Hold down release mechanism with integral sensing
View Patent ↗One aspect of the present invention involves a hold-down and release mechanism (“HDRM”) that includes a hold-then-release mechanism configured to hold an element until the hold-then-release mechanism is commanded to release the element; and an integral sensor configured to sense an amount of a parameter of interest associated with the HDRM and to communicate the sensed amount of the parameter of interest to a receiving device. The parameter of interest comprises one of tensile preload, temperature, vibration, shock, and time from application of an HDRM firing current to HDRM release of the element.
1. A hold down and release mechanism (“HDRM”), comprising:
a hold-then-release mechanism configured to hold an element until the hold-then-release mechanism is commanded to release the element; and
an integral sensor configured to sense an amount of a parameter of interest associated with the HDRM and to communicate the sensed amount of the parameter of interest to a receiving device.
2. The HDRM of claim 1 , wherein the parameter of interest comprises one of tensile preload, temperature, vibration, shock, and time from application of an HDRM firing current to HDRM release of the element.
3. The HDRM of claim 1 , wherein the HDRM further comprises a load bearing device to which an amount of tensile preload is applied to hold the element, wherein the tensile preload comprises the parameter of interest, and wherein the integral sensor is configured to sense the amount of tensile preload applied to the load bearing device and to communicate the sensed amount of applied tensile preload to the receiving device.
4. The HDRM of claim 1 , wherein the load bearing device comprise a release pin and the integral sensor comprises a compressive load washer in contact with the release pin.
5. The HDRM of claim 4 , further comprising an additional washer disposed in contact with the release pin and the compressive load washer, wherein the additional washer is configured to even out the applied tensile preload on the compressive load washer.
6. The HDRM of claim 1 , wherein the HDRM comprises one of a non-energetic HDRM and an energetic HDRM.
7. The HDRM of claim 6 , wherein the non-energetic HDRM includes a split spool release device having a link wire that breaks upon application of electrical energy.
8. The HDRM of claim 1 , wherein the receiving device comprises a control unit configured to receive from the integral sensor the communicated sensed amount of the parameter of interest.
9. The HDRM of claim 8 , wherein the control unit is configured to communicate with a networked initiation system comprising a controller, the HDRM, a plurality of additional HDRMs, and an interface bus connecting together the controller, the HDRM and the plurality of additional HDRMs.
10. The HDRM of claim 9 , wherein the HDRM is addressable within the networked initiation system.
11. The HDRM of claim 1 , wherein the element is attached to a spacecraft, and wherein the element comprises a solar array, an antenna reflector, a radiator, an instrument boom, a propulsion pointing actuator, a door, or a sensor.
12. A networked initiation system, comprising:
a control unit;
at least one hold down and release mechanism (“HDRM”) configured to hold in place an element and to release the held element upon receipt of an activate command from the control unit, wherein the at least one HDRM comprises a hold-then-release mechanism configured to hold the element until the hold-then-release mechanism is commanded by the activate command from the control unit to release the element, the at least one HDRM also comprises an integral sensor configured to sense an amount of a parameter of interest associated with the at least one HDRM and to communicate the sensed amount of the parameter of interest to the control unit; and
an interface bus configured to connect together the control unit and the at least one HDRM, to provide power from the control unit to the at least one HDRM, and to communicate between the control unit and the at least one HDRM.
13. The networked initiation system of claim 12 , wherein the parameter of interest comprises one of tensile preload, temperature, vibration, shock, and time from application of an HDRM firing current to HDRM release of the held element.
14. The networked initiation system of claim 12 , wherein the at least one HDRM further comprises a load bearing device to which an amount of tensile preload is applied, wherein the integral sensor is configured to sense the amount of tensile preload applied to the load bearing device and to communicate the sensed amount of applied tensile preload to the control unit, the tensile preload comprising the parameter of interest.
15. The networked initiation system of claim 14 , wherein the load bearing device comprises a release pin and the integral sensor comprises a compressive load washer in contact with the release pin.
16. The networked initiation system of claim 15 , further comprising an additional washer disposed in contact with the release pin and the compressive load washer, wherein the additional washer is configured to even out the applied tensile preload on the compressive load washer.
17. The networked initiation system of claim 12 , wherein the element comprises a solar array, an antenna reflector, a radiator, an instrument boom, a propulsion pointing actuator, a door, or a sensor.
18. The networked initiation system of claim 12 , wherein the at least one HDRM comprises a split spool release device (“SSRD”) having a link wire that breaks upon application of electrical energy upon receipt by the at least one HDRM of the activate command from the control unit.
19. The networked initiation system of claim 12 , wherein the at least one HDRM comprises a non-energetic HDRM.
20. The networked initiation system of claim 12 , wherein the at least one HDRM comprises an energetic HDRM.