Multifunctional repairing hammer for aircraft

Abstract

The utility model provides a multifunctional repair hammer for an aircraft. The multifunctional repair hammer comprises a grip, a hammer handle, a hammer head, an adjusting shaft and a conversion sleeve, the hammer handle comprises a handle body and a butt joint, the handle body is connected with a grip, the butt joint is rotationally connected with a hammer head, a through hole is formed in the butt joint, a limiting groove is formed in the through hole, the butt joint is further provided with a rotating space for containing the hammer head, and a positioning groove is formed in the side, close to the rotating space, of the butt joint; an adjusting shaft is arranged between the butt joint and the hammer head; the hammerhead comprises a connecting part used for being connected with the butt joint, a first hammerhead end and a second hammerhead end are arranged at the two ends of the connecting part respectively, a shaft hole is formed in the connecting part, a plurality of clamping grooves are formed around the shaft hole, and a positioning protruding block is arranged between every two adjacent clamping grooves. The types of hammers needing to be carried are reduced, and some pits in complex positions can be repaired.

Description

Technical Field

[0001] The utility model relates to the technical field of aircraft repair, in particular to a multifunctional repair hammer for aircraft. Background Art

[0002] During use, aircraft are prone to dents and bending deformations on their external surfaces and some internal components. These damages will affect the aerodynamic performance of the aircraft, as well as the service life of the internal components and thus the structural performance of the aircraft. Currently, dents and deformations are usually treated by continuously knocking on the dents with a repair hammer to restore them to their original state. This can restore the aircraft to operation in the fastest way and reduce the losses caused by outages. However, the repair hammers currently used have the following problems: hammers made of metal are prone to excessive knocking during use; the hammer head cannot rotate, resulting in dents in some positions that cannot be repaired, and other tools need to be used for processing; the hammer head has a single shape, and multiple hammers of different shapes need to be carried for repair; the internal structure of the aircraft is complex and there are many components. Some dents cannot be repaired by maintenance personnel, and they often need to disassemble the components for repair, which has low repair efficiency and high labor costs; therefore, a multi-functional repair hammer for aircraft is needed. Utility Model Content

[0003] The utility model provides a multifunctional repair hammer for aircraft, which can effectively solve the above problems.

[0004] The utility model is achieved in this way:

[0005] The utility model provides a multifunctional repair hammer for aircraft, comprising: a grip, a hammer handle, a hammer head, an adjustment shaft and a conversion sleeve; the hammer handle comprises a handle body and a docking joint, the handle body is connected to the grip, the docking joint is rotatably connected to the hammer head, the docking joint is provided with a through hole, the docking joint is also provided with a rotation space for placing the hammer head, and the docking joint is provided with a positioning groove on a side close to the rotation space; an adjustment shaft is provided between the docking joint and the hammer head; the hammer head comprises a connecting portion for connecting with the docking joint, a first hammer head end and a second hammer head end are respectively provided at both ends of the connecting portion, an axial hole is opened in the connecting portion, a plurality of clamping grooves are provided around the axial hole, and a positioning protrusion is provided between two adjacent clamping grooves.

[0006] As a further improvement, the handle is provided with a plurality of grooves on the outer side wall, and a button is provided on one of the side walls.

[0007] As a further improvement, the handle body is provided with a plurality of adjustment holes in the vertical direction at positions corresponding to the buttons, and a limiting groove is provided inside the through hole.

[0008] As a further improvement, the first hammer head end is provided with a stepped groove.

[0009] As a further improvement, the adjusting shaft is provided with a translation shaft, both ends of the translation shaft are provided with a pushing part.

[0010] As a further improvement, the adjusting shaft is provided with a limiting plate at one end close to the translation shaft, and the adjusting shaft is provided with a clamping block matched with the clamping groove.

[0011] As a further improvement, the hammer head is connected with a conversion sleeve on one side of the second hammer head end.

