slide rail slidable mounting connects and realizes the selectivity and open and close, wherein, people's air defense door alloy plate body bottom is equipped with the mounting groove installation sliding drive subassembly in the mounting groove, sliding drive subassembly includes fixed mounting and is in the drive mounting panel of people's air defense door alloy plate body bottom, install driving gear and the driven gear that the meshing is connected on the drive mounting panel respectively, the driving gear is connected with the driving motor drive, driven gear is connected with the spur rack meshing of installing in people's air defense door alloy plate body bottom under driving motor's the drive effect, people's air defense door alloy plate body is in slide in the slide rail and realize the selectivity and open and close.
Preferably, the first alloy plate and the second alloy plate are made of alloy steel plates, and the alloy steel plates comprise the following components:
1-2.5 wt% aluminum;
0.08-0.15 wt% carbon;
1-2 wt% manganese;
0.08-0.2 wt% titanium;
0.2-0.6 wt% chromium;
the balance of iron;
and carrying out a nitriding treatment process on the alloy steel plate, and forming a durable nitriding protective layer on the surface of the alloy steel plate.
The invention provides a sliding driving assembly arranged at the bottom of an alloy plate body of a civil air defense door, wherein the sliding driving assembly comprises a driving gear and a driven gear which are in meshed connection, the driving gear realizes driving rotation through a driving motor, then transmits driving rotating force to the driven gear through meshed transmission relation, and realizes driving of the alloy plate body of the civil air defense door through meshed connection of the driven gear and a spur rack arranged at the bottom of a door frame, so that the alloy plate body of the civil air defense door selectively slides in a sliding rail of the door frame, and further automatic selective opening and closing of the door frame are realized; the potential safety hazard existing in manual operation is avoided, and meanwhile, the sealing effect in closing is also ensured.
The invention creatively provides an alloy steel plate with 1-2.5 wt% of aluminum and 0.2-0.6 wt% of chromium as a raw material steel plate, and then the alloy steel plate is subjected to a nitriding treatment process, so that a durable nitriding protective layer is formed on the surface of the alloy steel plate.
The invention creatively provides a civil air defense door alloy plate body structure which is formed by using a first alloy plate and a second alloy plate which have an interval space and are in a parallel and level shape as base plate materials of the civil air defense door alloy plate body, integrally press-mounting a middle core layer alloy panel in the middle of the interval space through a cold assembly process, and integrally press-mounting a left end surface core layer alloy panel and a right end surface core layer alloy panel on two sides of the interval space through the cold assembly process, so that the civil air defense door alloy plate body structure is formed, the sound insulation effect can be obviously improved by the double-layer alloy plates distributed at intervals, and the structural strength of the civil air defense door alloy plate body can be further improved by the middle core layer alloy panel, the left end surface core layer alloy panel and the right; the invention further preferably provides a structure that the first sealing reinforcing lug boss and the second sealing reinforcing lug boss which extend outwards are arranged for each core layer alloy panel, so that the structural strength can be improved, and the sealing effect of the alloy plate body of the civil air defense door when the alloy plate body is closed can be further ensured.
Drawings
FIG. 1 is a schematic structural diagram of an alloy structure of a safe and efficient civil air defense door according to an embodiment of the invention;
FIG. 2 is an exploded view of FIG. 1;
FIG. 3 is a schematic structural diagram of a civil air defense door alloy plate according to an embodiment of the invention;
FIG. 4 is an enlarged view of the structure of FIG. 3 at A;
FIG. 5 is a block diagram of the steps of a gas nitriding process for a high strength alloy for a passenger door according to an embodiment of the present invention;
FIG. 6 illustrates a cold assembly process according to an embodiment of the present invention.
Detailed Description
The embodiment of the invention discloses a processing method of high-strength alloy for a civil air defense door, wherein the high-strength alloy is used as a civil air defense door alloy plate body of the civil air defense door, the civil air defense door alloy plate body comprises a first alloy plate and a second alloy plate which are provided with a spacing space and are in a parallel and level shape, the first alloy plate and the second alloy plate are integrally pressed and installed with a middle core layer alloy panel strip positioned in the middle of the spacing space through a cold assembly process, and simultaneously, a left end surface core layer alloy panel strip and a right end surface core layer alloy panel strip positioned on two sides of the spacing space are integrally pressed and installed through the cold assembly process, wherein, the middle core layer alloy panel strip and the left end surface core layer alloy panel strip and the right end surface core layer alloy panel strip respectively form intervals which are distributed in a bilateral symmetry mode, rollers are respectively installed in the intervals positioned at the upper end and the lower end, and the civil air defense door alloy.
