Search results
Results from the WOW.Com Content Network
Supervised injection sites are also known as overdose prevention centers (OPCs), [6] supervised injection facilities, [7] safe consumption rooms, [8] safe injection sites, [1] safe injection rooms, [9] fix rooms, [10] fixing rooms, [11] safer injection facilities (SIF), drug consumption facilities (DCF), [2] drug consumption rooms (DCRs), [12] medically supervised injecting centres (MSICs) and ...
OnPoint NYC is a New York City nonprofit that operates two privately run safe injection sites (also known as Overdose Prevention Centers) in East Harlem and Washington Heights. [2] Placed at the sites of existing syringe service programs , [ 3 ] these were America's first safe injection facilities when they opened in November 2021.
Insite is a supervised drug injection site in the Downtown Eastside (DTES) neighbourhood of Vancouver, British Columbia, Canada [1] The DTES had 4,700 chronic drug users in 2000 and has been considered to be the centre of an "injection drug epidemic". The site provides a supervised and health-focused location for injection drug use, primarily ...
The GE Passport is a high bypass ratio turbofan. The engine is a twin-spool, axial-flow turbofan with a high bypass ratio of 5.6:1 and an overall pressure ratio of 45:1. The front fan is attached to the three-stage low-pressure compressor; the 23:1 pressure ratio 10-stage high-pressure compressor includes five blisk stages for weight reduction.
There is an axial combustion chamber between the compressor stages and the HP turbine. A mixer is built in to the jetpipe to mix cold bypass air with the hot exhaust gases. The engine has an overall pressure ratio of 35:1, which is extremely high for an engine with a
The engines involved in the July and September incidents had 154 and 230 cycles, respectively, while the October failure occurred to an engine with 1,654 cycles since new but within 300 cycles after an electronic engine-control update. Pratt & Whitney recommends inspections on engines with up to 300 cycles after the update.
The Honeywell/ITEC F124 is a low-bypass turbofan engine derived from the civilian Honeywell TFE731.The F125 is an afterburning version of the engine. The engine began development in the late 1970s for the Republic of China (Taiwan) Air Force AIDC F-CK Indigenous Defence Fighter (IDF), and it first ran in 1979.
The F118 is a non-afterburning derivative of the F110 specially developed for the B-2 Spirit stealth bomber. A single stage HP turbine drives the 9 stage HP compressor, while a 2-stage LP turbine drives the 3 stage fan.