Modular actuation device for an aerodynamic control surface of a missile
US-9531238-B2 · Dec 27, 2016 · US
US10794673B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10794673-B2 |
| Application number | US-201715482737-A |
| Country | US |
| Kind code | B2 |
| Filing date | Apr 8, 2017 |
| Priority date | Apr 24, 2012 |
| Publication date | Oct 6, 2020 |
| Grant date | Oct 6, 2020 |
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Official abstract text for this publication.
A munition including: a control surface actuation device including: an actuator comprising two or more pistons, each of the pistons being movable between an extended and retracted position, the retracted position resulting from an activation of each of the two or more pistons; and a rotatable plate having a pocket corresponding to each of the two or more pistons, each pocket being engageable with a corresponding portion of each of the two or more pistons, a distance between the pockets being different than a distance between the portions of the two or more pistons, such that activation of the portion into the corresponding pocket sequentially rotates the plate; and a control surface operatively connected to the plate such that rotation of the plate rotates the control surface.
Opening claim text (preview).
What is claimed is: 1. A munition comprising: a control surface actuation device comprising: an actuator comprising first and second pistons, each of the first and second pistons being movable between an extended and retracted position, the extended position resulting from an activation of each of the first and second pistons; and a rotatable plate having more than two pockets, each pocket being engageable with a corresponding portion of a respective one of the first and second pistons, a distance between adjacent pockets of the more than two pockets being different than a distance between the portions of the first and second pistons, such that activation of the portion into a respective pocket rotates the plate; and a control surface operatively connected to the plate such that rotation of the plate rotates the control surface. 2. The munition of claim 1 , wherein the actuator comprises: a bellows for movably housing each of the first and second pistons; and a plurality of gas generation charges generating a gas in fluid communication with the bellows; wherein activation of each of the plurality of gas generation charges results in an increase in pressure in the bellows causing the piston to extend from the retracted to the extended position such that the portion extends into the corresponding pocket. 3. The munition of claim 1 , wherein the control surface is a fin. 4. The munition of claim 1 , wherein the munition further comprises a second control surface actuation device comprising: another actuator comprising first and second pistons, each of the first and second pistons being movable between an extended and retracted position, the extended position resulting from an activation of each of the first and second pistons; and another rotatable plate having more than two pockets, each pocket being engageable with a corresponding portion of a respective one of the first and second pistons, a distance between adjacent pockets of the more than two pockets being different than a distance between the portions of the first and second pistons, such that activation of the portion into a respective pocket rotates the plate; wherein the munition further comprises another control surface operatively connected to the another plate such that rotation of the another plate rotates the another control surface. 5. The munition of claim 4 , wherein the another control surface is a fin.
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