Deployment and actuation mechanisms

• US 4,709,877 A
• Filed: 04/09/1986
• Issued: 12/01/1987
• Est. Priority Date: 11/25/1983
• Status: Expired due to Term

• Current Assignee: MBDA UK Ltd. (MBDA SAS)
• Original Assignee: British Aerospace, Inc.
• Inventors: Goulding, Kenneth
• Primary Examiner(s): Kyle, Deborah L.
• Assistant Examiner(s): Carone, Michael J.
• Application Number:
  US06/849,945
• Time in Patent Office: 601 Days
• Field of Search: 244/3.22, 244/3.28, 244/3.29, 244/49, 74/425, 74/411.5, 74/89.14, 74/89, 15/250.16
• US Class Current: 244/3.28
• CPC Class Codes: F42B 10/14 using fins spread or deployed after launch, e.g. after leaving the barrel
• CPC Class Codes: F42B 10/64 of fins
• CPC Class Codes: Y10T 74/18792 including worm
• CPC Class Codes: Y10T 74/19637 with brake means for gearing
• CPC Class Codes: Y10T 74/19828 Worm

Abstract

A mechanism for rotating a missile control surface 6 about an axis 26 from the illustrated stowed position within the missile to a deployed position in which it extends radially from the missile axis M--M and for then turning the surface about radial axis 13 so as to steer the missile. A single drive motor 22 is coupled by worm 20 to a bevel gear 18 mounted in a bracket 12, the bracket being turnable about axis 13 with respect to a fixed support 10. The control surface 6 is fixed via arm 23 to a bevel gear 24, which gear is mounted to the bracket 12 for rotation about axis 26 and is engaged with gear 18. While the surface 6 is stowed, a sprung locking pin 14 carried by the bracket 12 is held in engagement with support 10 by gear 18 so that rotation of the motor 22 rotates gear 18 with respect to bracket 12 and hence rotates gear 24 along with arm 23 and control surface 6 about axis 26. When the surface so comes to its deployed position, a hole 25 in gear 18 becomes aligned with pin 14 and the pin moves into the hole so fixing gear 18 with respect to the bracket. Rotation of the shaft of motor 22 then produces rotation of bracket 12, gear 18 and surface 6 about axis 13.

The mechanism can be used in other situations where it is required to erect a member from a stowed position to one of a range of operative positions and to then move the member within that range.

Claims

1. A mechanism for erecting a member from an initial stowed position to one of a range of operative positions by turning movement about a first axis, and for then moving the member within said range by turning movement about a second axis arranged at an angle other than zero with respect to said first axis, the mechanism comprising a support structure operable for supporting said member for movement with respect to said support structure, a drive motor connected to said support structure and having a movable output element, means coupling said motor output element to said member and operable whilst said member is at said stowed position and between said stowed and operative positions for translating movement of said motor output element to produce said erection of said member and which becomes operable when said member is erected for translating movement of said motor output element to produce movement of said member within said range of operative positions.

2. A mechanism according to claim 1, wherein said coupling means comprises:

a first rotatable element supported by said support structure and able to turn with respect to said support structure about a fixed axis,

a second rotatable element supported by said first rotatable element and turnable with respect to said first rotatable element about said first axis, and

means for alternately locking and unlocking said first rotatable element with respect to said support structure and unlocking and locking said second rotatable element with respect to said first element,

said member being supported by said first rotatable element and being turnable with respect to said first rotatable element about a second axis transverse to said first axis between said stowed and erected positions, the output element of the drive motor being arranged to apply a turning moment about said first axis to said second rotatable element and said member being coupled to said second rotatable element such that, with said first element locked to said support structure by said locking means, said turning moment causes said second rotatable element to turn with respect to said first rotatable element and said member to be turned about said second axis and, with said first rotatable element unlocked from said support structure but instead locked by said locking means to said second element, said turning moment causes said first and second rotatable elements and said member to turn together about said first axis with respect to said support structure.

3. A mechanism according to claim 2, wherein said second rotatable element is a gear-toothed element and said drive motor and said member are coupled to said gear-toothed element by way of respective gears.

4. A mechanism according to claim 2 or 3, wherein the locking means comprises a locking pin supported by the first rotatable element and spring means for urging said pin to move towards the second rotatable element, the support structure having a hole in it which, in one relative position of said support structure and said first rotatable element, is able to receive one end of said pin, and said second rotatable element having a hole into which, when it is aligned with said pin, said pin is urged to move by said spring means, said one end of said pin thereby coming out of engagement with said hole in said support structure.

5. A mechanism according to claim 4, wherein the support structure has an arcuate slot formed therein extending each side of the hole, said one end of the pin remaining engaged within said slot when said pin moves into engagement with the second rotatable member so as to then limit the range of movement of the first rotatable member with respect to said support structure.