jet pipe การใช้
- Smoke belched from its jet pipe and flames enveloped the tail section.
- As this temperature cannot reliably be measured, the operating limits are determined by jet pipe temperature.
- The primary exhaust nozzle and jet pipe were designed for a life of 30, 000 hours.
- Official interest had also been cooled by the expression of doubts voiced by Rolls-Royce Limited on the viability of the bifurcated jet pipes that the design used.
- The aircraft had the ability to perform a " dump and burn " which involved dumping fuel from an outlet between the engine jet pipes and igniting it with the engine s afterburners.
- Hawker Aircraft also submitted a proposal, for a swept-wing, swept-tail fighter based on the Hawker P . 1052, but using a straight-through jet pipe could be installed.
- Further improvement of the equipment for hydro-slotting perforation must follow the scientific and technical progress in this technology, not on the way of mindless increase of the holes in the hydro jets pipe.
- Ten spiral ducts connected the compressor outlet to a single, large, reverse-flow combustion chamber, the outlet of which discharged forward through the turbine before turning rearwards to exhaust through ten jet pipes.
- "Two 20 feet [ 6.1 m ] circumference brake parachutes and one 20 feet [ 6.1 m ] anti-spin parachute . . . housed in the rear fuselage above the jet pipe ."
- The use of a twin boom enabled the jet pipe to be kept relatively short, which avoided the power loss that would have occurred if a long pipe was used, as would have been necessary by a conventional fuselage.
- Also, acoustic sources within the " jet pipe " also contribute to the noise, mainly at lower speeds, which include combustion noise and sounds produced by interactions of a turbulent stream with fans, compressors, and turbine systems.
- The nose undercarriage rotated 90?to lie flat under the forward engine, and the twin wheeled main undercarriage legs, with long travel levered suspension, retracted into the centre fuselage above the forward jet pipe and astride the fuel tank and intake trunking for the rear engine.
- Power was supplied by a Shenyang Aircraft Development Office PF-1A, ( Chinese copy of the Klimov RD-500 / Rolls-Royce Derwent ), centrifugal compressor turbojet fitted in the centre fuselage, exhausting through a jet pipe extending to the tail of the fuselage.
- Two jet pipe / rear fuselage arrangements were also originally considered due to the potential loss of thrust through the jet pipe itself : a'short jet'with a cutaway rear fuselage and short exhaust necessitating the tailplane to be carried on booms, and a'long jet'with a fully enclosed jet pipe; the'long jet'was subsequently selected.
- Two jet pipe / rear fuselage arrangements were also originally considered due to the potential loss of thrust through the jet pipe itself : a'short jet'with a cutaway rear fuselage and short exhaust necessitating the tailplane to be carried on booms, and a'long jet'with a fully enclosed jet pipe; the'long jet'was subsequently selected.
- Two jet pipe / rear fuselage arrangements were also originally considered due to the potential loss of thrust through the jet pipe itself : a'short jet'with a cutaway rear fuselage and short exhaust necessitating the tailplane to be carried on booms, and a'long jet'with a fully enclosed jet pipe; the'long jet'was subsequently selected.