In order to make those skilled in the art better understand the technical solution of the present invention, the technical solution in the embodiment of the present invention will be clearly and completely described below with reference to the drawings in the embodiment of the present invention, and it is obvious that the described embodiment is only a part of the embodiment of the present invention, and not all embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Example 1: please refer to fig. 1 and 2, which illustrate a safe and efficient civil air defense door alloy structure 1, comprising a door frame 10 fixedly installed on a wall, one side opening of the door frame 10 is closed by the wall, the other side opening is selectively opened and closed by a civil air defense door alloy plate 20, slide rails 13 are respectively arranged in an upper frame 11 and a lower frame 12 of the door frame 10, the civil air defense door alloy plate 20 can be relatively slidably installed in the slide rails 13 to selectively open and close, the civil air defense door alloy plate 20 comprises a civil air defense door alloy plate body 21, the upper end and the lower end of the civil air defense door alloy plate body 21 are respectively slidably installed in the corresponding slide rails 13 by rollers, and a sliding driving assembly 30 is arranged at the bottom of the civil air defense door alloy plate body 21, wherein the sliding driving assembly 30 comprises a driving installation plate 31 fixedly installed at the bottom of the civil air defense door alloy plate body 21, a driving gear 32 and a driven gear 33 which are respectively installed on, the driving gear 32 is in driving connection with the driving motor 34, the driven gear 33 is in meshing connection with the spur rack 23 arranged at the bottom of the civil air defense door alloy plate body 21, and under the driving action of the driving motor 34, the civil air defense door alloy plate body 21 slides in the slide rail 13 to realize selective opening and closing; preferably, in the present embodiment, the driving motor 34 is a servo motor, and is connected to an operation panel installed on the wall board in a wired manner, or is connected to an external operation remote controller in a wireless manner, so as to enable the servo motor to be turned on and off;
preferably, in the present embodiment, the upper end and the lower end of the civil air defense door alloy plate body 21 are respectively provided with a first roller 22a and a second roller 22b which are distributed at intervals, and the first roller 22a and the second roller 22b are respectively installed on the civil air defense door alloy plate body 21 through a roller shaft 24; the slide rail 13 positioned on the lower frame 12 and the spur rack 23 are arranged in parallel, and the spur rack 23 is positioned at the outer side relative to the slide rail 13;
preferably, in the present embodiment, the outer diameter of the driving gear 32 is smaller than that of the driven gear 33 for realizing the reduction transmission effect; the driving motor 34 is installed on the driving installation plate 31, and the output shaft thereof is fixedly connected with the driving gear 32; the driven gear 33 is sleeved on a gear shaft 36 in a relatively rotatable manner through a flange bearing 35, and the gear shaft 36 is fixedly installed on the driving installation plate 31 and is locked by a nut 37.
The embodiment proposes that the sliding driving assembly 30 is arranged at the bottom of the alloy plate body 21 of the civil air defense door, the sliding driving assembly 30 comprises a driving gear 32 and a driven gear 33 which are connected in a meshed manner, the driving gear 32 is driven to rotate through a driving motor 34, then the driving rotating force is transmitted to the driven gear 33 through a meshed transmission relation, and the driven gear 33 is meshed with a spur rack 23 arranged at the bottom of the door frame 10 to drive the alloy plate body 21 of the civil air defense door, so that the alloy plate body 21 of the civil air defense door selectively slides in the door frame slide rail 13, and further, the automatic selective opening and closing of the door frame 10 are realized; the potential safety hazard existing in manual operation is avoided, and meanwhile, the sealing effect in closing is also ensured.
