A hybrid pressure and flowguage regulator apparatus includes a regulator body, an inlet, and an outlet assembly. The outlet assembly includes a first orifice of a first size, a second orifice of a second size that is larger than the first size, and a mechanism that automatically moves the first orifice between a first position and a second position. When the first orifice is in the first position, the flow of gas passes through both the first orifice and second orifice. When the first orifice is in the second position, the flow of gas bypasses the first orifice and flows through the second orifice with a specific flow rate or a second pressure that is less than the first pressure. The apparatus may also include a gauge that provides a visual indication of both the specific flow rate and the second pressure.

A hybrid pressure and flowguage regulator apparatus includes a regulator body, an inlet, and an outlet assembly. The outlet assembly includes a first orifice of a first size, a second orifice of a second size that is larger than the first size, and a mechanism that automatically moves the first orifice between a first position and a second position. When the first orifice is in the first position, the flow of gas passes through both the first orifice and second orifice. When the first orifice is in the second position, the flow of gas bypasses the first orifice and flows through the second orifice with a specific flow rate or a second pressure that is less than the first pressure. The apparatus may also include a gauge that provides a visual indication of both the specific flow rate and the second pressure.

A method of and a system for presenting an operating status of an aircraft engine. The method comprises accessing a first indication indicative of a position of an aircraft engine start switch and accessing a second indication indicative of an aircraft engine start operating mode, the second indication having been generated based on an analysis of a parameter associated with an operating condition of the aircraft engine. The method, upon determining that the position of the aircraft engine start switch is an on position and the aircraft engine start operating mode is a healthy start causes the display of a visual indication indicative of the healthy start. The method upon determining that the position of the aircraft engine start switch is an on position and the aircraft engine start operating mode is an abnormal start causes the display of a visual indication indicative of the abnormal start.

A method of and a system for presenting an operating status of an aircraft engine. The method comprises accessing a first indication indicative of a position of an aircraft engine start switch and accessing a second indication indicative of an aircraft engine start operating mode, the second indication having been generated based on an analysis of a parameter associated with an operating condition of the aircraft engine. The method, upon determining that the position of the aircraft engine start switch is an on position and the aircraft engine start operating mode is a healthy start causes the display of a visual indication indicative of the healthy start. The method upon determining that the position of the aircraft engine start switch is an on position and the aircraft engine start operating mode is an abnormal start causes the display of a visual indication indicative of the abnormal start.

This display control system is used in a work machine comprising a work unit and a drive device. The work unit performs work by driving an attachment attached to a machine body of the work machine. The drive device drives the attachment by supplying motive power thereto. The display control system comprises a display processing unit which displays, on a display device, a first display screen containing drive information relating to the drive device.

A smart phone user captures video and still images of a motor and makes a sound recording of his observations. The images and recordings are tagged with a date/time stamp, a serial number, bar code, matrix code, RFID code, or geolocation and sent wirelessly to an infrared camera. The infrared camera has a collocation application that reads the tag and creates a folder which holds the infrared image and the auxiliary information from the smartphone related to an asset. The collocation program also adds icons to the infrared image. By operating the user interface (not shown) of the infrared camera, the user may select an icon to view the images and listen to the sound recording.

A smart phone user captures video and still images of a motor and makes a sound recording of his observations. The images and recordings are tagged with a date/time stamp, a serial number, bar code, matrix code, RFID code, or geolocation and sent wirelessly to an infrared camera. The infrared camera has a collocation application that reads the tag and creates a folder which holds the infrared image and the auxiliary information from the smartphone related to an asset. The collocation program also adds icons to the infrared image. By operating the user interface (not shown) of the infrared camera, the user may select an icon to view the images and listen to the sound recording.

A marker display device for an electromechanical device including at least two scales on which a plurality of markers are distributed, respectively linked to the values of physical magnitudes corresponding to at least a first and second physical magnitude linked to each other and relative to the operation of an electromechanical device; a first and a second indicator are adapted to indicate a value associated with the first and second physical magnitude, respectively, both indicators being aligned on aligned markers, belonging to a first and a second graduated scale during the normal operation of the elements of the device assembly.

A marker display device for an electromechanical device including at least two scales on which a plurality of markers are distributed, respectively linked to the values of physical magnitudes corresponding to at least a first and second physical magnitude linked to each other and relative to the operation of an electromechanical device; a first and a second indicator are adapted to indicate a value associated with the first and second physical magnitude, respectively, both indicators being aligned on aligned markers, belonging to a first and a second graduated scale during the normal operation of the elements of the device assembly.

A multilayer structure for a garment, optionally footwear, includes a flexible substrate film for accommodating electronics, a number of flexible sensor pads provided on the film utilizing printed electronics technology, optionally screen printing or ink jetting, at least one electronic circuit, preferably integrated circuit, further provided on the film for controlling capacitive measurements via the number of sensor pads for obtaining an indication of pressure subjected to the multilayer structure, a number of conductor traces further printed on the film for electrically connecting the at least one electronic circuit and the number of capacitive sensor pads, a power supply element for powering electricity-driven components including the at least one electronic circuit, and at least one plastic layer molded upon the film substantially embedding the number of sensor pads, conductor traces and the at least one electronic circuit therewithin. A related method of manufacture is presented.