[0012] As a further improvement, the conversion sleeve extends outwardly on one side away from the hammer handle and has a hitting part.

[0013] The beneficial effects of the present application are:

[0014] The present application has the beneficial effects that: the hammer head and the hammer handle are rotationally connected, so that the repair hammer can adjust the angle of the hammer head according to the position to be repaired, the repair personnel can repair some pits with peculiar repair angles, the service life of the aviation components can be effectively improved, the length of the hammer handle and the handle can be adjusted, which is beneficial for the repair personnel to operate in narrow spaces, the positioning protrusion is arranged on the hammer head, so that the hammer head can rotate within a specific angle, the clamping groove is arranged on the hammer head and the clamping block is arranged on the adjusting shaft, so that the position of the hammer head can be fixed, the angle of the hammer head can be quickly adjusted by pushing the adjusting shaft, the conversion sleeve head is arranged, so that the repair hammer can repair components with different shapes, the number of types of hammers to be carried is reduced, the hammers are made of nylon, hard rubber and other materials, and additional damage to the components during the repair process can be effectively avoided. BRIEF DESCRIPTION OF DRAWINGS

[0015] In order to more clearly illustrate the technical scheme of the embodiments of the present application, the following will briefly introduce the drawings needed to be used in the embodiments, and it should be understood that the following drawings only show some embodiments of the present application, and should not be regarded as a limitation to the scope, and for those skilled in the art, other related drawings can also be obtained without creative labor on the basis of these drawings.

[0016] Figure 1 is an embodiment one structure schematic view of a multifunctional repair hammer for an aircraft of the present application.

[0017] Figure 2 is an embodiment one structure main view schematic view of a multifunctional repair hammer for an aircraft of the present application.

[0018] Figure 3This is a structural schematic diagram of a second embodiment of the utility model, a multifunctional repair hammer for aircraft.

[0019] Figure 4 The utility model is a schematic diagram of the main structure of a second embodiment of a multifunctional repair hammer for aircraft.

[0020] Figure 5 The utility model is a schematic diagram of the hammer handle structure of a multifunctional repair hammer for aircraft.

[0021] Figure 6 The utility model is a schematic diagram of the structure of the hammer handle A of a multifunctional repair hammer for aircraft.

[0022] Figure 7 The utility model is a schematic diagram of the hammer head structure of a multifunctional repair hammer for aircraft.

[0023] Figure 8 The utility model is a schematic diagram of the main view of the hammer head structure of a multifunctional repair hammer for aircraft.

[0024] Figure 9 The utility model is a schematic diagram of the structure of an adjusting shaft of a multifunctional repair hammer for aircraft.

[0025] In the figure: 1-handle, 11-groove, 12-button, 2-hammer handle, 21-handle body, 211-adjusting hole, 22-butt joint, 221-through hole, 222-limiting groove, 223-positioning groove, 224-rotation space, 3-hammer head, 31-first hammer head end, 311-step groove, 32-second hammer head end, 33-connecting part, 331-axis hole, 332-positioning protrusion, 333-card slot, 4-adjusting shaft, 41-pushing part, 42-translation axis, 43-card block, 44-limiting plate, 5-conversion sleeve. DETAILED DESCRIPTION

[0026] In order to make the purpose, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments are part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments in the present invention, all other embodiments obtained by ordinary technicians in this field without making creative work are within the scope of protection of the present invention. Therefore, the following detailed description of the embodiments of the present invention provided in the drawings is not intended to limit the scope of the utility model for which protection is sought, but merely represents the selected embodiments of the present invention. Based on the embodiments in the present invention, all other embodiments obtained by ordinary technicians in this field without making creative work are within the scope of protection of the present invention.

[0027] In the description of this utility model, the terms "first" and "second" are used for descriptive purposes only and should not be understood to indicate or imply relative importance or implicitly specify the number of the technical features indicated. Therefore, a feature specified as "first" or "second" may explicitly or implicitly include one or more of such features. In the description of this utility model, "plurality" means two or more, unless otherwise specifically specified.

