# US 9,434,483 B2 · Assembling method of mandrel used for manufacturing composite material structure and assembling apparatus of mandrel

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- Number: US 9,434,483 B2
- Document ID: US9434483B2
- Status: Granted
- Kind: B2
- Application number: 14/704,492
- Filed: 2015-05-05
- Published: 2015-10-01
- Granted: 2016-09-06
- Earliest claimed: 2009-12-25
- Assignees: Kawasaki Jukogyo Kabushiki Kaisha
- Applicants: Kawasaki Jukogyo Kabushiki Kaisha
- Inventors: Toshikazu Sana; Naoki Tamura; Tomoya Takahashi; Toshiaki Takechi
- Web page: https://patentgrep.com/patent/US9434483B2

## CPC

- B29C 33/38: characterised by the material or the manufacturing process (B29C33/44 takes precedence)
- B29C 33/485: {cores or mandrels (collapsible mandrels for shaping tube ends B29C57/02; collapsible mandrels for winding and joining B29C53/824)}
- B64C 1/069: {Joining arrangements therefor}
- B64F 5/10: Manufacturing or assembling aircraft, e.g. jigs therefor
- B29L 2031/3082: {Fuselages}
- Y02T 50/40: Weight reduction
- Y10T 29/4978: Assisting assembly or disassembly
- Y10T 29/49828: Progressively advancing of work assembly station or assembled portion of work
- Y10T 29/53539: including work conveyor
- B29C: SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING (making preforms B29B11/00; making laminated products by combining previously unconnected layers which become one product whose layers will remain together B32B37/00 - B32B41/00)
- B64C: AEROPLANES; HELICOPTERS
- B64F: GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B29L: INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- Y02T: CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y10T: TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION

## Abstract

A technique which can assemble a mandrel having a substantially cylindrical shape and being dividable into plurality of segments, which is used for manufacturing, for example, a fuselage of an aircraft, with high position accuracy and an easy manner. In a segment fastening step, a segment which is a fastened target is fastened to a specified fastening portion which is one of a plurality of fastening portions set along a pair of support rings placed to face each other. In a rotation step, before the segment fastening step, the support rings are rotated so that the specified fastening portion is located at an uppermost portion of the support rings. In the segment fastening step, the segment which is the fastened target is placed between the support rings and lifted vertically up to a height corresponding to the specified fastening portion and then fastened to the support rings.

## Claims

### Claim 1

An assembling apparatus of a mandrel for use in assembling of a tubular mandrel by joining a plurality of segments together, the mandrel being supported by a pair of support rings facing each other, the segments having a substantially rectangular shape and being parts into which the mandrel is divided along a center axis direction, in which
a plurality of fastening portions of the segments are set along a circumferential direction on each of the pair of support rings, the assembling apparatus comprising:
a rail body inserted into a hollow space of the pair of support rings;
a ring rotation drive section for rotating each of the support rings to position at an uppermost portion of each of the support rings a specified fastening portion which is one of the fastening portions set on the pair of support rings;
a horizontal movement mechanism which is provided on the rail body and configured to horizontally move the segment from a rear end of the rail body toward a tip end of the rail body; and
a vertical movement mechanism which is provided on the rail body and configured to lift up the segment moved from the horizontal movement mechanism to a height position corresponding to the specified fastening portion along the vertical direction, to fasten the segment to the specified fastening portion.

### Claim 2 (depends on 1)

The assembling apparatus of the mandrel according to claim 1,
wherein the vertical movement mechanism includes segment support members which support at least portions in the vicinity of four corners of the segment having the substantially rectangular shape and displace the portions independently along the vertical direction, between the support rings, in a state in which the rail body is inserted into the hollow space of the support rings.

### Claim 3 (depends on 1)

The assembling apparatus of the mandrel according to claim 1, comprising:
a rail movement support table for supporting the rail body; and
a pair of rail support work tables for supporting the rail body, the pair of support rings being placed between the pair of rail support work tables;
wherein the rail movement support table and the rail support work tables include a movement support mechanism which supports the rail body such that the rail body is movable.

### Claim 4 (depends on 1)

The assembling apparatus of the mandrel according to claim 1,
a carriage on which the pair of support rings are placed;
wherein the pair of rail support work tables are configured such that the support rings and the carriage are placed between the pair of rail support work tables, and the rail support work tables support the support rings together with the carriage.

### Claim 5 (depends on 1)

The assembling apparatus of the mandrel according to claim 1, further comprising:
a cradle for supporting each of the support rings from below on at least two locations sandwiching a vertical line passing through a center axis of the support ring;
wherein the rail support work table supports each of the support rings on an upper portion of the rail support work table such that movement of the support ring in a direction of the center axis is restricted.

### Claim 6 (depends on 1)

The assembling apparatus of the mandrel according to claim 1,
wherein the ring rotation drive section includes a position detector section which detects that the specified fastening portion is positioned at an uppermost portion of each of the support rings.

### Claim 7 (depends on 6)

The assembling apparatus of the mandrel according to claim 6,
wherein the plurality of segments include a first segment and a second segment which are different in shape;
the plurality of fastening portions set on each of the pair of support rings include a first fastening portion to which the first segment is fastened and a second fastening portion to which the second segment is fastened;
the first fastening portion and the second fastening portion are set alternately on each of the pair of support rings along a circumferential direction the support ring; and
the position detector section detects whether or not the first fastening portion or the second fastening portion as the specified fastening portion is positioned at the uppermost portion of each the support rings, as the specified fastening portion.

### Claim 8 (depends on 1)

The assembling apparatus of the mandrel according to claim 1,
wherein the plurality of segments include a first segment and a second segment which are different in shape, and an obverse surface of the second segment, which is an outer peripheral surface of the mandrel, has a greater area than an obverse surface of the first segment, which is the outer peripheral surface of the mandrel,
after all of the second segments are fastened to each of the support rings in every two locations along the circumferential direction; the first segment is lifted up to a location between two second segments, is fitted and fastened to the second segments.
