CN217898477U - Storage hanger of aviation pipe fitting - Google Patents

Abstract

The utility model relates to a storage hanger of aviation pipe fitting belongs to pipe fitting storage field. The technical scheme is mainly used for storing the problematic aviation pipe fittings and comprises a fixing plate and a fixing shell, wherein nine groups of shock absorbers are mounted on the front surface of the fixing plate, and the fixing shell is mounted on the front surface of the nine groups of shock absorbers; the utility model discloses a drying layer, including the set casing, the inboard of intercommunication shell is installed through solid fixed ring, the one side surface mounting of set casing has humidity control switch, the top of set casing is run through and is installed the intercommunication shell, two sets of air discharge fans are installed through the connecting plate to the inboard of intercommunication shell, the drying layer is installed through solid fixed ring to the inboard of intercommunication shell. The utility model discloses a humidity control switch, air discharge fan and dry layer are installed to the set casing, and humidity control switch carries the electric energy to the inside of air discharge fan, and the air discharge fan produces suction to the inside air of set casing, and the dry layer absorbs the steam in the air, accomplishes the dehumidification of the inside air of device, prolongs the corrosion speed of aviation pipe fitting metal, improves device storage effect.

Description

Storage hanger of aviation pipe fitting

Technical Field

The utility model relates to a pipe fitting storage technology field especially relates to a storage hanger of aviation pipe fitting.

Background

Aviation pipe fitting is as the transport unit who uses commonly in the modern aviation field, its main function lies in installing the inside to the aircraft, undertake oil transport, tasks such as gas transport and water transport, and in current aircraft use and maintenance process, in order to guarantee the safety of aircraft, often need to store the hanger at the internally mounted aviation pipe fitting of aircraft, thereby when the damage takes place for the inside pipe fitting of aircraft, can take out the inside aviation pipe fitting of aviation pipe fitting storage hanger, the replacement of aircraft aviation pipe fitting of being convenient for, the current aviation pipe fitting storage hanger of while, because of lacking dry auxiliary component, often lead to aviation pipe fitting because of the air erosion that contains a large amount of steam, cause aviation pipe fitting part metal to take place the corrosion, and then influence the storage effect of aviation pipe fitting.

Compare in current aviation pipe fitting storage hanger, the utility model discloses added dehumidification auxiliary component, in the device use, can store up the inside dehumidification of hanger and handle to delay aviation pipe fitting and receive the corrosion speed of vapor erosion, improve the storage effect of hanger.

SUMMERY OF THE UTILITY MODEL

The utility model aims at providing a storage hanger of aviation pipe fitting to the problem that exists among the background art.

The technical scheme of the utility model: the storage rack for the aviation pipe fittings comprises a fixing plate and a fixing shell, wherein nine groups of shock absorbers are mounted on the front surface of the fixing plate, the fixing shell is mounted on the front surface of the nine groups of shock absorbers, a coded lock is mounted on the front surface of the fixing shell, a box door is mounted on the front surface of the fixing shell through an opening and closing page and located on one side of the coded lock, and an inspection window is mounted on the front surface of the box door;

the humidity control switch is mounted on the outer surface of one side of the fixed shell, the communicating shell is mounted at the top of the fixed shell in a penetrating mode, two groups of exhaust fans are mounted on the inner side of the communicating shell through connecting plates, the drying layer is mounted on the inner side of the communicating shell through a fixing ring, and the drying layer is located below the exhaust fans;

and a lock bolt is arranged on the front surface of the box door and is positioned on the other side of the observation window, and the lock bolt is connected with the coded lock in an embedded manner.

Preferably, ten groups of threaded fixing holes are formed in the front face of the fixing plate in a penetrating mode, and the threaded fixing holes are located on the outer side of the shock absorber.

Preferably, the inner wall of the back of the fixed shell is provided with a plurality of hanging hooks.

Preferably, the gas bomb is installed through the gim peg to the opposite side surface of set casing, the output tube is installed at the top of gas bomb, and the tail end of output tube extends to the inboard of set casing.

