Patent classifications
G02B23/2492
Imaging system for inspecting components of turbomachines and method of assembly thereof
An imaging system includes a sight tube extending along a longitudinal axis of the imaging system and configured to extend through an access port. The sight tube includes a wall extending about the longitudinal axis and defining a cavity. The imaging system also includes a plurality of cooling channels extending through the sight tube. The plurality of cooling channels are configured to direct cooling fluid through the sight tube for cooling the imaging system. The plurality of cooling channels are formed in the sight tube such that at least one cooling channel of the plurality of cooling channels extends in a direction oblique to the longitudinal axis.
Switch unit, image pickup apparatus for endoscope including switch unit, and endoscope including switch unit
A switch unit includes a frame body which is fixed to an opening section and in which a plurality of holes are formed, a plurality of switches provided in each of two of the plurality of holes, a soft switch cover that is disposed in each of the two holes and covers the plurality of switches, a first catch section formed as part of the switch cover in a position between the plurality of switches, a switch fixing member that is disposed in each of the two holes, is covered with the switch cover, fixes the plurality of switches to the opening section, and catches the first catch section in a position facing the first catch section, and a second catch section formed at an outer circumference of the switch cover and caught by the frame body.
SYSTEM AND METHOD FOR HANDLING AND CHARTING DATA OBTAINED BY AN INSPECTION VEHICLE
A method and system for acquiring, manipulating and displaying inspection data obtained by sensors associated with submersible inspection vehicle within a housing having a liquid medium is disclosed in the present application. A control system including an electronic controller is operably coupled with the inspection vehicle and is configured to display data transmitted from the sensor and overlay input data from an operator on the display to facilitate real time analysis during the inspection event.
Borescope that processes image data into 3-d data for optically inspecting gas turbines
A borescope is for optically inspecting gas turbines of aircraft engines. The borescope having an electronic image capture unit as a borescope objective at an end of a shaft, which is suitable for insertion into a borescope opening and configured for accurate positioning of the borescope objective relative to the borescope opening and through which data lines and supply lines for the image capture unit are guided. The image capture unit has: two spaced apart image capture sensors, recording cones of which overlap in a specified recording plane forming a recording region, in such a way that image data of the two image capture sensors are configured to be processed into 3-D data by way of triangulation.
HIGH-TEMPERATURE ENDOSCOPE PREVENTING IMPURITIES OF INGOT GROWTH APPARATUS FROM BEING DEPOSITED
Disclosed is a high-temperature endoscope of an ingot growth apparatus in which impurity deposition is prevented by having a structure that increases a flow rate of an inert gas for preventing impurities from being deposited. A high-temperature endoscope preventing impurities of an ingot growth apparatus from being deposited, according to one embodiment of the present invention, may comprise: a frame extending to the inside of a chamber of the ingot growth apparatus and having a gas discharge port provided at an end portion thereof through which an inert gas is discharged; a lens installed at the center of the end portion of the frame and protected by the inert gas discharged from the gas discharge port; and a guide tube installed on an outer surface of the frame and having a guide portion extending from the end portion of the frame so as to guide the inert gas to prevent impurities from being deposited on the lens by increasing a flow rate of the inert gas.
IMAGING SYSTEMS WITH IMPROVED THREAD LIFE
Systems, methods, and devices are provided that facilitate reducing wear of threads of a camera head of an imaging system (e.g., a borescope), thereby increasing the lifespan of an imaging system. In some embodiments, an imaging system is provided that includes a camera head made of anodized TiAl.sub.6V.sub.4 and coated with a solid film lubricant. The imaging system can also include a probe tip made of 303 stainless steel and coated with a diamond-line carbon coating. By using a camera head made of anodized TiAl.sub.6V.sub.4 and coated with a SFL in combination with a probe tip made of 303 SS and coated with a DLC, wear on threads of the camera head can be reduced, thereby increasing the lifespan of the imaging system.
Image pickup apparatus and endoscope
An image pickup apparatus includes an image pickup device on which a light receiving section is formed, a heat transfer member made of a material having thermal conductivity equal to or higher than 15 W/(m.Math.K), the heat transfer member including a wiring board, a joining section joined to the image pickup device, a bending section extended from the joining section, and a fixed section extended from the bending section, and a housing made of metal, an inner surface of which is in contact with a part of the fixed section of the heat transfer member housed on an inside.
Apparatus for insertion into a cavity of an object
Apparatus for insertion into a cavity of an object, the apparatus comprising: a first tube comprising a first end, a second end and a first cavity extending between the first end and the second; a member positioned within the first cavity of the first tube and configured to enable an action to be performed; a heat pipe including a first end, a second end, and a second cavity extending between the first end and the second end, the first tube being positioned within the second cavity of the heat pipe; and an actuator configured to move the first tube relative to the heat pipe.
Optical apparatus and sight tube for inspecting turbine engine components
An apparatus for insertion through an opening in an outer casing of a gas turbine engine and inspection of internal turbine components at elevated temperatures having an optical sight tube configured to optically communicate with an interior of gas turbine engine via a distal end disposed at the interior and a proximal end disposed exterior of the internal turbine components and defined by a first longitudinal wall, at least one lens at the distal end of the optical sight tube adjacent to the longitudinal wall; and at least one longitudinal cooling groove in the longitudinal wall for flowing a cooling medium from a location external to the turbine to cool the optical sight tube at a location at least adjacent the distal end.
OPTICAL SYSTEM AND METHOD FOR CLEANING OPTICAL WINDOWS
A system for downhole optical analysis includes a housing forming at least part of a pressure barrier. The system also includes a window, formed at an end of the housing, the window being at least semi-transparent to permit light to travel through the window. The system further includes at least one light source, arranged within the housing, wherein the at least one light source is configured to emit a beam of light at a wavelength to enable non-contact, optical cleaning of the window, the wavelength being selected to reduce interaction with the window while heating a fluid film formed on the window outside the housing.