JP6714329B2 - 胴体を製作するための自律的なフレキシブル製造システム - Google Patents
胴体を製作するための自律的なフレキシブル製造システム Download PDFInfo
- Publication number
- JP6714329B2 JP6714329B2 JP2015119176A JP2015119176A JP6714329B2 JP 6714329 B2 JP6714329 B2 JP 6714329B2 JP 2015119176 A JP2015119176 A JP 2015119176A JP 2015119176 A JP2015119176 A JP 2015119176A JP 6714329 B2 JP6714329 B2 JP 6714329B2
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- assembly
- fixture
- tower
- panel
- panels
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- 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
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
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- G—PHYSICS
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- B21J15/00—Riveting
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- B21J15/28—Control devices specially adapted to riveting machines not restricted to one of the preceding subgroups
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- B21J15/00—Riveting
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- B21J15/40—Accessories for use in connection with riveting, e.g. pliers for upsetting; Hand tools for riveting for forming rivet heads
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Description
A1.航空機の胴体アセンブリを製作する方法であって、組み立てフィクスチャを形成するために、フロアを横切って組み立て領域へいくつかのフィクスチャを駆動するステップと、組み立てフィクスチャ上で胴体アセンブリを製作するステップとを含む方法。
B1.駆動可能なタワーと、前記駆動可能なタワーに自律的に接続可能な、いくつかの駆動可能なフィクスチャとを備える、フレキシブル製造システム。
C1.いくつかの駆動可能なクレードルフィクスチャで構成された組み立てフィクスチャと、前記組み立てフィクスチャ上で複数のパネルを互いに接合する、自律的なパネル接合システムとを備える、フレキシブル製造システム。
D1.分散ユーティリティネットワークを確立する方法であって、ユーティリティフィクスチャに対して、選択されたタワー位置へと、フロアを横切ってタワーを駆動するステップと、前記分散ユーティリティネットワークを確立するために、前記タワーと前記ユーティリティフィクスチャとの間にいくつかのユーティリティを接続するステップとを含む方法。
E1.組み立て領域に固定に関連付けられたユーティリティフィクスチャと、いくつかのユーティリティが、前記ユーティリティフィクスチャから前記駆動可能な移動システムまで分配されるように、前記ユーティリティフィクスチャに接続された駆動可能な移動システムとを備える、分散ユーティリティネットワーク。
F1.ユーティリティフィクスチャと、前記ユーティリティフィクスチャに自律的に接続可能な駆動可能なタワーと、前記タワーに直列に、自律的に接続可能ないくつかの駆動可能なクレードルフィクスチャとを備える、フレキシブル製造システム。
