Panel deployment apparatus and panel deployment method

A panel deployment apparatus includes a guide provided on a first hinge axis of a main hinge; a guide provided on a second hinge axis of a side hinge; and a deployment stop arm that stops deployment of a second side panel by sequential engagement with the guide and the guide, the deployment stop arm...

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Bibliographische Detailangaben
Hauptverfasser:	Hirose, Taichi, Kaneko, Naoyuki
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT AVIATION CONVERSION OR DISTRIBUTION OF ELECTRIC POWER COSMONAUTICS ELECTRICITY GENERATION GENERATION OF ELECTRIC POWER BY CONVERSION OF INFRA-REDRADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, E.G. USINGPHOTOVOLTAIC [PV] MODULES PERFORMING OPERATIONS TRANSPORTING VEHICLES OR EQUIPMENT THEREFOR
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Beschreibung
Zusammenfassung:	A panel deployment apparatus includes a guide provided on a first hinge axis of a main hinge; a guide provided on a second hinge axis of a side hinge; and a deployment stop arm that stops deployment of a second side panel by sequential engagement with the guide and the guide, the deployment stop arm being fixed to the second side panel, wherein the second main panel is deployed in a state of the deployment stop arm being engaged with the guide and, when the deployment stop arm is disengaged from the guide and then engaged with the guide, the first side panel is deployed in a state of the deployment stop arm being engaged with the guide and, when the deployment stop arm is disengaged from the guide, the second side panel is deployed.