A. David Johnson - San Leandro CA, US Michael Bokaie - San Rafael CA, US Valery Martynov - San Francisco CA, US
Assignee:
Tini Alloy Company - San Leandro CA
International Classification:
F16B 35/00
US Classification:
411 825, 411DIG 2, 411392
Abstract:
A device and method for holding or clamping components together, and with the clamping being selectively loosened to permit the components to move through a predetermined distance without being fully released. A bolt has its head end attached to one component and its threaded end attached to the other component. A portion of the bolt's shank is formed with a necked-down portion. An actuator of shape memory alloy material is mounted about the bolt. When energized by heat, the actuator expands and exerts a great force which stretches the bolt, permanently deforming the bolt. This enables limited movement of the components while still restraining them from separating.
Single Crystal Shape Memory Alloy Devices And Methods
A. David Johnson - San Leandro CA, US Michael Bokaie - San Leandro CA, US Valery Martynov - San Francisco CA, US
Assignee:
TiNi Alloy Company - San Leandro CA
International Classification:
C22F 1/08
US Classification:
148562, 148563, 117 16, 117 25
Abstract:
Devices and methods of making devices having one or more components made of single crystal shape memory alloy capable of large recoverable distortions, defined herein as “hyperelastic” SMA. Recoverable Strains are as large as 9 percent, and in special circumstances as large as 22 percent. Hyperelastic SMAs exhibit no creep or gradual change during repeated cycling because there are no crystal boundaries. Hyperelastic properties are inherent in the single crystal as formed: no cold work or special heat treatment is necessary. Alloy components are Cu—Al—X where X may be Ni, Fe, Co, Mn. Single crystals are pulled from melt as in the Stepanov method and quenched by rapid cooling to prevent selective precipitation of individual elemental components. Conventional methods of finishing are used: milling, turning, electro-discharge machining, abrasion. Fields of application include aerospace, military, automotive, medical devices, microelectronics, and consumer products.
Single Crystal Shape Memory Alloy Devices And Methods
A. David Johnson - San Leandro CA, US Michael Bokaie - San Rafael CA, US Valery Martynov - San Francisco CA, US
Assignee:
TiNi Alloy Company - San Leandro CA
International Classification:
C22C 9/01
US Classification:
148402, 148435, 623 119
Abstract:
Devices and methods of making devices having one or more components made of single crystal shape memory alloy capable of large recoverable distortions, defined herein as “hyperelastic” SMA. Recoverable Strains are as large as 9 percent, and in special circumstances as large as 22 percent. Hyperelastic SMAs exhibit no creep or gradual change during repeated cycling because there are no crystal boundaries. Hyperelastic properties are inherent in the single crystal as formed: no cold work or special heat treatment is necessary. Alloy components are Cu—Al—X where X may be Ni, Fe, Co, Mn. Single crystals are pulled from melt as in the Stepanov method and quenched by rapid cooling to prevent selective precipitation of individual elemental components. Conventional methods of finishing are used: milling, turning, electro-discharge machining, abrasion. Fields of application include aerospace, military, automotive, medical devices, microelectronics, and consumer products.
Hyperelastic Shape Setting Devices And Fabrication Methods
Alfred David Johnson - San Leandro CA, US Valery Martynov - San Francisco CA, US Michael D. Bokaie - San Rafael CA, US George R. Gray - Fremont CA, US
Assignee:
TiNi Alloy Company - San Leandro CA
International Classification:
C22F 1/08
US Classification:
148562, 148563
Abstract:
Shape-setting methods for fabricating devices made of single crystal shape memory alloys. The method include drawing a single crystal of a shape memory alloy from a melt of the alloy. This is followed by heating and quenching the crystal sufficiently rapid to limit the formation of alloy precipitates to an amount which retains hyperelastic composition and properties of the crystal.
A. David Johnson - San Leandro CA, US Michael Bokaie - San Leandro CA, US Valery Martynov - San Francisco CA, US
International Classification:
F16B 35/00
US Classification:
411392
Abstract:
Devices and methods for making fasteners, such as bolts, having one or more components made of single crystal shape memory alloy capable of large recoverable distortions, and in particular having a plateau in the stress-strain relationship. A constant load is applied by a bolt that is tightened until the force exerted by the bolt is equal to the stress multiplied by the cross-section of a tension component in the bolt. Increasing or decreasing the length of the tension component by as much as several percent causes a negligible change in the load.
Alfred David Johnson - San Leandro CA, US Michael D. Bokaie - San Rafael CA, US Valery Martynov - San Francisco CA, US
Assignee:
TINI ALLOY COMPANY - San Leandro CA
International Classification:
F16B 31/04 F16B 35/02 F16B 29/00
US Classification:
411 145, 411395, 411392
Abstract:
Described herein are fasteners and devices for securing together several components so that the load applied to the components is constant or nearly constant. The fasteners described herein include a hyperelastic member having first end to which a first retainer is coupled and a second end to which a second retainer is coupled. The retainers are configured to contact the structures being fastened and transfer the load from the structures to the hyperelastic member. The hyperelastic member may be an elongate shaft (e.g., a rod, cylinder, strut, etc.), and is a shape memory alloy that is typically fabricated as a single crystal.
Michael D. Bokaie - Fremont CA John D. Busch - San Jose CA A. David Johnson - San Leandro CA Bruce Petty - Dunsmuir CA
Assignee:
TiNi Alloy Company - San Leandro CA
International Classification:
B25G 318
US Classification:
74 2
Abstract:
A release mechanism employing an actuating element of a shape memory alloy material. When the actuating element is heated through its phase-change transition temperature it applies a force which moves a latch to a position which activates the higher energy stored in a drive spring for moving a retaining element out of engagement with a structure. A detent when in a captured position releasably holds the retaining element in its locked position, and the detent is moved from a captured position to a retracted position to release the retaining element when the latch is moved by the actuating element.
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