Patent classifications
C03B2205/67
FIBER OPTIC MANUFACTURING IN SPACE
Aspects of the embodiments are directed to systems and methods for forming an optical fiber in a low gravity environment, and an optical fiber formed in a low gravity environment. The system can include a preform holder configured to secure a preform; a heating element secured to a heating element stage and residing adjacent the preform holder; a heating element stage motor configured to move the heating element stage; a tension sensor; a spool; a spool tension motor coupled to the spool and configured to rotate the spool; and a control system communicably coupled to the heating element stage motor and the spool tension motor and configured to control the movement of the heating element stage based on a rotational speed of the spool. The optical fiber can include a fluoride composition, such ZrF4-BaF2-LaF3-AlF3-NaF (ZBLAN), and can be characterized by an insertion loss in a range from 13 dB/1000 km to 120 dB/1000 km.
METHOD AND DEVICE FOR MANUFACTURING AN OPTICAL FIBRE
A method for manufacturing an optical fibre, in which a preform is inserted into a furnace, the preform is drawn via an outlet of the furnace, and at least one laser beam is applied to a working zone of the drawn preform, each laser beam being power-modulated according to a modulation frequency. A device for manufacturing an optical fibre is also provided.
Fiber optic manufacturing in space
Aspects of the embodiments include an optical fiber formed in a low gravity environment. The optical fiber can be used in airframe applications for missile defense, oil-field applications for down-well laser applications, optical communications, and other applications. The optical fiber can include a fluoride composition, such ZrF4-BaF2-LaF3-AlF3-NaF (ZBLAN), and can be characterized by an insertion loss in a range from 13 dB/1000 km to 120 dB/1000 km. The optical fiber can deliver optical energy with low insertion loss at the desired power and wavelength for the various applications.
Method for manufacturing optical connection component
The present embodiment makes it possible to reduce the height of an optical connection component including a bent optical fiber having a bent-shape part and a fiber fixing component in a safer and more stable manner compared to a conventional technique. Before the fiber fixing component is fixed to the bent optical fiber, formation of a bent portion using the fiber fixing component obliquely disposed and heating of the bent portion are repeated a plurality of times for the optical fiber to which the fiber fixing component is movably fitted. At that time, movement of the optical fiber and the heating of the bent portion are alternately repeated. Thus, a plurality of bent portions where stress is released is formed in the optical fiber along the longitudinal direction thereof.
MICROGRAVITY CRUCIBLE-CONTROLLED MANUFACTURING
Embodiments are directed to systems and methods for material processing in a low gravity environment, and an optical fiber formed in a low gravity environment. In some embodiments, the system may include a radiation-based heating element, such as a laser, to heat portions of a work volume of the system to process materials in the work volume. The system may control temperature and the temperature gradients to compensate for effects of a microgravity environment on the material during processing.
FIBER OPTIC MANUFACTURING IN SPACE
Aspects of the embodiments include an optical fiber formed in a low gravity environment. The optical fiber can be used in airframe applications for missile defense, oil-field applications for down-well laser applications, optical communications, and other applications. The optical fiber can include a fluoride composition, such ZrF4-BaF2-LaF3-AlF3-NaF (ZBLAN), and can be characterized by an insertion loss in a range from 13 dB/1000 km to 120 dB/1000 km. The optical fiber can deliver optical energy with low insertion loss at the desired power and wavelength for the various applications.
METHOD FOR MANUFACTURING OPTICAL CONNECTION COMPONENT
The present embodiment makes it possible to reduce the height of an optical connection component including a bent optical fiber having a bent-shape part and a fiber fixing component in a safer and more stable manner compared to a conventional technique. Before the fiber fixing component is fixed to the bent optical fiber, formation of a bent portion using the fiber fixing component obliquely disposed and heating of the bent portion are repeated a plurality of times for the optical fiber to which the fiber fixing component is movably fitted. At that time, movement of the optical fiber and the heating of the bent portion are alternately repeated. Thus, a plurality of bent portions where stress is released is formed in the optical fiber along the longitudinal direction thereof.
Fiber optic manufacturing in space
Aspects of the embodiments are directed to systems and methods for forming an optical fiber in a low gravity environment, and an optical fiber formed in a low gravity environment. The system can include a preform holder configured to secure a preform; a heating element secured to a heating element stage and residing adjacent the preform holder; a heating element stage motor configured to move the heating element stage; a tension sensor; a spool; a spool tension motor coupled to the spool and configured to rotate the spool; and a control system communicably coupled to the heating element stage motor and the spool tension motor and configured to control the movement of the heating element stage based on a rotational speed of the spool. The optical fiber can include a fluoride composition, such ZrF4-BaF2-LaF3-AlF3-NaF (ZBLAN), and can be characterized by an insertion loss in a range from 13 dB/1000 km to 120 dB/1000 km.
FIBER OPTIC MANUFACTURING IN SPACE
Aspects of the embodiments are directed to systems and methods for forming an optical fiber in a low gravity environment, and an optical fiber formed in a low gravity environment. The system can include a preform holder configured to secure a preform; a heating element secured to a heating element stage and residing adjacent the preform holder; a heating element stage motor configured to move the heating element stage; a tension sensor; a spool; a spool tension motor coupled to the spool and configured to rotate the spool; and a control system communicably coupled to the heating element stage motor and the spool tension motor and configured to control the movement of the heating element stage based on a rotational speed of the spool. The optical fiber can include a fluoride composition, such ZrF4-BaF2-LaF3-AlF3-NaF (ZBLAN), and can be characterized by an insertion loss in a range from 13 dB/1000 km to 120 dB/1000 km.
Fiber optic manufacturing in space
Aspects of the embodiments are directed to systems and methods for forming an optical fiber in a low gravity environment, and an optical fiber formed in a low gravity environment. The system can include a preform holder configured to secure a preform; a heating element secured to a heating element stage and residing adjacent the preform holder; a heating element stage motor configured to move the heating element stage; a tension sensor; a spool; a spool tension motor coupled to the spool and configured to rotate the spool; and a control system communicably coupled to the heating element stage motor and the spool tension motor and configured to control the movement of the heating element stage based on a rotational speed of the spool. The optical fiber can include a fluoride composition, such ZrF4-BaF2-LaF3-AlF3-NaF (ZBLAN), and can be characterized by an insertion loss in a range from 13 dB/1000 km to 120 dB/1000 km.