Example 2: the present embodiment proposes a high-strength alloy for a civil air defense door, which is a civil air defense door alloy plate body 21 in embodiment 1, using an alloy steel plate as a raw material steel plate, the alloy steel plate comprising the following components:
1-2.5 wt% aluminum;
0.08-0.15 wt% carbon;
1-2 wt% manganese;
0.08-0.2 wt% titanium;
0.2-0.6 wt% chromium;
the balance of iron;
performing a nitriding treatment process on the alloy steel plate to form a durable nitriding protective layer on the surface of the alloy steel plate;
preferably, in the present embodiment, the thickness of the durable nitriding protective layer ranges from 10 to 30 μm, and the thickness of the alloy steel plate ranges from 1 to 5 mm;
preferably, in this embodiment, the nitridation process is a gas nitridation process, and as shown in fig. 5, the gas nitridation process includes the following steps:
A10) carrying out surface physical treatment or chemical treatment on the alloy steel plate for removing oil stains on the surface of the alloy steel plate; the physical treatment can be polishing treatment, and the chemical treatment can be cleaning agent treatment;
A20) placing the alloy steel plate after the surface treatment in a nitriding furnace, injecting ammonia gas into the nitriding furnace, wherein the ammonia gas is subjected to thermal decomposition at the nitriding temperature to obtain a nitrogen monomer, and the nitrogen monomer permeates into the surface of the alloy steel plate to form a durable nitriding protective layer on the surface of the alloy steel plate; preferably, the nitriding temperature is 560-;
A30) and taking out after cooling to obtain the high-strength alloy 21 for the civil air defense door.
The embodiment creatively provides an alloy steel plate with 1-2.5 wt% of aluminum and 0.2-0.6 wt% of chromium as a raw material steel plate, then the alloy steel plate is subjected to a nitriding treatment process, so that a durable nitriding protective layer is formed on the surface of the alloy steel plate, and the surface of the alloy steel plate has good wear resistance and corrosion resistance on the basis of ensuring good adhesive force and impact resistance of the durable nitriding protective layer due to the excellent nitriding characteristics of the aluminum and the chromium, and the high-strength alloy is applied to the alloy plate body 21 of the civil air defense door, so that the installation strength of the civil air defense door can be further improved.
The applicant compares the technical effects of the high-strength alloy for the civil air defense door obtained in the embodiment with the raw steel plate (a 5 size sample plate is taken by cutting for comparative test) used in the embodiment, and the comparison results are shown in the following table 1:
the application also carries out abrasion test comparison, and finds that the wear resistance of the high-strength alloy for the civil air defense door with the durable nitriding protective layer is obviously better than that of a raw steel plate.
Example 3: referring to fig. 3 and 4 in combination with fig. 1 and 2, this embodiment proposes a method for processing a high-strength alloy for a civil air defense door, in which the high-strength alloy is used as the alloy plate body 21 of the civil air defense door in example 1, the alloy plate body 21 of the civil air defense door includes a first alloy plate 21a and a second alloy plate 21b which are parallel and level with each other and have a spacing space, the first alloy plate 21a and the second alloy plate 21b are integrally press-fitted with a middle core alloy insert 21c located in the middle of the spacing space by a cold-fitting process, and also integrally press-fitted with a left end core alloy insert 21d and a right end core alloy insert 21e located on both sides of the spacing space by a cold-fitting process, wherein the middle core alloy insert 21c forms a left-right symmetrically distributed spacing with the left end core alloy insert 21d and the right end core alloy insert 21e, a first roller 22a and a second roller 22b are respectively arranged in the space between the upper end and the lower end, and the civil air defense door alloy plate body 21 is connected with the sliding rail 13 on the door frame 10 in a sliding way through the first roller 22a and the second roller 22 b;
preferably, in the present embodiment, the upper and lower end surfaces of the middle core alloy insert 21c, the left end surface core alloy insert 21d, and the right end surface core layer alloy insert 21e respectively extend outward relative to the first alloy plate 21a to form a first seal reinforcement boss 21f engaged with the door frame 10, and the right end surfaces of the left end surface core alloy insert 21d and the right end surface core layer alloy insert 21e extend outward to form a second seal reinforcement boss 21g engaged with the door frame;
preferably, in the present embodiment, the first alloy plate 21a and the second alloy plate 21b are respectively provided with roller mounting holes 21h which are correspondingly engaged, a mounting shaft 21i is fixedly inserted into the roller mounting holes 21h, and rollers 22a and 22b are relatively rotatably mounted on the mounting shaft 21 i;
preferably, in the present embodiment, the cold-assembling process uses a freezer to freeze the middle core alloy insert 21c, the left end core alloy insert 21d, and the right end core alloy insert 21e, and the temperature of the freezer is not greater than-20 ℃;