G1.胴体アセンブリを製作する方法であって、ユーティリティフィクスチャに対して、選択されたタワー位置にタワーを自律的に駆動するステップと、いくつかのユーティリティを、前記ユーティリティフィクスチャから前記タワーへと流すことを可能にするために、前記タワーを前記ユーティリティフィクスチャに自律的に接続するステップと、組み立てフィクスチャを製作するために、いくつかのクレードルフィクスチャを、前記タワーに対して、いくつかの選択されたクレードル位置へと自律的に駆動するステップと、前記いくつかのユーティリティを、前記タワーから前記いくつかのクレードルフィクスチャの各々へと下流に流すことを可能にするために、前記いくつかのクレードルフィクスチャを前記タワーに直列に、自律的に接続するステップと、前記胴体アセンブリの複数のパネルを、前記組み立てフィクスチャに係合させるステップと、前記複数のパネルを互いに対して動かぬように保持するために、前記複数のパネルを互いに一時的に接続するステップと、前記胴体アセンブリが前記組み立てフィクスチャによって支持されている間に、自律的なツールシステムを使用して前記胴体アセンブリを製作するために、前記複数のパネルを互いに接合するステップとを含む方法。
601 保持環境
602 組み立て環境
603 フロア
608 フレキシブル製造システム
626 ユーティリティフィクスチャ
700 第1のタワー
716 自律的な車両
800 クレードルシステム
804 フィクスチャ
806,808,810 クレードルフィクスチャ
823 保持構造体
912 組み立てフィクスチャ
1000 胴体アセンブリ
1001 端部パネル
1004 キールパネル
1018 胴体部分
1102 第1の側面パネル
1104 第2の側面パネル
1302 クラウンパネル
1400 第2のタワー
1408 内部移動プラットフォーム
1410 内部ロボット装置
1505 外部移動プラットフォーム
1506 外部ロボット装置
1510 エンドエフェクタ
1511 自律的な車両
Claims (37)
- 航空機(104)の胴体アセンブリ(114)を製作する方法であって、
インターフェースをタワー(332)とユーティリティフィクスチャ(150)との間に形成するために、組み立て領域(304)に位置するユーティリティフィクスチャ(150)に対して、タワー(332)を選択されたタワー位置(338)へ自律的に駆動するステップと、
組み立てフィクスチャ(324)を形成するために、フロア(130)を横切って組み立て領域(304)へいくつかのフィクスチャ(313)を駆動するステップと、
前記組み立てフィクスチャ(324)上で前記胴体アセンブリ(114)を製作するステップと
を含む方法。 - 前記胴体アセンブリ(114)を製作する方法は、
複数の移動プラットフォーム(344)を使用して、前記組み立てフィクスチャ(324)上で前記胴体アセンブリ(114)を製作するステップを含む、請求項1に記載の方法。 - 分散ユーティリティネットワーク(144)を介して、いくつかのユーティリティ(146)を前記複数の移動プラットフォーム(344)に分配するステップを更に含む、請求項2に記載の方法。
- 前記いくつかのフィクスチャ(313)を駆動するステップは、
前記組み立てフィクスチャ(324)を形成するために、いくつかの選択されたクレードル位置(320)へいくつかのクレードルフィクスチャ(314)を駆動するステップを含む、請求項1に記載の方法。 - 前記いくつかのクレードルフィクスチャ(314)を駆動するステップは、
前記組み立てフィクスチャ(324)を形成するために、前記いくつかの選択されたクレードル位置(320)へ前記いくつかのクレードルフィクスチャ(314)を自律的に駆動するステップを含む、請求項4に記載の方法。 - 前記いくつかのフィクスチャ(313)を駆動するステップは、
前記組み立てフィクスチャ(324)を形成するために、いくつかのクレードルフィクスチャ(314)を、前記タワー(332)に対して、いくつかの選択されたクレードル位置(320)へ駆動するステップを含む、請求項1に記載の方法。 - 前記タワー(332)とユーティリティフィクスチャ(150)との間にいくつかのユーティリティ(146)を接続するステップを更に含む、請求項6に記載の方法。
- 前記タワー(332)と前記ユーティリティフィクスチャ(150)との間に前記いくつかのユーティリティ(146)を接続するステップは、
前記ユーティリティフィクスチャ(150)から前記タワー(332)への前記いくつかのユーティリティ(146)の流れを可能にするために、前記タワー(332)を前記ユーティリティフィクスチャ(150)に自律的に接続するステップを含む、請求項7に記載の方法。 - 前記胴体アセンブリ(114)を製作するステップは、
前記胴体アセンブリ(114)の複数の胴体部分(205)を前記組み立てフィクスチャ(324)に係合させるステップを含む、請求項1に記載の方法。 - 前記複数の胴体部分(205)を係合させるステップは、
