A method for imitating hole processing of aircraft tie rod

Abstract

The invention relates to the field of aviation repair and production technology, and specifically to a method for processing an imitation hole of an aircraft tie rod, comprising an adapter, type I bolts, an inner sleeve, type II bolts and an outer sleeve, disassembling the bolts to make a conversion piece, measuring the hole position of the connection hole and making a process hole at the marked position, fixing the conversion piece on the adapter so that the connection hole on the adapter can be observed through the process hole, processing the imitation hole on the other side of the process hole on the conversion piece, matching the conversion piece with the outer circle of the inner sleeve, sleeved on a new inner sleeve, using the imitation hole on the conversion piece to process the imitation hole of a new inner sleeve, processing the hole on the other side of the new inner sleeve, so that the hole of the imitated new inner sleeve can be made consistent with that of the old piece. Compared with the prior art, the invention uses the guiding effect of the hole of the old piece to process the hole of the new piece, thereby solving the problems of poor maintainability and poor interchangeability.

Description

Technical Field

[0001] The invention relates to the technical field of aviation repair and production, in particular to a method for imitating hole processing of an aircraft tie rod. Background Art

[0002] Due to the influence of ocean, climate and other factors, the corrosion of aircraft bodies and their components of various types of naval aircraft has become an important issue for naval combat forces and related parties. Before this issue can be well resolved, some parts affected by corrosion must be replaced during factory overhauls; on the other hand, due to long-term use, the force causes the holes to deform, the bolts to loosen, and the pull rods cannot be used normally and need to be replaced.

[0003] However, during the manufacturing process of the pull rod, the maintainability of the part was not taken into consideration. During processing, the two parts were matched and then holes were made. The maintainability and interchangeability were extremely poor, and many holes of the parts that were connected and matched with each other had problems such as slanted holes. When the old holes were on the inside of the new parts, it was an unconventional hole matching. Mainly because of the obstruction of the new parts, the relative position of the holes in the old parts could not be seen, which caused great difficulties in the imitation hole processing and the cost of replacing the entire part was relatively high.

[0004] This method uses simple principles to perform hole-simulating machining.

[0005] Therefore, it is necessary to design a method for imitation hole processing of aircraft tie rods to solve the problem of poor subsequent maintainability and interchangeability caused by the original drilling in the production and manufacturing process. It can solve the problem of replacing various types of sleeve parts and realize the role of changing the replacement of a whole set into the replacement of a single part. Summary of the invention

[0006] The purpose of the present invention is to provide a method for imitation hole processing of aircraft tie rods to solve the problems raised in the above background technology.

[0007] To achieve the above object, the present invention provides the following technical solution: a method for imitation hole processing of an aircraft tie rod, comprising the following steps:

[0008] It includes an adapter, a type I bolt, an inner sleeve, a type II bolt, and an outer sleeve, and includes the following steps:

[0009] S1: Remove type I bolts and type II bolts;

[0010] S2: Make a conversion piece, the inner hole of the conversion piece matches the adapter, and the outer circle of the conversion piece is larger than the outer circle of the inner sleeve;

[0011] S3: Measure the position of the connection hole, mark it on the conversion part, and make process holes at the marked position;

[0012] S4: The conversion piece is fixedly mounted on the adapter so that the connection hole on the adapter can be observed through the process hole;

[0013] S5: Use the connection hole on the adapter to guide the imitation hole on the other side of the process hole on the conversion part;

[0014] S6: Match the inner hole of the conversion piece with the outer circle of the new inner sleeve to be replaced, and fix the conversion piece on the new inner sleeve;

[0015] S7: using the imitation hole on the conversion part to process the imitation hole of the new inner sleeve;

[0016] S8: Fix the new inner sleeve onto the adapter;

[0017] S9: By using the imitation hole of the new inner sleeve and the guiding function of the connecting hole on the adapter, the hole on the other side of the new inner sleeve is processed, so that the hole of the imitation new inner sleeve can be consistent with the old one.

[0018] In S2, the outer circle of the conversion piece is 10 mm larger than the outer circle of the inner sleeve.

[0019] The process hole in S3 is a single-side hole, which is 2mm larger than the original connection hole.

[0020] The new internal sleeve in S7 has a single-sided hole.

[0021] The connection hole positions in S3 can be multiple hole positions.

