Fin retention and release mechanism

Patent metadata

Field	Value
Publication number	US-10295318-B2
Application number	US-201515123330-A
Country	US
Kind code	B2
Filing date	Mar 12, 2015
Priority date	Mar 13, 2014
Publication date	May 21, 2019
Grant date	May 21, 2019

Abstract

An improved fin retention and release mechanism (15) comprising an elongated body (16), at least one fin (18a) mounted to the body and capable of moving from a stowed position (30) to a deployed position (32), an actuator (20a) connected to the fin and arranged to rotate the fin about a first axis (33), a fin retention member (19a) connected to the body and configured and arranged to rotate about a second axis (34) from a locked position (36) to a release position (38), the fin and the fin retention member configured and arranged such that the fin is held in the stowed position by the fin retention member when being in the locked position and the fin is not held in the stowed position by the fin retention member when being in the release position, and wherein actuation of the fin about the first axis by the actuator rotates the fin about the first axis in a first direction (39) and correspondingly rotates the fin retention member about the second axis in a second direction (40) opposite to the first direction and from the locked position to the release position.

First claim

What is claimed is:

1. A projectile comprising:
an elongated body;
at least one fin mounted to said body and capable of moving from a stowed position to a deployed position;
an actuator connected to said fin and configured to selectively rotate said fin about a first axis in both a first direction and a second direction to operatively adjust a position of said fin about said first axis;
a fin retention member connected to said body and configured to rotate about a second axis from a locked position to a release position;
said fin and said fin retention member configured such that said fin is held in said stowed position by said fin retention member when said fin retention member is in said locked position and said fin is not held in said stowed position by said fin retention member when said fin retention member is in said release position; and
wherein selective actuation of said fin about said first axis by said actuator rotates said fin about said first axis in said first direction and correspondingly rotates said fin retention member about said second axis in a second direction opposite to said first direction and from said locked position to said release position.

2. The projectile set forth in claim 1 , wherein said fin is pivotably mounted to said body and rotatable about a third axis from said stowed position to said deployed position.

3. The projectile set forth in claim 1 , and further comprising a spring element arranged between said fin retention member and said body and configured to bias said fin retention member toward said locked position.

4. The projectile set forth in claim 3 , wherein said fin retention member comprises a retaining end portion and a shaft portion and said spring element comprises a torsion spring orientated about said shaft portion.

5. The projectile set forth in claim 3 , wherein said fin retention member comprises a reset groove configured to receive a reset tool, wherein said fin retention member may be manually rotated from said locked position to said release position.

6. The projectile set forth in claim 1 , wherein said fin comprises a retaining pocket, said fin retention member comprises a retaining end portion, and said fin retaining pocket is configured to receive said end portion of said retention member when said fin is in said stowed position.

7. The projectile set forth in claim 1 , wherein said fin retention member comprises a substantially tear shaped retaining end portion and a shaft portion.

8. The projectile set forth in claim 1 , wherein said fin retention member is connected to said body with a retaining ring.

9. The projectile set forth in claim 1 , wherein said body comprises a fin stop.

10. The projectile set forth in claim 1 , wherein said first axis and said second axis are parallel.

11. The projectile set forth in claim 1 , and further comprising a second fin mounted to said body and capable of moving from a stowed position to a deployed position, a second actuator connected to said second fin and configured to selectively rotate said second fin about a second fin axis in both a first direction and a second direction to operatively adjust a position of said second fin about said second fin axis, a second fin retention member connected to said body and configured to rotate about a second fin retention member axis from a locked position to a release position, said second fin and said second fin retention member configured such that said second fin is held in said stowed position by said second fin retention member when said second fin retention member is in said locked position and said second fin is not held in said stowed position by said second fin retention member when said second fin retention member is in said release position, and wherein selective actuation of said second fin about said second fin axis by said second actuator rotates said second fin about said second fin axis in a first direction and correspondingly rotates said second fin retention member about said second fin retention member axis in a second direction opposite to said first direction and from said locked position to said release position.

Assignees

• Moog Inc

Inventors

• Hammond Laurie
• Pickard Jonathon

Classifications

• F42B10/18

  using a longitudinally slidable support member · CPC title

• F42B10/20

  deployed by combustion gas pressure, or by pneumatic or hydraulic forces · CPC title

• B64C5/12

  for retraction against or within fuselage or nacelle · CPC title

• F42B10/16

  Wrap-around fins · CPC title

• F42B10/14 Primary

  using fins spread or deployed after launch, e.g. after leaving the barrel · CPC title