Preferably, the outer surface of the output pipe is provided with a manual throttle valve in a penetrating way.

Preferably, the inner walls of the two sides of the fixed shell are respectively provided with a small ultrasonic driving and separating device.

Preferably, the inner side of the communicating shell is provided with a shielding strip, and the shielding strip is positioned above the exhaust fan.

Compared with the prior art, the utility model discloses following profitable technological effect has:

1. the utility model discloses an install humidity control switch, air discharge fan and drying layer, the inside humidity monitoring part of humidity control switch after the device circular telegram, detect the inside humidity of set casing, when the inside humidity of set casing is too high, the inside resistance value of humidity control switch reduces, carry the inside to relay module with the electric energy, relay module switching-over this moment, carry the inside to the air discharge fan with the electric energy, the air discharge fan drives the flabellum and rotates this moment, produce suction to the inside air of set casing, and with air guide to the bottom of drying layer, under the drive of air discharge fan, after getting into the inside of drying layer, the inside dry particle of drying layer, absorb the steam in the air, accomplish the dehumidification of device inside air, the corrosion speed of extension aviation pipe fitting metal, improve the device storage effect.

2. The utility model discloses an install gas bomb, output tube and manual choke valve, after the access of single pipe fitting was accomplished, through external force rotation manual choke valve, manual choke valve was opened this moment, made the output tube intercommunication, and the output tube guides the inside carbon dioxide of gas bomb to the inside of set casing under the pressure effect this moment, dilutes the inside active gas of set casing to delay, pipe fitting surface rubber's oxidation rate, further improve the device and preserve the effect.

Drawings

Fig. 1 is a schematic structural view of a storage hanger for aviation pipe fittings according to the present invention;

FIG. 2 is a schematic view of a front connection portion of the fixing plate of FIG. 1;

FIG. 3 is a cross-sectional partial structural schematic view of the stationary housing of FIG. 1;

fig. 4 is a cross-sectional partial structural schematic view of the communication shell of fig. 1.

Reference numerals: 1. a fixing plate; 2. a shock absorber; 3. a stationary housing; 4. a coded lock; 5. a box door; 6. viewing the window; 7. a humidity control switch; 8. a communicating shell; 9. an exhaust fan; 10. drying the layer; 11. a lock bolt; 12. a threaded fixing hole; 13. hanging a hook; 14. a gas cylinder; 15. an output pipe; 16. a manual throttle valve; 17. a small ultrasonic drive; 18. a shield strip.

Detailed Description

The technical solution of the present invention will be further explained with reference to the accompanying drawings and specific embodiments.