specifically, in this embodiment, referring to fig. 6, the operation steps of the cold assembling process are as follows:
s10), setting the temperature of the freezer at-35 ℃ to-25 ℃, specifically, in the present embodiment, setting the temperature of the freezer at-30 ℃;
s20), placing the middle core layer alloy insert 21c, the left end surface core layer alloy insert 21d and the right end surface core layer alloy insert 21e to be frozen in a freezer, wherein the freezing time is not less than 20 minutes, particularly preferably, the freezing time is kept at 25 minutes, and the freezing effect of the middle core layer alloy insert 21c, the left end surface core layer alloy insert 21d and the right end surface core layer alloy insert 21e is ensured;
s30), taking the middle core layer alloy panel 21c out of the refrigerator and pressing the middle core layer alloy panel into the middle of the spacing space, and then taking the left end surface core layer alloy panel 21d and the right end surface core layer 21e out of the refrigerator and pressing the left end surface core layer alloy panel 21d and the right end surface core layer alloy panel into two sides of the spacing space in sequence;
s40), and after the middle core layer alloy gib 21c, the left end surface core layer alloy gib 21d, and the right end surface core layer alloy gib 21e return to room temperature, completing the cold assembly process.
In the present embodiment, the high-strength alloy for a passenger air door described in example 2 is preferably used for the first alloy plate 21a and the second alloy plate 21 b.
The embodiment creatively provides that a first alloy plate 21a and a second alloy plate 21b which are provided with an interval space and are in a parallel and level shape are used as base plate materials of the alloy plate body of the civil air defense door, meanwhile, a middle core layer alloy panel 21c is integrally pressed in the middle of the interval space through a cold assembly process, and a left end surface core layer alloy panel 21d and a right end surface core layer alloy panel 21e are integrally pressed in two sides of the interval space through the cold assembly process, so that the structure of the alloy plate body 21 of the civil air defense door is formed, the sound insulation effect can be obviously improved through the double-layer alloy plates distributed at intervals, and meanwhile, the structural strength of the alloy plate body 21 of the civil air defense door can be further improved through the middle core layer alloy panel 21c, the left end surface core layer alloy panel 21d and the right; the present embodiment further preferably proposes a structure that a first seal reinforcement boss 21f and a second seal reinforcement boss 21g extending outward are provided for each core layer alloy panel 21c, 21d, 21e, which not only can improve the structural strength, but also can further ensure the sealing effect of the civil air defense door alloy plate body 21 when being closed.
It will be evident to those skilled in the art that the invention is not limited to the details of the foregoing illustrative embodiments, and that the present invention may be embodied in other specific forms without departing from the spirit or essential attributes thereof. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Furthermore, it should be understood that although the present description refers to embodiments, not every embodiment may contain only a single embodiment, and such description is for clarity only, and those skilled in the art should integrate the description, and the embodiments may be combined as appropriate to form other embodiments understood by those skilled in the art.
Claims (7)
1. A processing method of high-strength alloy for a civil air defense door, the high-strength alloy is used as a civil air defense door alloy plate body of the civil air defense door, it is characterized in that the alloy plate body of the civil air defense door comprises a first alloy plate and a second alloy plate which are provided with a spacing space and are in a flush state, the first alloy plate and the second alloy plate are integrally pressed and mounted with a middle core layer alloy panel positioned in the middle of the spacing space through a cold assembly process, meanwhile, the left end surface core layer alloy inlaid strip and the right end surface core layer alloy inlaid strip which are positioned at the two sides of the spacing space are integrally pressed and installed through a cold assembling process, wherein, the middle core layer alloy inlaid strips respectively form intervals which are distributed in bilateral symmetry with the left end surface core layer alloy inlaid strips and the right end surface core layer alloy inlaid strips, and the upper end and the lower end of the frame are respectively provided with a roller, and the alloy plate body of the civil air defense door is connected with a sliding rail on the door frame in a sliding installation manner through the rollers.
2. The processing method of the high-strength alloy for the civil air defense door as claimed in claim 1, wherein the upper and lower end faces of the middle core layer alloy gib, the left end face core layer alloy gib and the right end face core layer alloy gib extend outwards relative to the first alloy plate to form a first sealing reinforcing boss clamped with the door frame, and the right end faces of the left end face core layer alloy gib and the right end face core layer alloy gib extend outwards to form a second sealing reinforcing boss clamped with the door frame.
