发明名称 |
Alignment defect compensating method for airplane, involves determining gaps i.e. positioning errors, between theoretical sight line of equipment and aircraft sight line, and carrying out correction operation to eliminate errors |
摘要 |
<p>The method involves choosing a direction i.e. aircraft sight line, fixed with respect to a structure of an aircraft i.e. airplane, and a structural element e.g. chair, fixed with respect to the structure of the aircraft. Angular gaps i.e. positioning errors, between a theoretical sight line (12) of corresponding equipment e.g. head-up display device (5), and the aircraft sight line are determined for equipment supports e.g. head-up display support. A correction operation is carried out using the positioning errors to eliminate the positioning errors.</p> |
申请公布号 |
FR2930933(A1) |
申请公布日期 |
2009.11.13 |
申请号 |
FR20080002497 |
申请日期 |
2008.05.06 |
申请人 |
AIRBUS FRANCE SOCIETE PAR ACTIONS SIMPLIFIEE |
发明人 |
POUSSIN SANDRA;BIDEAU DAVID;COLOMA LAURENT;GAUTHIER STEPHANE |
分类号 |
B64F5/00;G01B11/26;G02B27/01 |
主分类号 |
B64F5/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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