CN211731857U

CN211731857U - Auxiliary assembly is used in aircraft equipment maintenance

Info

Publication number: CN211731857U
Application number: CN201921935699.5U
Authority: CN
Inventors: 瑁磋蕉; 裴轶
Original assignee: XI'AN KANGBEI ELECTROMECHANICAL TECHNOLOGY CO LTD
Current assignee: XI'AN KANGBEI ELECTROMECHANICAL TECHNOLOGY CO LTD
Priority date: 2019-11-11
Filing date: 2019-11-11
Publication date: 2020-10-23
Anticipated expiration: 2029-11-11

Abstract

The utility model relates to an auxiliary assembly technical field just discloses an auxiliary assembly is used in aircraft equipment maintenance, which comprises a base plate, the bottom fixed mounting of base plate has the universal wheel, the top fixed mounting of base plate has the cabinet, the left side fixed mounting of cabinet has the push rod, the top fixed mounting of cabinet has a servo motor, the top of cabinet and the right side fixed mounting who is located a servo motor have the bearing frame. This auxiliary assembly is used in aircraft equipment maintenance, through starting first servo motor, first servo motor passes through the output shaft and drives the pivot and the swivel mount is rotatory, and the swivel mount passes through carousel and mounting panel and drives second leading truck and splint vertical rotation, reaches the effect of simple and convenient vertical rotation regulation, avoids appearing the dead angle in the maintenance process and the condition emergence of the maintenance of being not convenient for to this auxiliary assembly's practicality has been improved, makes this auxiliary assembly facilitate promotion.

Description

Auxiliary assembly is used in aircraft equipment maintenance

Technical Field

The utility model relates to an auxiliary assembly technical field specifically is an auxiliary assembly is used in aircraft equipment maintenance.

Background

The aviation maintenance refers to the maintenance and repair of technical equipment on an airplane to ensure the safety of the airplane, the aviation maintenance is a precondition and a necessary condition for the use of the airplane and is also an important component of aviation industry, an aero-engine is the heart of the airplane, the maintenance of the aero-engine is a part of the maintenance of the airplane and is also an important component of aviation engineering work, and the maintenance of the aviation equipment is generally carried out by taking a lifter as an auxiliary device.

The traditional aviation maintenance auxiliary device is generally of a fixed structure, is inconvenient to adjust the maintenance angle, causes the situations of inconvenient maintenance and the like, and provides an auxiliary device for aviation equipment maintenance to solve the problems.

SUMMERY OF THE UTILITY MODEL

Technical problem to be solved

The utility model provides a not enough to prior art, the utility model provides an auxiliary assembly is used in aircraft equipment maintenance possesses the advantage such as be convenient for adjust, has solved traditional aircraft maintenance auxiliary device and generally is fixed structure, is not convenient for adjust its maintenance angle, causes the problem that the condition emergence such as maintenance is inconvenient.

(II) technical scheme

For the purpose of realizing the aforesaid regulation of being convenient for, the utility model provides a following technical scheme: the utility model provides an auxiliary assembly for maintenance of aviation equipment, includes the base plate, the bottom fixed mounting of base plate has the universal wheel, the top fixed mounting of base plate has the cabinet, the left side fixed mounting of cabinet has the push rod, the top fixed mounting of cabinet has first servo motor, the top of cabinet just is located the right side fixed mounting of first servo motor and has the bearing frame, cup jointed the pivot that runs through and extend to the bearing frame right side on the output shaft of first servo motor, the right side fixed mounting of pivot has the swivel mount, the equal fixed mounting in top and the bottom of swivel mount has the carousel, the inner wall fixed mounting of carousel has the mounting panel, the equal fixed mounting in the back of the body of mounting panel has first leading truck, the equal fixed mounting in the back of the body of first leading truck has electric putter, electric putter's the equal fixed mounting in the back of the body of mutually has the second leading truck that runs through and, the equal fixed mounting in opposite side of second leading truck has splint, the top fixed mounting that the left side of swivel mount just is located the pivot has the balancing weight, the below fixed mounting that the mounting panel bottom just is located the swivel mount has the support, the outer wall of support has cup jointed the toothed disc, the below fixed mounting that the left side of swivel mount just is located the pivot has second servo motor, cup jointed the drive gear with toothed disc engaged with on the output shaft of second servo motor.

Preferably, the number of the universal wheels is four, the four universal wheels are distributed on the bottom of the base plate in a rectangular array, and the brake valves are movably mounted inside the universal wheels.

Preferably, the inner wall fixed mounting of cabinet has the baffle, the outer wall of push rod has cup jointed the resistance-increasing rubber sleeve, the resistance-increasing rubber sleeve is nitrile rubber.

Preferably, the top of cabinet just is located the equal fixed mounting in front and the back of first servo motor and has first fixed block, the left side of swivel mount just is located the equal fixed mounting in front and the back of second servo motor and has the second fixed block.

Preferably, the number of the bearing seats and the number of the turntables are two, and the two turntables are distributed on the opposite sides of the rotating frame by taking the rotating shaft as a symmetry axis.