3. The method of processing a high-strength alloy for a civil air defense door according to claim 1, wherein the first alloy plate and the second alloy plate are provided with roller mounting holes respectively in a corresponding fit, a mounting shaft is fixedly inserted into the roller mounting holes, and the rollers are relatively rotatably mounted on the mounting shaft.
4. The method of claim 1, wherein the cold assembly process comprises freezing the middle core alloy panel, the left end core alloy panel and the right end core alloy panel with a freezer at a temperature of no greater than-20 ℃.
5. The processing method of the high-strength alloy for the civil air defense door according to claim 4, wherein the cold assembly process comprises the following operation steps:
s10), setting the temperature of the refrigerator at-35 ℃ to-25 ℃;
s20), placing the middle core layer alloy panel to be frozen, the left end surface core layer alloy panel and the right end surface core layer alloy panel in a freezer, wherein the freezing time is not less than 20 minutes, and the freezing effect of the middle core layer alloy panel, the left end surface core layer alloy panel and the right end surface core layer alloy panel is ensured;
s30), taking out the middle core layer alloy panel from the refrigerator and pressing the alloy panel into the middle of the spacing space, and then taking out the left end surface core layer alloy panel and the right end surface core layer from the refrigerator in sequence and laminating the alloy panel and the right end surface core layer into two sides of the spacing space;
s40), and after the middle core layer alloy inlaid strip, the left end surface core layer alloy inlaid strip and the right end surface core layer alloy inlaid strip return to the room temperature, finishing the cold assembly process.
6. The method for processing the high-strength alloy for the civil air defense door according to claim 1, wherein the alloy is a high-strength alloy, the upper frame and the lower frame of the door frame are respectively provided with a sliding rail, the alloy plate body of the civil air defense door is connected with the sliding rail in a sliding way through a roller to realize selective opening and closing, wherein, the bottom of the alloy plate body of the civil air defense door is provided with an installation groove, a sliding drive component is arranged in the installation groove, the sliding driving component comprises a driving mounting plate fixedly mounted at the bottom of the alloy plate body of the civil air defense door, the driving mounting plate is respectively provided with a driving gear and a driven gear which are connected in a meshing way, the driving gear is connected with a driving motor in a driving way, the driven gear is connected with a straight rack arranged at the bottom of the alloy plate body of the civil air defense door in a meshing way, under the driving action of the driving motor, the alloy plate body of the civil air defense door slides in the slide rail to realize selective opening and closing.
7. The method of processing a high-strength alloy for a civil air defense door according to claim 1, wherein the first alloy plate and the second alloy plate are made of an alloy steel plate as a raw steel plate, and the alloy steel plate comprises the following components:
1-2.5 wt% aluminum;
0.08-0.15 wt% carbon;
1-2 wt% manganese;
0.08-0.2 wt% titanium;
0.2-0.6 wt% chromium;
the balance of iron;
and carrying out a nitriding treatment process on the alloy steel plate, and forming a durable nitriding protective layer on the surface of the alloy steel plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010391516.9A CN111577077A (en) | 2020-05-11 | 2020-05-11 | Processing method of high-strength alloy for civil air defense door |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010391516.9A CN111577077A (en) | 2020-05-11 | 2020-05-11 | Processing method of high-strength alloy for civil air defense door |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN111577077A true CN111577077A (en) | 2020-08-25 |
Family
ID=72126532