Example one

As shown in fig. 1, 2, 3 and 4, the utility model provides a storage rack for aviation pipe fittings, which comprises a fixing plate 1 and a fixing shell 3, nine sets of dampers 2 are installed on the front surface of the fixing plate 1, the fixing plate 1 provides fixing points for the dampers 2 installed on the outer surface of the fixing plate and threaded fixing holes 12, the dampers 2 are installed on the front surface of the fixing plate 1 and provide fixing points for the fixing shell 3 installed at the tail end of the fixing plate, meanwhile, when the front surface of the fixed shell 3 is impacted by external force, the spring of the shock absorber 2 converts the impact force into elastic potential energy, the impact force is partially absorbed, the stability of the device after impact is improved, the fixed shell 3 is arranged on the front surface of the nine groups of shock absorbers 2, the fixed shell 3 is arranged on the front surface of the shock absorbers 2 and provides fixed points for the coded lock 4, the box door 5, the humidity control switch 7, the communicating shell 8, the hanging hook 13, the gas storage bottle 14 and the small ultrasonic drive-off device 17 which are arranged on the outer surface and inside, meanwhile, a containing space is provided for the aviation pipe fittings stored in the fixing shell 3, the coded lock 4 is arranged on the front surface of the fixing shell 3, an extension rod inside the coded lock 4 extends to the inside of the lock bolt 11 at regular time, the door 5 is fixed to the front surface of the stationary case 3 via the latch 11, and when it is required to open the door 5, the correct password can be input into the coded lock 4, at the moment, the extension rod in the coded lock 4 is contracted to ensure that the box door 5 can be opened under the action of external force, the front surface of the fixed shell 3 is provided with the box door 5 through the opening and closing leaf, the box door 5 is positioned on one side of the coded lock 4, the box door 5 is installed on the front surface of the fixed shell 3 and provides a fixed point for the viewing window 6 and the lock bolt 11 which are installed on the outer surface of the box door, the viewing window 6 is installed on the front surface of the box door 5, and the viewing window 6 is installed on the front surface of the box door 5 and provides a space for a user to observe pipe fittings inside the device; lock plunger 11 is installed in the front of chamber door 5, lock plunger 11 is located the opposite side of looking into window 6, and lock plunger 11 is connected with 4 gomphosis of trick lock, when the extension rod inserts the inside of lock plunger 11, lock plunger 11 provides the fixed point for the tail end of extension rod, fix chamber door 5 to the front of set casing 3, ten sets of screw thread fixing hole 12 have been seted up in running through to the front of fixed plate 1, and screw thread fixing hole 12 is located the outside of bumper shock absorber 2, insert the inside of external bolt screw thread fixing hole 12 before the use device, and be connected the bolt and the wall and accomplish the fixed of device, a plurality of hooks 13 of hanging are installed to the back inner wall of set casing 3, will treat the storage pipe fitting to hang the storage of hanging the inboard completion pipe fitting of hook 13 after the device is fixed, small-size ultrasonic wave driving and separating device 17 is all installed to the both sides inner wall of set casing 3, small-size ultrasonic wave driving and separating device 17 releases the ultrasonic wave that the human ear can's to the inboard of set casing 3 release after the device circular telegram, the ultrasonic wave that the inside small-size animal that the entering into of set casing 3 produced the influence this moment, cause the small-size animal drives the inside fan 8 that the inside of the fan that shelters that the inside of the fan 8 that shelters from entering of the fan that shelters from, and communicate and the inside of the air exhaust fan 8, and communicate the top that the fan that the inside of 18 communicates that the fan that the communication of the fan that prevents to carry out, and communicate the inside of the air, the inside of the fan 8 that shelters from the installation of the device, the inside of 18, and communicate the fan 8, the inside of the fan that the inside of the fan that prevents.

The working principle of the aviation pipe storage hanger based on the first embodiment is that firstly, an external bolt is inserted into the threaded fixing hole 12, the bolt is connected with the wall surface to complete fixing of the device, then, a correct password is input into the coded lock 4, at the moment, an extension rod in the coded lock 4 contracts to ensure that a box door 5 can be opened under the action of external force, a pipe to be stored is hung on the inner side of a hanging hook 13 to complete storage of the pipe, then, a power supply is connected, and at the moment, the fixing shell 3 provides a stable storage space for the aviation pipe.

Example two

As shown in fig. 1 and fig. 4, the utility model provides a storage hanger of aviation pipe fitting compares in embodiment one, and this embodiment still includes: set casing 3 and humidity control switch 7, one side surface mounting of set casing 3 has humidity control switch 7, the inside humidity monitoring part of humidity control switch 7 after the device circular telegram, detect the inside humidity of set casing 3, when the inside humidity of set casing 3 is too high, the inside resistance value of humidity control switch 7 reduces, carry the inside to relay module with the electric energy, relay module switching-over this moment, carry the inside to air discharge fan 9 with the electric energy, the top of set casing 3 is run through and is installed intercommunication shell 8, intercommunication shell 8 is installed to the top of set casing 3, for its inboard air discharge fan 9 of installing, drying layer 10 and sheltering from strip 18 provide the fixed point, two sets of air discharge fan 9 are installed through the connecting plate to the inboard of intercommunication shell 8, when the electric energy carries to the inside of air discharge fan 9 via humidity control switch 7, air discharge fan 9 drives the flabellum rotation, produce the suction to the inside air of set casing 3, and lead the bottom to drying layer 10, drying layer 10 is installed through solid fixed ring to the inboard of intercommunication shell 8, and drying layer 10 is located the below air discharge fan 9, the inside air that the extension goes into, the dry particle device that the extension goes on the inside of drying pipe, the dry particle, the extension of dry particle, the inside of drying device, the extension is carried out, the inside of dry particle, the extension of dry particle, the extension is carried out, the dry particle.