複数のパネル(120)を前記組み立てフィクスチャ(324)に係合させるステップを含む、請求項9に記載の方法。 - 前記複数のパネル(120)を前記組み立てフィクスチャ(324)に係合させるステップは、
前記複数のパネル(120)におけるキールパネル(222)を前記組み立てフィクスチャ(324)に係合させるステップと、
前記複数のパネル(120)における側面パネル(220)を前記キールパネル(222)に係合させるステップと、
前記複数のパネル(120)におけるクラウンパネル(218)を前記側面パネル(220)に係合させるステップとを含む、請求項10に記載の方法。 - 前記複数のパネル(120)を前記組み立てフィクスチャ(324)に係合させるステップは、
端部パネル(228)を、前記組み立てフィクスチャ(324)及び前記キールパネル(222)、前記側面パネル(220)、又は前記クラウンパネル(218)のうちの少なくとも1つに係合させるステップであって、前記端部パネル(228)が、円すい形のパネル、円筒形のパネル、及びテーパ状の円筒形のパネルのうちの1つから選択される、端部パネルを係合させるステップを更に含む、請求項11に記載の方法。 - 前記複数のパネル(120)における前記キールパネル(222)を前記組み立てフィクスチャ(324)に係合させるステップは、
前記キールパネル(222)をいくつかの保持構造体(326)に係合させるステップを含む、請求項11に記載の方法。 - 前記胴体アセンブリ(114)を製作するステップは、
前記複数のパネル(120)を互いに一時的に接続するステップを更に含む、請求項10に記載の方法。 - 前記複数のパネル(120)を一時的に接続するステップは、前記複数のパネル(120)を互いに一時的な締め具(328)で留めるステップを含む、請求項14に記載の方法。
- 前記胴体アセンブリ(114)を製作するステップは、
前記複数のパネル(120)が前記組み立てフィクスチャ(324)に支持されている間に、前記複数のパネル(120)を互いに接合するステップを更に含む、請求項10に記載の方法。 - 前記複数のパネル(120)を互いに接合するステップは、
第1のパネルを第2のパネルに直接固定すること、前記第1のパネルに関連付けられた第1の部材を前記第2のパネルに関連付けられた第2の部材に接合すること、前記第1のパネルに関連付けられた部材を前記第2のパネルに直接接合すること、前記第1のパネル及び前記第2のパネルの両方に関連付けられた1つの部材を別の部材に接合すること、又は選択された部材を前記第1のパネル及び前記第2のパネルの両方に接合することのうちの少なくとも1つによって、第1のパネルと第2のパネルとを互いに接合するステップを含む、請求項16に記載の方法。 - 前記複数のパネル(120)を互いに接合するステップは、
前記複数のパネル(120)を互いに接合するために、複数の締め具(264)を実質的に自律的に据え付けるステップを含む、請求項17に記載の方法。 - 前記胴体アセンブリ(114)の製作中に、前記組み立てフィクスチャ(324)を使用して、複数のパネル(120)、及び前記胴体アセンブリ(114)の前記複数のパネル(120)に関連付けられた複数の部材(122)を支持するステップを更に含む、請求項1に記載の方法。
- 前記胴体アセンブリ(114)の前記製作中に、前記組み立てフィクスチャ(324)を使用して、前記胴体アセンブリ(114)の形状及び構成を選択された公差の範囲内に維持するステップを更に含む、請求項1に記載の方法。
- 選択された公差の範囲内で、前記胴体アセンブリ(114)の外側モールドラインの要件及び内側モールドラインの要件の順守を維持するために、前記胴体アセンブリ(114)の製作中に、前記いくつかのフィクスチャ(313)のうちの少なくとも1つを調節するステップを更に含む、請求項1に記載の方法。
- 前記胴体アセンブリ(114)を製作するステップは、
自律的なツールシステム(312)を使用して、複数のパネル(120)を互いに接合するステップを含む、請求項1に記載の方法。 - 前記胴体アセンブリ(114)を製作するステップは、
前記胴体アセンブリ(114)上の位置(426)に対して外部位置(414)へ外部移動プラットフォーム(404)を駆動するステップと、
前記胴体アセンブリ(114)上の前記位置(426)に対して内部位置(422)へ内部移動プラットフォーム(406)を駆動するステップとを含む、請求項1に記載の方法。 - 前記外部移動プラットフォーム(404)を駆動するステップは、
前記外部位置(414)へ前記外部移動プラットフォーム(404)を自律的に駆動するステップを含み、前記内部移動プラットフォーム(406)を駆動するステップは、
前記内部位置(422)へ前記内部移動プラットフォーム(406)を自律的に駆動するステップを含む、請求項23に記載の方法。 - 前記胴体アセンブリ(114)を製作するステップは、
