发明名称 REIBUNGSFREIES SELBSTANGETRIEBENES GELENK UND EINE GELENKIGE EINHEIT, BEISPIELSWEISE EIN SATELLITENSOLARPANEEL, DAS MIT SOLCHEN GELENKEN VERSEHEN IST.
摘要 In order to connect two adjacent elements (E1,E2) joined, for example, onto a satellite solar panel, an antifriction joint (10) is used. The deployment kinematics of the joint enable deployment to be done extremely accurately. The joint comprises two braces (12,14) suitable for rolling one onto the other by two cylindrical surfaces (12a,14a). Guiding of rolling is ensured by two flexible members, such as rolling plates (16,28) extremities are secured to the braces and which pass by crossing between the cylindrical surfaces (12a,14a). A traction prestressing stored in the plates avoids any stray movement between the braces, especially at the time of deployment. The drive torque ensuring the automatic deployment of the joint and its end-of-travel locking are ensured by elastic bands (36) connecting the two braces and each formed of two superimposed plates. Successive joints may be joined using a synchronization deployment mechanism.
申请公布号 DE68902110(T2) 申请公布日期 1993.03.25
申请号 DE1989602110T 申请日期 1989.08.07
申请人 AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE, PARIS, FR 发明人 AUTERNAUD, JACQUES, F-06250 MOUGINS, FR;BARTEVIAN, JEAN, F-06150 CANNES LA BOCCA, FR;BERTHEUX, PHILIPPE, F-83600 LES ADRETS, FR;BLANC, ERIC, F-06110 LE CANNET, FR;DE MOLLERAT DU JEU, THIERRY, F-06270 VILLENEUVE LOUBET, FR;FOUCRAS, JEAN, F-06250 MOUGINS, FR;LOUIS, MICHEL, F-06200 NICE, FR;MARELLO, GEORGES, F-06210 MANDELIEU, FR;POVEDA, PIERRE, F-06110 LE CANNET ROCHEVILLE, FR;ROUX, CHRISTIAN, F-6210 MANDELIEU, FR
分类号 B64G1/44;B25J17/02;B64G1/22;E05D1/02;F16C11/12;(IPC1-7):B64G1/44;E05D1/00;B64G9/00 主分类号 B64G1/44
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