[0022] Compared with the prior art, the present invention utilizes the principle that the existing hole has a guiding effect on the drill bit, fully utilizes the guiding effect of the hole of the old part, and processes the hole of the new part so that the position of the hole of the new part can effectively match the old part, thereby solving the problems of poor maintainability and poor interchangeability; similarly, a conversion part similar to the new part is made with a hole one level larger on one side of the part, so that the hole on the matching part can be seen, and then the hole on the new part is reversely processed to ensure that the hole of the new part is consistent with the hole of the old part. BRIEF DESCRIPTION OF THE DRAWINGS

[0023] Figure 1 It is a schematic diagram of the conversion part and processing of the present invention;

[0024] Description of reference numerals:

[0025] 1 is an adapter, 2 is a type I bolt, 3 is an inner sleeve, 4 is a type II bolt, and 5 is an outer sleeve. DETAILED DESCRIPTION

[0026] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.

[0027] See also Figure 1 The present invention provides a technical solution: a method for imitation hole processing of an aircraft tie rod, comprising the following steps:

[0028] The method comprises an adapter 1, a type I bolt 2, an inner sleeve 3, a type II bolt 4, and an outer sleeve 5, and includes the following steps:

[0029] S1: Remove type I bolt 1 and type II bolt 2;

[0030] S2: making a conversion piece, the inner hole of the conversion piece matches the adapter 1, and the outer circle of the conversion piece is larger than the outer circle of the inner sleeve 3;

[0031] S3: Measure the position of the connection hole, mark it on the conversion part, and make process holes at the marked position;

[0032] S4: The conversion piece is fixedly sleeved on the adapter 1 so that the connection hole on the adapter 1 can be observed through the process hole;

[0033] S5: using the connection hole on the adapter 1 to guide the imitation hole on the other side of the process hole on the processing conversion part;

[0034] S6: Match the inner hole of the conversion piece with the outer circle of the new inner sleeve 3 to be replaced, and fix the conversion piece on the new inner sleeve 3;

[0035] S7: using the imitation hole on the conversion piece to process the imitation hole of the new inner sleeve 3;

[0036] S8: Fix the new inner sleeve 3 onto the adapter 1;

[0037] S9: Using the imitation hole of the new inner sleeve 3 and the guiding function of the connecting hole on the adapter 1, the hole on the other side of the new inner sleeve 3 is processed, so that the hole of the imitation new inner sleeve 3 can be consistent with the old one.

[0038] The outer circle of the conversion piece in S2 is 10 mm larger than the outer circle of the inner sleeve 3.

[0039] The process hole in S3 is a single-side hole, which is 2mm larger than the original connection hole.

[0040] The imitation hole of the new inner sleeve 3 in S7 is a single-side hole.

[0041] The connection hole positions in S3 can be multiple hole positions.

[0042] Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.

[0043] The present invention solves the problem of poor subsequent maintainability and interchangeability caused by the punching in the original production process and the replacement problem of various shaft sleeve parts as a whole. It does not require complex precision measurement, is simple to process, is low in cost, and has great market application prospects.

Claims

1. A method for imitation hole processing of aircraft tie rods, characterized in that: The method comprises an adapter (1), a type I bolt (2), an inner sleeve (3), a type II bolt (4), and an outer sleeve (5), and includes the following steps: S1: Remove the type I bolts (2) and type II bolts (4); S2: manufacturing a conversion piece, wherein the inner hole of the conversion piece matches the adapter (1), and the outer circle of the conversion piece is larger than the outer circle of the inner sleeve (3); S3: Measure the position of the connection hole, mark it on the conversion part, and make process holes at the marked position; S4: The conversion piece is fixedly mounted on the adapter (1) so that the connection hole on the adapter (1) can be observed through the process hole; S5: using the connection hole on the adapter (1) to guide the imitation hole on the other side of the process hole on the processing conversion part; S6: Matching the inner hole of the conversion piece with the outer circle of the new inner sleeve (3) to be replaced, and fixing the conversion piece on the new inner sleeve (3); S7: using the imitation hole on the conversion piece to machine an imitation hole of a new inner sleeve (3); S8: fixing a new inner sleeve (3) on the adapter (1); S9: Using the imitation hole of the new inner sleeve (3) and the guiding function of the connecting hole on the adapter (1), the hole on the other side of the new inner sleeve (3) is processed, so that the hole of the imitation new inner sleeve (3) is consistent with the old one.

2. The method for imitating hole processing of an aircraft tie rod according to claim 1, characterized in that: The outer circle of the conversion piece in S2 is 10 mm larger than the outer circle of the inner sleeve (3).

3. The method for imitating hole processing of an aircraft tie rod according to claim 1, characterized in that: The process hole in S3 is a single-side hole, which is 2 mm larger than the original connection hole.

4. The method for imitating hole processing of an aircraft tie rod according to claim 1, characterized in that: The imitation hole of the new inner sleeve (3) in S7 is a single-side hole.

5. The method for imitating hole processing of an aircraft tie rod according to claim 1, characterized in that: The connection hole positions in S3 are multiple hole positions.

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