Preferably, the opposite sides of the clamping plate are fixedly provided with backing plates, and the opposite sides of the backing plates are provided with anti-skidding grooves.

(III) advantageous effects

Compared with the prior art, the utility model provides an auxiliary assembly is used in aircraft equipment maintenance possesses following beneficial effect:

the auxiliary equipment for maintaining the aviation equipment comprises a clamp plate, a part to be maintained is placed on the clamp plate, an electric push rod is started to stretch, the electric push rod drives the clamp plate to move up and down through a second guide frame, so that the distance between the two clamp plates is adjusted, the simple and convenient fixing effect is achieved, a second servo motor is started to rotate, the second servo motor drives a transmission gear to rotate through an output shaft, the transmission gear drives a mounting plate and the second guide frame to rotate horizontally through a gear plate and a support, the simple and convenient horizontal rotation adjustment effect is achieved, the first servo motor is started, the first servo motor drives a rotating shaft and a rotating frame to rotate through the output shaft, the rotating frame drives the second guide frame and the clamp plate to rotate vertically through a turntable and the mounting plate, the simple and convenient vertical rotation adjustment effect is achieved, and the occurrence of dead angle and inconvenience in maintenance is avoided, thereby the practicality of this auxiliary assembly has been improved for this auxiliary assembly facilitate promotion.

Drawings

FIG. 1 is a schematic structural view of the present invention;

fig. 2 is an enlarged view of a position a in the structure diagram 1 of the present invention.

In the figure: the device comprises a base plate 1, universal wheels 2, a storage cabinet 3, a push rod 4, a first servo motor 5, a bearing seat 6, a rotating shaft 7, a rotating frame 8, a rotating disc 9, a mounting plate 10, a first guide frame 11, an electric push rod 12, a second guide frame 13, a clamping plate 14, a balancing weight 15, a support 16, a gear disc 17, a second servo motor 18 and a transmission gear 19.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

Referring to fig. 1-2, an auxiliary device for aircraft equipment maintenance includes a base plate 1, universal wheels 2 are fixedly mounted at the bottom of the base plate 1, the number of the universal wheels 2 is four, the four universal wheels 2 are distributed in a rectangular array at the bottom of the base plate 1, brake valves are movably mounted inside the universal wheels 2, a storage cabinet 3 is fixedly mounted at the top of the base plate 1, a push rod 4 is fixedly mounted at the left side of the storage cabinet 3, a partition plate is fixedly mounted at the inner wall of the storage cabinet 3, a resistance-increasing rubber sleeve is sleeved on the outer wall of the push rod 4, the resistance-increasing rubber sleeve is nitrile rubber, a first servo motor 5 is fixedly mounted at the top of the storage cabinet 3, a bearing seat 6 is fixedly mounted at the top of the storage cabinet 3 and located at the right side of the first servo motor 5, a rotating shaft 7 penetrating and extending to the right side of the bearing seat 6 is sleeved on an output shaft of the, the top and the bottom of a rotating frame 8 are fixedly provided with rotating discs 9, the number of the bearing seats 6 and the rotating discs 9 is two, the two rotating discs 9 are distributed on the rotating frame 8 in opposite sides by taking a rotating shaft 7 as a symmetrical shaft, the inner wall of the rotating disc 9 is fixedly provided with a mounting plate 10, the back side of the mounting plate 10 is fixedly provided with a first guide frame 11, the back side of the first guide frame 11 is fixedly provided with an electric push rod 12, the model of the electric push rod 12 is XTL100, the back side of the electric push rod 12 is fixedly provided with a second guide frame 13 which penetrates through and extends to the opposite side of the mounting plate 10, the opposite side of the second guide frame 13 is fixedly provided with a clamping plate 14, the opposite side of the clamping plate 14 is fixedly provided with a backing plate, the opposite side of the backing plate is provided with an anti-skid groove, the left side of the rotating frame 8 is fixedly provided with a balancing weight 15, the outer wall of the bracket 16 is sleeved with a gear plate 17, the left side of the rotating frame 8 and the lower part of the rotating shaft 7 are fixedly provided with a second servo motor 18, the models of the first servo motor 5 and the second servo motor 18 are POWSM-T-M1-80-02430, the top of the storage cabinet 3 and the front and the back of the first servo motor 5 are fixedly provided with a first fixed block, the left side of the rotating frame 8 and the front and the back of the second servo motor 18 are fixedly provided with a second fixed block, the output shaft of the second servo motor 18 is sleeved with a transmission gear 19 meshed with the gear plate 17, a part to be maintained is placed on the clamping plate 14, the electric push rod 12 is started to extend and retract, the electric push rod 12 drives the clamping plate 14 to move up and down through a second guide frame, so as to adjust the distance between the two clamping plates 14, and achieve the effect of simple and convenient fixation, through starting second servo motor 18 rotatory, second servo motor 18 drives drive gear 19 rotatory through the output shaft, drive gear 19 drives mounting panel 10 and second leading truck 13 horizontal rotation through toothed disc 17 and support 16, reach the effect of simple and convenient horizontal rotation regulation, rethread starts first servo motor 5, first servo motor 5 drives pivot 7 and swivel mount 8 through the output shaft and rotates, swivel mount 8 drives second leading truck 13 and splint 14 vertical rotation through carousel 9 and mounting panel 10, reach the effect of simple and convenient vertical rotation regulation, the condition emergence of dead angle and the maintenance of not being convenient for appears in avoiding the maintenance process, thereby the practicality of this auxiliary assembly has been improved, make this auxiliary assembly facilitate promotion.

