System and method of using Coriolis mass flow rate meter

A method of measuring fluid flow using a Coriolis mass flow rate meter comprising:

• providing a fluid line connected to the Coriolis mass flow rate meter;
• flowing a fluid through the fluid line;
• providing a first pressure regulator in the fluid line upstream of the Coriolis mass flow rate meter;
• monitoring the regulated pressure in the fluid line downstream of the first pressure regulator;
• venting any air bubbles from the fluid line downstream of the first pressure regulator;
• providing a second pressure regulator in the fluid line downstream of the Coriolis mass flow rate meter;
• monitoring the regulated pressure in the fluid line downstream of the second pressure regulator;
• minimizing the change in pressure across the meter;
• and
• maintaining the second pressure regulator above zero p.s.i.g.

A fuel measurement system for an engine comprising:

• a primary fuel line for carrying fuel;
• a first pressure regulator connected to the primary fuel line for regulating the fuel pressure;
• a first pressure measurement device connected to the primary fuel line downstream of first pressure regulator;
• a vapor tank connected to the primary fuel line downstream of the first pressure measurement device for venting air bubbles from the fuel line;
• a Coriolis fuel measurement meter connected to the primary fuel line downstream of the vapor tank;
• a second pressure regulator connected to the primary fuel line downstream of the Coriolis mass flow rate meter for maintaining the fuel at a pressure greater than zero p.s.i.g. and substantially equal to the fuel pressure at the first pressure regulator;
• and
• a second pressure measurement device connected to the primary fuel line downstream of the second pressure regulator.

A method of measuring fluid flow using a Coriolis mass flow rate meter with a multi-engine fuel measurement system comprising:

• providing a primary fuel line connected to the Coriolis mass flow rate meter;
• supplying pressurized fuel to the primary fuel line upstream of the meter, the fuel having an initial pressure greater than zero p.s.i.g.;
• providing a first pressure regulator downstream of the meter;
• minimizing the change in pressure across the meter;
• connecting a plurality of secondary fuel lines to the primary fuel line downstream of the first pressure regulator in parallel arrangement, each secondary fuel line having an entry valve and a secondary pressure regulator;
• connecting each secondary fuel line to an engine downstream of each secondary fuel line's respective secondary pressure regulator;
• and
• maintaining each secondary pressure regulator at a pressure less than or equal to the fuel pressure at the first pressure regulator and greater than zero p.s.i.g.

A multiple-engine fuel measurement system comprising:

• a fuel source means providing fuel at a pressure substantially above zero p.s.i.g.;
• a primary fuel line for carrying fuel from the fuel source means;
• a Coriolis mass flow rate meter connected to the primary fuel line;
• a filter connected to the primary fuel line upstream of the Coriolis mass flow rate meter;
• a first pressure regulator connected to the primary fuel line downstream of the Coriolis mass flow rate meter for maintaining the fuel pressure above zero p.s.i.g.;
• a plurality of secondary fuel lines arranged in parallel for carrying fuel to each of the multiple engines;
• a plurality of selector valves, each selector valve connected to its respective secondary fuel line;
• a plurality of secondary pressure regulators, each secondary pressure regulator connected to its respective secondary fuel line downstream of the respective selector valve for the respective secondary fuel line and upstream of the respective engine, each of the secondary pressure regulators being set at a certain pressure to simulate that fuel pressure entering the respective engine;
• a plurality of three-way valves, each three-way valve connected to its respective secondary fuel line for supplying and venting fuel to and from the respective engine;
• a plurality of pressure measurement devices, each device connected to its respective secondary fuel line immediately adjacent and upstream of its respective three-way valve;
• and
• a pressure relief valve downstream of the plurality of three-way valves.