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202010391516.9A Pending CN111577077A (en) | 2020-05-11 | 2020-05-11 | Processing method of high-strength alloy for civil air defense door |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN111577077A (en) |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2003328635A (en) * | 2002-05-16 | 2003-11-19 | Hokuyo Automatic Co | Smoke interruption sliding door |
| CN103031487A (en) * | 2011-09-29 | 2013-04-10 | 财团法人交大思源基金会 | Composition design and treatment method of high-strength, high-ductility and high-corrosion-resistance iron-manganese-aluminum-carbon alloy |
| CN202954816U (en) * | 2012-12-20 | 2013-05-29 | 河南省煤科院耐磨技术有限公司 | Cold-assembly low-cutting resistance durable point-attack pick |
| CN106244770A (en) * | 2016-08-23 | 2016-12-21 | 马鞍山市恒兴耐火炉料厂 | A kind of microalloy reinforcing agent and application and methods for using them thereof |
| CN106433255A (en) * | 2016-08-31 | 2017-02-22 | 南通苏通人防防护设备有限公司 | High-strength civil-air-defence door |
| CN106705748A (en) * | 2016-12-20 | 2017-05-24 | 江苏法尔胜技术开发中心有限公司 | Carbon fiber composite barrel containing metal liner and cold assembly manufacturing method of carbon fiber composite barrel |
| CN108825082A (en) * | 2018-08-18 | 2018-11-16 | 上海祈祿机械有限公司 | A kind of plug-type closed guard gate |
| CN209339803U (en) * | 2018-08-31 | 2019-09-03 | 西安北方惠安机电设备有限公司 | Closed guard gate |
-
2020
- 2020-05-11 CN CN202010391516.9A patent/CN111577077A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2003328635A (en) * | 2002-05-16 | 2003-11-19 | Hokuyo Automatic Co | Smoke interruption sliding door |
| CN103031487A (en) * | 2011-09-29 | 2013-04-10 | 财团法人交大思源基金会 | Composition design and treatment method of high-strength, high-ductility and high-corrosion-resistance iron-manganese-aluminum-carbon alloy |
| CN202954816U (en) * | 2012-12-20 | 2013-05-29 | 河南省煤科院耐磨技术有限公司 | Cold-assembly low-cutting resistance durable point-attack pick |
| CN106244770A (en) * | 2016-08-23 | 2016-12-21 | 马鞍山市恒兴耐火炉料厂 | A kind of microalloy reinforcing agent and application and methods for using them thereof |
| CN106433255A (en) * | 2016-08-31 | 2017-02-22 | 南通苏通人防防护设备有限公司 | High-strength civil-air-defence door |
| CN106705748A (en) * | 2016-12-20 | 2017-05-24 | 江苏法尔胜技术开发中心有限公司 | Carbon fiber composite barrel containing metal liner and cold assembly manufacturing method of carbon fiber composite barrel |
| CN108825082A (en) * | 2018-08-18 | 2018-11-16 | 上海祈祿机械有限公司 | A kind of plug-type closed guard gate |
| CN209339803U (en) * | 2018-08-31 | 2019-09-03 | 西安北方惠安机电设备有限公司 | Closed guard gate |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN105134021B (en) | Pressing sliding door | |
| WO2006097542A1 (en) | Frameless glass door | |
| CN111577077A (en) | Processing method of high-strength alloy for civil air defense door | |
| EP2885479B1 (en) | Sliding window with improved air tightness | |
| CN111550164A (en) | High-strength alloy for civil air defense door | |
| CN204941191U (en) | A kind of pressing sliding door | |
| CN111520039A (en) | Safe and efficient civil air defense door alloy structure | |
| WO2016110161A1 (en) | Refrigerator | |
| CN111207188A (en) | Compound bevel gear reduction box of cold roll forming unit | |
| CN105155960A (en) | Hardware system suitable for laminated sliding door | |
| US9751386B1 (en) | Vehicle screen for side window assembly | |
| KR101065120B1 (en) | Sliding door | |
| CN204941128U (en) | A kind of five metals system being applicable to pressing sliding door | |
| CN108397090A (en) | A kind of pressing sliding door | |
| CN112832627A (en) | A but structure is drawn to formula side that closes for door and window cupboard | |
| CN219509535U (en) | Thermal insulation door | |
| CN209959086U (en) | Foldable prefabricated cabin door structure | |
| CN219572407U (en) | Cold storage door with sealing device | |
| CN2868762Y (en) | Heat-insulation car box of cold-storage fresh-preservation vehicle | |
| CN209523679U (en) | A kind of electric and hand rolling screen door that noise reduction is wear-resisting | |
| CN214792101U (en) | Low-temperature water chilling unit | |
| CN217129349U (en) | Bridge-cut-off aluminum alloy heat insulation window | |
| CN220645786U (en) | Rolling slats door movable support | |
| CN215108069U (en) | Door and window hardware transmission system | |
| CN102242595B (en) | Airtight door and window |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20200825 |