In conclusion, the auxiliary equipment for aircraft equipment maintenance achieves the effect of simple and convenient fixing by placing the parts to be maintained on the clamping plate 14 and then starting the electric push rod 12 to stretch, the electric push rod 12 drives the clamping plate 14 to move up and down through the second guide frame, so as to adjust the distance between the two clamping plates 14, the second servo motor 18 is started to rotate, the second servo motor 18 drives the transmission gear 19 to rotate through the output shaft, the transmission gear 19 drives the mounting plate 10 and the second guide frame 13 to rotate horizontally through the gear disc 17 and the bracket 16, the effect of simple and convenient horizontal rotation adjustment is achieved, then the first servo motor 5 is started, the first servo motor 5 drives the rotating shaft 7 and the rotating frame 8 to rotate through the output shaft, the rotating frame 8 drives the second guide frame 13 and the clamping plate 14 to rotate vertically through the rotary disc 9 and the mounting plate 10, and the effect of simple and convenient vertical rotation adjustment is achieved, the condition that avoids appearing the dead angle in the maintenance process and be not convenient for the maintenance takes place to improve this auxiliary assembly's practicality, makeed this auxiliary assembly facilitate promotion, solved traditional aviation maintenance auxiliary device and generally be fixed structure, be not convenient for adjust its maintenance angle, cause the problem that the condition emergence such as maintenance inconvenience.

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. Without further limitation, an element defined by the phrase "comprising an … …" does not exclude the presence of other identical elements in a process, method, article, or apparatus that comprises the element.

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.

Claims

1. An auxiliary assembly for aircraft equipment maintenance, includes base plate (1), its characterized in that: the bottom of the base plate (1) is fixedly provided with universal wheels (2), the top of the base plate (1) is fixedly provided with a storage cabinet (3), the left side of the storage cabinet (3) is fixedly provided with a push rod (4), the top of the storage cabinet (3) is fixedly provided with a first servo motor (5), the top of the storage cabinet (3) is fixedly provided with a bearing seat (6) on the right side of the first servo motor (5), a rotating shaft (7) penetrating through and extending to the right side of the bearing seat (6) is sleeved on an output shaft of the first servo motor (5), the right side of the rotating shaft (7) is fixedly provided with a rotating frame (8), the top and the bottom of the rotating frame (8) are both fixedly provided with turntables (9), the inner wall of the turntables (9) is fixedly provided with a mounting plate (10), and the opposite sides of the mounting plate (10) are both fixedly provided with first guide, electric push rods (12) are fixedly arranged on the opposite sides of the first guide frame (11), the opposite sides of the electric push rods (12) are fixedly provided with second guide frames (13) which penetrate through and extend to the opposite sides of the mounting plate (10), clamping plates (14) are fixedly arranged on the opposite sides of the second guide frame (13), a balancing weight (15) is fixedly arranged on the left side of the rotating frame (8) and above the rotating shaft (7), a bracket (16) is fixedly arranged at the bottom of the mounting plate (10) and below the rotating frame (8), a gear disc (17) is sleeved on the outer wall of the support (16), a second servo motor (18) is fixedly arranged on the left side of the rotating frame (8) and below the rotating shaft (7), and a transmission gear (19) meshed with the gear disc (17) is sleeved on an output shaft of the second servo motor (18).

2. An auxiliary device for aircraft equipment maintenance according to claim 1, wherein: the number of universal wheels (2) is four, four the universal wheels (2) are distributed in a rectangular array at the bottom of the base plate (1), and brake valves are movably mounted inside the universal wheels (2).

3. An auxiliary device for aircraft equipment maintenance according to claim 1, wherein: the inner wall fixed mounting of cabinet (3) has the baffle, the outer wall of push rod (4) has cup jointed and has increased the resistance rubber sleeve, it is nitrile rubber to increase the resistance rubber sleeve.

4. An auxiliary device for aircraft equipment maintenance according to claim 1, wherein: the top of cabinet (3) just is located the equal fixed mounting in front and the back of first servo motor (5) and has first fixed block, the left side of swivel mount (8) just is located the equal fixed mounting in front and the back of second servo motor (18) and has the second fixed block.

5. An auxiliary device for aircraft equipment maintenance according to claim 1, wherein: the number of the bearing seats (6) and the number of the turntables (9) are two, and the turntables (9) are distributed on the opposite sides of the rotating frame (8) by taking the rotating shaft (7) as a symmetrical shaft.

6. An auxiliary device for aircraft equipment maintenance according to claim 1, wherein: the opposite sides of the clamping plate (14) are fixedly provided with backing plates, and the opposite sides of the backing plates are provided with anti-skidding grooves.