前記内部移動プラットフォーム(406)と前記外部移動プラットフォーム(404)とを使用して、前記胴体アセンブリ(114)上の前記位置(426)において固定プロセス(424)を自律的に実行するステップを更に含む、請求項24に記載の方法。 - 前記固定プロセス(424)を実行するステップは、
前記外部移動プラットフォーム(404)又は前記内部移動プラットフォーム(406)のうちの少なくとも1つを使用して、前記位置(426)に孔(436)を自律的に穿孔するステップと、
前記外部移動プラットフォーム(404)又は前記内部移動プラットフォーム(406)のうちの少なくとも1つを使用して、前記孔(436)に締め具(438)を自律的に挿入するステップと、
前記外部移動プラットフォーム(404)又は前記内部移動プラットフォーム(406)のうちの少なくとも1つを使用して、前記締め具(438)を自律的に据え付けるステップとを含む、請求項25に記載の方法。 - 第1のタワー(334)及び第2のタワー(336)のうちの1つを使用して、前記胴体アセンブリ(114)の内部(236)にアクセスするステップを更に含む、請求項1に記載の方法。
- 前記胴体アセンブリ(114)を製作するステップは、
ロボットタワーから前記胴体アセンブリ(114)の内部(264)へいくつかの内部移動プラットフォーム(402)を自律的に駆動するステップと、
前記いくつかの内部移動プラットフォーム(402)を使用して、前記胴体アセンブリ(114)の前記内部(264)で自律的に作業(124)を実行するステップとを含む、請求項1に記載の方法。 - 前記胴体アセンブリ(114)の自律的な製作を可能にするために、ユーティリティフィクスチャ(150)、タワー(332)、組み立てフィクスチャ(324)、及びいくつかの内部移動プラットフォーム(402)又はいくつかの外部移動プラットフォーム(400)のうちの少なくとも1つの間に、分散ユーティリティネットワーク(144)を確立するステップを更に含む、請求項1に記載の方法。
- 前記胴体アセンブリ(114)を製作するステップは、
前記いくつかの内部移動プラットフォーム(402)及び前記いくつかの外部移動プラットフォーム(400)を使用して、前記胴体アセンブリ(114)を自律的に製作するステップを含む、請求項29に記載の方法。 - 航空機(104)の胴体アセンブリ(114)を製造するためのフレキシブル製造装置であって、
ユーティリティフィクスチャ(150)と、
前記ユーティリティフィクスチャ(150)に電気的及び物理的に接続可能な、自律的に駆動可能なタワー(332)と、
前記駆動可能なタワー(332)に自律的に接続可能な、いくつかの駆動可能な組み立てフィクスチャとを備える、フレキシブル製造装置。 - 自律的なツールシステム(312)を更に備える、請求項31に記載のフレキシブル製造装置。
- 前記いくつかの駆動可能な組み立てフィクスチャは、いくつかの自律的に駆動可能な組み立てフィクスチャである、請求項31に記載のフレキシブル製造装置。
- いくつかの駆動可能なクレードルフィクスチャで構成された組み立てフィクスチャ(324)と、
前記組み立てフィクスチャ(324)上で複数のパネル(120)を互いに接合する、自律的なパネル接合システムと、
電気的又は物理的の少なくとも一方にて、前記組み立てフィクスチャ(324)に接続可能な駆動可能なタワー(332)と、を備え、
前記駆動可能なタワー(332)は、自律的に駆動可能なタワー(332)であり、前記いくつかの駆動可能なクレードルフィクスチャは、いくつかの自律的に駆動可能なクレードルフィクスチャであり、
前記自律的に駆動可能なタワー(332)に、電気的及び物理的に接続可能なユーティリティフィクスチャ(150)を更に備える、フレキシブル製造システム(106)。 - 前記自律的なパネル接合システムは、
いくつかの駆動可能な外部移動プラットフォームを備え、前記いくつかの駆動可能な外部移動プラットフォームの各々は、前記組み立てフィクスチャ(324)に自律的に接続可能な、請求項34に記載のフレキシブル製造システム(106)。 - 前記駆動可能なタワー(332)を、製造環境のフロア(300)を横切って自律的に駆動させることが可能な、自律的な車両(716、1514)を更に含む、請求項34に記載のフレキシブル製造システム(106)。
- 前記いくつかの駆動可能なクレードルフィクスチャにおける駆動可能なクレードルフィクスチャは、
前記駆動可能なクレードルフィクスチャに関連付けられた、いくつかの保持構造体(326)を備える、請求項34に記載のフレキシブル製造システム(106)。
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