阅读说明：本技术 部署装置 (Deployment device ) 是由 J·拉巴特 E·泰克斯 于 2019-09-30 设计创作，主要内容包括：本发明涉及旨在被定位在支承结构(80)上的部署装置(20),其特征在于,该部署装置包括：第一仪器(11)和第二仪器(12)；部署机构,该部署机构包括：○主臂(14),该主臂一方面在第一附接点处连接至支承结构(80)的外表面(81),并且另一方面连接至第一仪器(11),第二仪器(12)连接至主臂(14)；○主电动机(15),该主电动机被配置成相对于面(81)致动主臂(14)；○辅助电动机(16),该辅助电动机被配置成相对于主臂(14)致动第二仪器(12),并且两个仪器(11、12)适于从收起配置转换到部署配置和/或从部署配置转换到收起配置,在收起配置中,一个仪器在另一个仪器上地在支承结构(80)的面(81)上,在部署配置中,两个仪器(11、12)彼此相距一距离并且与支承结构(80)相距一距离。(The invention relates to a deployment device (20) intended to be positioned on a support structure (80), characterized in that it comprises: a first instrument (11) and a second instrument (12); a deployment mechanism, the deployment mechanism comprising: -a main arm (14) connected, on the one hand, to the outer surface (81) of the supporting structure (80) at a first attachment point and, on the other hand, to the first instrument (11), the second instrument (12) being connected to the main arm (14); a main motor (15) configured to actuate the main arm (14) with respect to the face (81); an auxiliary motor (16) configured to actuate the second instrument (12) with respect to the main arm (14), and the two instruments (11, 12) are adapted to pass from a stowed configuration, in which one is on the other on a face (81) of the supporting structure (80), to a deployed configuration, in which the two instruments (11, 12) are at a distance from each other and from the supporting structure (80), and/or from the deployed configuration to the stowed configuration.)

1. A deployment device (10, 20, 30, 40, 50, 60, 70) designed to be positioned on a support structure (80), characterized in that it comprises:

a first instrument (11) and a second instrument (12),

a deployment mechanism (13) comprising:

-a main arm (14) connected on the one hand to a face (81) of the supporting structure (80) at a first attachment point (82) and on the other hand to the first instrument (11), the second instrument (12) being connected to the main arm (14),

a main motor (15) configured to actuate the main arm (14) with respect to the face (81),

an auxiliary motor (16) configured to actuate the second instrument (12) with respect to the main arm (14),

and the two instruments (11, 12) being able to be converted from a stowed configuration, in which one instrument is on the other on the face (81) of the supporting structure (80), to a deployed configuration, in which the two instruments (11, 12) are distant from each other and from the supporting structure (80), and/or from the deployed configuration to the stowed configuration.

2. Deployment device (20, 30, 40, 50, 60, 70) according to claim 1, characterized in that said deployment mechanism (13) comprises an auxiliary arm (21) connected on the one hand to said main arm (14) at a second attachment point (22) and on the other hand to said second instrument (12).

3. The deployment device (30, 40, 50, 60, 70) according to claim 1 or 2, characterized in that the main motor (15) is configured to actuate the main arm (14) to rotate about a main rotation axis (31) with respect to the face (81) of the support structure (80).

4. The deployment device (40, 70) according to any one of claims 1 to 3, characterized in that the face (81) of the support structure (80) extends along a plane (XY) defined by a first axis (X) and a second axis (Y), the second axis (Y) being substantially perpendicular to the first axis (X), and in that the main axis (31) is parallel to the plane (XY).

5. The deployment device (50, 60, 70) according to any one of claims 1 to 3, characterized in that the face (81) of the support structure (80) extends along a plane (XY) defined by a first axis (X) and a second axis (Y), the second axis (Y) being substantially perpendicular to the first axis (X), and the main axis (31) intersecting the plane (XY).

6. The deployment device (60, 70) according to claim 5, characterized in that the main axis (31) is perpendicular to the plane (XY).

7. The deployment device (70) according to one of claims 1 to 6, characterized in that at least the primary arm (14) and/or, if present, the secondary arm (21) is connected to the instrument (11, 12) to which the arm is connected by means of N arm sections (71N), N being an integer greater than or equal to 1, and N motors (72N), each motor being associated with an arm section and configured to actuate the relative arm section in order to position the instrument (11, 12) to which the arm is connected relative to the other of the two instruments.

8. The deployment device (10, 20, 30, 40, 50, 60, 70) according to any one of the preceding claims, characterized in that the instrument is an antenna.

9. A satellite (90), characterized in that it comprises at least one deployment device (10, 20, 30, 40, 50, 60, 70) according to one of the preceding claims.