[0028] Reference Figure 1-9 As shown, a multifunctional repair hammer for aircraft includes: a grip 1, a hammer handle 2, a hammer head 3, an adjustment shaft 4 and a conversion sleeve 5;

[0029] The hammer handle 2 is sleeved in the grip 1, and the hammer handle 2 includes a handle body 21 and a docking joint 22. The handle body 21 is connected to the grip 1 at one end away from the docking joint 22. The docking joint 22 is provided with a rotation space 224, and the rotation space 224 is used to place the hammer head 3. An adjusting shaft 4 is provided between the hammer handle 2 and the hammer head 3, so that the hammer head 3 is rotatably connected to the hammer handle 2. The hammer head 3 includes a first hammer head end 31, a second hammer head end 32 and a connecting portion 33. The first hammer head end 31 is connected to a conversion sleeve 5. The utility model changes the angle between the hammer head 3 and the hammer handle 2 through the adjusting shaft 4, so that the repair hammer can repair pits in special positions. The repair hammer is made of nylon, hard rubber and other materials, which can effectively protect the parts to be repaired from additional damage.

[0030] Furthermore, the handle 1 is provided with a plurality of grooves 11 on the outer side wall. The grooves 11 are convenient for human hand holding to prevent the repair hammer from slipping out of the hand and causing damage to the aircraft. A button 12 is provided on one of the side walls of the handle 1; the handle body 21 is provided with a plurality of adjustment holes 211 in the vertical direction at the position corresponding to the button 12. The length of the repair hammer can be adjusted by cooperating with the button 12 and the adjustment hole 211. When the button 12 is pressed, the ejector pin in the button 12 is disengaged from the adjustment hole 211, so that the handle 1 and the hammer handle 2 are in an active state. When the button 12 is released, the ejector pin extends out and is stuck in the adjustment hole 211, fixing the position of the hammer handle 2 so that the length of the repair hammer can be adjusted.

[0031] Furthermore, the butt joint 22 is provided with a rotation space 224 for placing the hammer head 3, and the butt joint 22 is provided with a through hole 221, the through hole 221 is used for the adjustment shaft 4 to pass through, and a limiting groove 222 is provided inside the through hole 221. The limiting groove 222 is used to prevent the adjustment shaft 4 from rotating when the adjustment shaft 4 is pushed, so that the hammer head 3 cannot be stuck. The butt joint 22 is provided with a positioning groove 223 on the side close to the rotation space 224. The hammer head 3 includes: a first hammer head end 31, a second hammer head end 32 and a connecting The connecting portion 33 has a first hammer head end 31 and a second hammer head end 32 at both ends thereof. The first hammer head end 32 is provided with a stepped groove 311, so that the repair hammer can repair parts with a stepped shape. At the same time, the stepped groove 311 can be used to detect some parts that need to be kept vertical. The second hammer head end 32 is connected to the conversion sleeve 5, and the connection method can be a threaded connection or a clamping connection. The conversion sleeve 5 has a striking portion extending outward on the side away from the hammer handle 2. The shape of the striking portion depends on the shape of the part to be repaired.

[0032] Furthermore, the connecting portion 33 is provided with an axial hole 331, which is used for the passage of the adjusting shaft 4 to connect the hammer handle 2 and the hammer head 3. A number of slots 333 are evenly arranged around the axial hole 331, and a positioning protrusion 332 is provided between two adjacent slots 333. The positioning protrusion 332 is adapted to the positioning slot 223; the adjusting shaft 4 is provided with a translation shaft 42, which passes through the through hole 221 and the axial hole 331. Both ends of the translation shaft 42 are provided with a pushing portion 41, and a limit plate 44 is provided at one end close to the translation shaft 42. The position of the limit plate 44 is adapted to the limit slot 222 to prevent rotation when the adjusting shaft 4 is pushed. The adjusting shaft 4 is provided with a block 43 adapted to the slot 333. The length of the block 43 is defined as A, and the length of the adjusting shaft 4 is defined as B, then A<1 / 2B.

