Abstract: A method for measuring a windspeed vector is described. A true airspeed vector of a flying machine is measured while the machine is in flight using one or more nanowires on the flying machine. Each nanowire is configured to measure a value of local air velocity relative to the flying machine. A velocity of the flying machine relative to the ground is measured while the machine is in flight, and then (a) the true airspeed vector is subtracted from (b) the velocity of the flying machine relative to the ground. Other applications are also described.
Abstract: A vaporizer (20) is shaped to define a flow channel (120) that is open to an environment external to the vaporizer at first and second ends of the flow channel. At the first end of the flow channel is a mouthpiece (112) of the vaporizer. A flow sensor (114) includes (a) a nanoscale resistive element (200) disposed at least partially within the flow channel and (b) sensing circuitry (115) configured to measure a change in the nanoscale resistive element due to airflow within the flow channel. Other applications are also described.
Type:
Application
Filed:
July 16, 2020
Publication date:
August 18, 2022
Applicant:
INSTRUMEMS INC.
Inventors:
Gilad ARWATZ, James BORTHWICK, Jeffrey DIAMENT
Abstract: Numerous embodiments of a bubble detection apparatus and method are disclosed. In one embodiment, a bubble detection module is placed into a liquid to be monitored. The module comprises a physical structure housing a nanowire sensing element. The liquid flows through the physical structure. An electric bias is placed across the nanowire sensing element, and the resistance of the nanowire sensing element changes when a bubble is in contact with the element. A change in voltage or current of the bias signal can be measured to identify the exact instances when a bubble is in contact with the nanowire sensing element.
Type:
Grant
Filed:
June 16, 2020
Date of Patent:
August 2, 2022
Assignee:
INSTRUMEMS, INC.
Inventors:
Gilad Arwatz, Jeffrey Diament, James Borthwick
Abstract: A method for measuring a windspeed vector is described. A true airspeed vector of a flying machine is measured while the machine is in flight using one or more nanowires on the flying machine. Each nanowire is configured to measure a value of local air velocity relative to the flying machine. A velocity of the flying machine relative to the ground is measured while the machine is in flight, and then (a) the true airspeed vector is subtracted from (b) the velocity of the flying machine relative to the ground. Other applications are also described.