SAE AIR6016 High Lift Systems Description
作者:标准资料网 时间:2024-05-19 04:11:18 浏览:9340
来源:标准资料网
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Product Code:SAE AIR6016
Title:High Lift Systems Description
Issuing Committee:A-6b3 Electro-Mechanical Actuation Committee
Scope: The scope of the project is to develop a comprehensive description document that displays various examples of High Lift Systems of commercial and military aircraft.The main focus is on mechanical systems which may be actuated hydraulically or electrically. The document is intended as an overview for those specifying or designing High Lift Systems in order to compare existing solutions as reference for implementation in new aircraft programs.
Rationale: The scope of the project is to develop a comprehensive description document that displays various examples of High Lift Systems of commercial and military aircraft.The main focus is on mechanical systems which may be actuated hydraulically or electrically. The document is intended as an overview for those specifying or designing High Lift Systems in order to compare existing solutions as reference for implementation in new aircraft programs.
Title:High Lift Systems Description
Issuing Committee:A-6b3 Electro-Mechanical Actuation Committee
Scope: The scope of the project is to develop a comprehensive description document that displays various examples of High Lift Systems of commercial and military aircraft.The main focus is on mechanical systems which may be actuated hydraulically or electrically. The document is intended as an overview for those specifying or designing High Lift Systems in order to compare existing solutions as reference for implementation in new aircraft programs.
Rationale: The scope of the project is to develop a comprehensive description document that displays various examples of High Lift Systems of commercial and military aircraft.The main focus is on mechanical systems which may be actuated hydraulically or electrically. The document is intended as an overview for those specifying or designing High Lift Systems in order to compare existing solutions as reference for implementation in new aircraft programs.
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