EXAMPLE III

As shown in fig. 3, the utility model provides a storage hanger of aviation pipe fitting compares in embodiment one or embodiment two, and this embodiment still includes: stationary casing 3 and gas bomb 14, gas bomb 14 is installed through the gim peg to the opposite side surface of stationary casing 3, and gas bomb 14 provides the storage space for the carbon dioxide gas of its inside storage, and output tube 15 for its top installation provides the fixed point simultaneously, output tube 15 is installed at gas bomb 14's top, and the tail end of output tube 15 extends to the inboard of stationary casing 3, output tube 15 intercommunication back, guide the inside carbon dioxide of gas bomb 14 to stationary casing 3's inside under the pressure effect, dilute the inside active gas of stationary casing 3, thereby delay, the oxidation rate of pipe fitting surface rubber, the effect is preserved to further improve the device, manual choke valve 16 is installed in the surface through of output tube 15, after single pipe fitting access is accomplished, manual choke valve 16 is rotated through external force, manual choke valve 16 is opened this moment, make output tube 15 communicate.

The above embodiments are merely some preferred embodiments of the present invention, and those skilled in the art can make various alternative modifications and combinations to the above embodiments based on the technical solution of the present invention and the related teachings of the above embodiments.

Claims (7)

1. The utility model provides a storage hanger of aviation pipe fitting, includes fixed plate (1) and set casing (3), its characterized in that: nine groups of shock absorbers (2) are mounted on the front surface of the fixing plate (1), a fixing shell (3) is mounted on the front surface of the nine groups of shock absorbers (2), a coded lock (4) is mounted on the front surface of the fixing shell (3), a box door (5) is mounted on the front surface of the fixing shell (3) through a folding page, the box door (5) is located on one side of the coded lock (4), and an observation window (6) is mounted on the front surface of the box door (5);

the humidity control switch (7) is mounted on the outer surface of one side of the fixed shell (3), the communicating shell (8) is mounted at the top of the fixed shell (3) in a penetrating mode, two groups of exhaust fans (9) are mounted on the inner side of the communicating shell (8) through connecting plates, the drying layer (10) is mounted on the inner side of the communicating shell (8) through fixing rings, and the drying layer (10) is located below the exhaust fans (9);

the front surface of the box door (5) is provided with a lock bolt (11), the lock bolt (11) is positioned on the other side of the viewing window (6), and the lock bolt (11) is connected with the coded lock (4) in an embedded mode.

2. The storage hanger of aviation pipe fitting of claim 1, wherein: ten groups of thread fixing holes (12) are formed in the front face of the fixing plate (1) in a penetrating mode, and the thread fixing holes (12) are located on the outer side of the shock absorber (2).

3. The storage hanger of aviation pipe fitting of claim 1, characterized in that: the inner wall of the back of the fixed shell (3) is provided with a plurality of hanging hooks (13).

4. The storage hanger of aviation pipe fitting of claim 1, wherein: gas bomb (14) are installed through the gim peg to the opposite side surface of set casing (3), output tube (15) are installed at the top of gas bomb (14), and the tail end of output tube (15) extends to the inboard of set casing (3).

5. The storage hanger of aviation pipe fitting of claim 4, wherein: and a manual throttle valve (16) is arranged on the outer surface of the output pipe (15) in a penetrating way.

6. The storage hanger of aviation pipe fitting of claim 1, wherein: and small ultrasonic driving and separating devices (17) are arranged on the inner walls of the two sides of the fixed shell (3).

7. The storage hanger of aviation pipe fitting of claim 1, wherein: the inner side of the communicating shell (8) is provided with a shielding strip (18), and the shielding strip (18) is positioned above the exhaust fan (9).

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