[0033] Furthermore, the specific implementation of the present invention is as follows:

[0034] Press the button 12 to adjust the connection position of the hammer handle 2 and the grip 1, and then adjust the length of the repair hammer, which is convenient for the repair hammer to perform repair operations in a narrow space; push the adjusting shaft 4 to disengage the block 43 on the adjusting shaft 4 from the connection with the slot 333, and keep the adjusting shaft 4 moving smoothly through the limit plate 44 to prevent rotation. The rotating hammer head 3 cooperates with the positioning groove 223 and the positioning protrusion 332 to make the hammer head 3 rotate to a specific angle, and temporarily fix the position of the hammer head 3. The positions of the slot 333 and the block 43 after rotation correspond to each other. Then push the adjusting shaft 4 to make the block 43 contact with the slot 333 to fix the position of the hammer head 3; connect the conversion sleeve 5 at the second hammer head end 32, and the conversion sleeve 5 allows the repair hammer to be used on parts with special shapes.

[0035] The above description is merely a preferred embodiment of the present invention and is not intended to limit the present invention. Those skilled in the art will readily appreciate that the present invention is susceptible to various modifications and variations. Any modifications, equivalent substitutions, or improvements made within the spirit and principles of the present invention shall be included within the scope of protection of the present invention.

Claims

1. A multifunctional repair hammer for aircraft, characterized in that: include: A handle (1), a hammer handle (2), a hammer head (3), an adjustment shaft (4) and a conversion sleeve (5); The hammer handle (2) comprises a handle body (21) and a docking joint (22), wherein the handle body (21) is connected to a grip (1), and the docking joint (22) is rotatably connected to the hammer head (3), the docking joint (22) is provided with a through hole (221), and the docking joint (22) is also provided with a rotation space (224) for the hammer head (3) to be placed, and the docking joint (22) is provided with a positioning groove (223) on a side close to the rotation space (224); an adjusting shaft (4) is provided between the docking joint (22) and the hammer head (3); The hammer head (3) comprises a connecting portion (33) for connecting to the docking head (22), a first hammer head end (31) and a second hammer head end (32) are respectively provided at both ends of the connecting portion (33), an axial hole (331) is formed in the connecting portion (33), a plurality of slots (333) are provided around the axial hole (331), and a positioning protrusion (332) is provided between two adjacent slots (333).

2. The multifunctional repair hammer for aircraft according to claim 1, characterized in that: The handle (1) is provided with a plurality of grooves (11) on an outer side wall, and a button (12) is provided on one side wall.

3. The multifunctional repair hammer for aircraft according to claim 2, characterized in that: The handle (21) is provided with a plurality of adjustment holes (211) in a vertical direction at positions corresponding to the buttons (12), and a limiting groove (222) is provided inside the through hole (221).

4. The multifunctional repair hammer for aircraft according to claim 1, characterized in that: The first hammer head end (31) is provided with a stepped groove (311).

5. The multifunctional repair hammer for aircraft according to claim 1, characterized in that: The adjustment shaft (4) is provided with a translation shaft (42), and both ends of the translation shaft (42) are provided with a pushing portion (41).

6. The multifunctional repair hammer for aircraft according to claim 5, characterized in that: The adjusting shaft (4) is provided with a limiting plate (44) at one end close to the translation shaft (42), and the adjusting shaft (4) is provided with a clamping block (43) adapted to the clamping slot (333).

7. The multifunctional repair hammer for aircraft according to claim 1, characterized in that: The hammer head (3) is connected to a conversion sleeve (5) on one side of the second hammer head end (32).

8. The multifunctional repair hammer for aircraft according to claim 7, characterized in that: The conversion sleeve (5) has a striking portion extending outwardly on a side away from the hammer handle (2).

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