초록 ▼

A two-stage acceleration sensing apparatus is disclosed which has applications for use in a fuze assembly for a projected munition. The apparatus, which can be formed by bulk micromachining or LIGA, can sense acceleration components along two orthogonal directions to enable movement of a shuttle fro

A two-stage acceleration sensing apparatus is disclosed which has applications for use in a fuze assembly for a projected munition. The apparatus, which can be formed by bulk micromachining or LIGA, can sense acceleration components along two orthogonal directions to enable movement of a shuttle from an "as-fabricated" position to a final position and locking of the shuttle in the final position. With the shuttle moved to the final position, the apparatus can perform one or more functions including completing an explosive train or an electrical switch closure, or allowing a light beam to be transmitted through the device.

대표청구항 ▼

What is claimed is: 1. A microelectromechanical safing and arming apparatus, comprising: (a) a subbase having an opening therethrough for holding a first explosive; (b) a shuttle suspended from a plurality of springs above the subbase, with the shuttle holding a second explosive initially misaligne

What is claimed is: 1. A microelectromechanical safing and arming apparatus, comprising: (a) a subbase having an opening therethrough for holding a first explosive; (b) a shuttle suspended from a plurality of springs above the subbase, with the shuttle holding a second explosive initially misaligned from the first explosive; (c) a first latch for locking the shuttle in a first position wherein the second explosive is misaligned with respect to the first explosive, with the first latch being disengageable to move in a direction substantially normal to a plane of the subbase in response to a first acceleration component directed substantially normal to the plane of the subbase to allow movement of the shuttle in an orthogonal direction substantially in-plane with the subbase to a second position wherein the first and second explosives are aligned in response to a second acceleration component directed substantially in-plane with the subbase; and (d) a second latch for locking the shuttle in the second position. 2. The apparatus of claim 1 further comprising a lid formed over the shuttle and subbase, with the lid including an initiator or detonator for igniting the second explosive when the shuttle is in the second position. 3. The apparatus of claim 1 wherein the first latch comprises a cantilevered beam having a thickness less than the thickness of the shuttle. 4. The apparatus of claim 3 wherein the first latch further comprises a clasp located at a free end of the cantilevered beam. 5. The apparatus of claim 4 wherein the shuttle comprises at least one tab for engaging the clasp to lock the shuttle in the first position. 6. The apparatus of claim 1 wherein the second latch comprises at least one cantilevered beam having a catch formed at a free end thereof for engaging a tang projecting from the shuttle to hold the shuttle in the second position. 7. The apparatus of claim 1 further comprising a stop to prevent an in-plane movement of the shuttle beyond the second position. 8. The apparatus of claim 1 wherein the subbase comprises silicon. 9. The apparatus of claim 1 wherein the first explosive comprises an explosive material selected from the group consisting of cyclic nitramine and polycyclic nitramine. 10. The apparatus of claim 1 wherein the second explosive comprises an explosive material selected from the group consisting of lead azide, silver azide and lead styphanate.