1
Graham David James: Gas turbines and engines. Boc Group, October 5, 1983: GB2117053-A (70 worldwide citation)

The combustion chambers 30 of gas turbine units 6(a) to 6(c) (or equivalent piston engines) are supplied with fuel gas via pipe 26 and in order to compensate for a substantial decline in the calorific value of the fuel gas over a period of time, commercially pure oxygen or oxygen-enriched air is sup ...


2
Hideki Ogata: Fuel supply device of gas turbine engine. KAWASAKI JUKOGYO KABUSHIKI KAISHA, Sughrue Mion PLLC, January 31, 2017: US09556797

A fuel divider included in a fuel supply device of a gas turbine engine includes a movable member which is movable according to a fuel pressure at a fuel entrance, opens only a pilot port when the fuel pressure at the fuel entrance is lower than a first pressure, and opens both of the pilot port and ...


3
Song Yali: Three-dimensional combined type ocean energy utilization power generation method. Song Yali, October 27, 2010: CN201010193469

The invention discloses a three-dimensional combined type ocean energy utilization power generation method. A system consisting of n wind power air compressors, m floating box direct supply type air compressors, air collection pipelines, compressed air storage tanks, compressed air gas turbines and ...


4
Method For Operating A Gas Sensor For Improving The Detection Of Nitrogen Oxides. Siemens Aktiengesellschaft, July 27, 2017: US20170212073-A1

A gas sensor for detecting nitrogen oxides in a gas mixture may include at least two electrodes of the same material arranged on an oxygen ion conductor. When the gas sensor is operated, both electrodes come into contact with the gas mixture. The gas sensor is then heated from a first temperature to ...


5
EXHAUST GAS TREATMENT DEVICE AND NOZZLE FOR THE SAME. March 29, 2018: US20180087423-A1

A nozzle (1) includes a nozzle body (10), a piston (2) movably disposed inside the nozzle body (10), and a spring (3) between the nozzle body (10) and the piston (2). A reducing agent flow channel (12) extends between a nozzle inlet (11) and a nozzle orifice (14), which widens towards a nozzle openi ...