Nghĩa của từ turbine engine bằng Tiếng Việt
@Chuyên ngành kỹ thuật
-động cơ tuabi
Đặt câu có từ "turbine engine"
1. Gas turbine engine fuel air mixer
2. A gas turbine engine system includes a gas turbine engine (10) having aerodynamic drag that retards movement.
3. Accessory mechanical drive for a gas turbine engine
4. Gas turbine engine component having vascular engineered lattice structure
5. Gas turbine engine with air-oil cooler oil tank
6. Method for coating turbine engine components with high velocity
7. Acoustic damping system for a combustor of a gas turbine engine
8. Gas turbine engine combustor circumferential acoustic reduction using flame temperature nonuniformities
9. An accessory drive system for an aircraft gas turbine engine is disclosed.
10. Non-streamlined propeller having blades with variable setting for a turbine engine
11. Method for manufacturing a turbine-engine fan casing having an acoustic coating
12. A jet turbine engine may run for 000 hours before being rebuilt.
13. Stiffened hub for unshrouded propeller with variable-pitch blades of a turbine engine
14. Gas turbine engine with system to adjust clearance between rotating and stationary components
15. aeroplanes equipped with a turbine engine (in the case of aircraft-rated organisations);
16. Gas turbine engine two degree of freedom variable bleed valve for ice extraction
17. A method for making a gas turbine engine ceramic matrix composite airfoil is disclosed.
18. Propeller for an aircraft turbine engine including a blade-retaining ring mounted around a hub
19. The invention is applicable to controlling the pitch of the blades of a turbine engine propeller.
20. — aircraft structural failure or engine disintegration, including uncontained turbine engine failures, not classified as an accident,
21. aircraft structural failure or engine disintegration, including uncontained turbine engine failures, not classified as an accident,
22. - Aircraft structural failure or engine disintegration, including uncontained turbine engine failures, not classified as an accident.
23. Process and tool for aligning a seal housing assembly with a casing of a gas turbine engine
24. Fairing for a pylon via which a turbine engine is suspended from a wing of an aircraft.
25. Apparatus for acoustic damping and operational control of damping, cooling, and emissions in a gas turbine engine
26. Fairing for a pylon via which a turbine engine is suspended from a wing of an aircraft
27. An aircraft comprises a turbine engine (104) suspended from a wing (102) by means of a pylon (105).
28. Intermediate casing for an aircraft turbine engine, comprising structural connecting arms that perform separate mechanical and aerodynamic functions
29. First, sunlight may be used to heat a liquid that produces steam, which, in turn, drives a turbine engine.
30. Rotor in a turbine engine coupled to provide individual and separate access to respective assemblies of compressor and turbine disks
31. Sunlight may, for example, be used to heat a liquid that produces steam, which, in turn, drives a turbine engine.
32. an acceptable level of turbine engine reliability is achieved in service by the world fleet for the particular airframe-engine combination;
33. (a) an acceptable level of turbine engine reliability is achieved in service by the world fleet for the particular airframe-engine combination;
34. The fuel injector includes an active cooling system that insulates fuel flowing through the fuel injector from heat energy within the turbine engine.
35. Their goal was to develop an aero-thermodynamic turbine engine design resulting in reduction in engine weight, time-to-market, costs and emissions.
36. Theoretical modelling predictions of the aero thermal, aeromechanical and combustion conditions, which have been validated with actual aero gas turbine engine (experimental or production) performance data.
37. 2. Theoretical modelling predictions of the aero thermal, aeromechanical and combustion conditions, which have been validated with actual aero gas turbine engine (experimental or production) performance data.
38. Hawkeye rigid, flexible and video Borescopes, videoscopes, and Borescope accessories for visual and video inspection of metal machined parts, castings, welds, and for aircraft and turbine engine service and maintenance
39. For ten years the company has partnered training programs with the National Aerotechnics School of Collège Édouard-Montpetit, particularly for college-level training in aircraft engine maintenance and turbine engine inspection.
40. Woodward provides complete Actuation system design, analysis, and testing across a wide range of turbine engine applications: engine start, variable geometry, thermal management, turbine clearance control, engine operability, and compressor bleed applications
41. The helicopter used for the Breakout scene is an Aerospatiale SA.313/318 Alouette II powered by a gas turbine engine, whilst the sound was dubbed from a Bell 47 piston-engine helicopter
42. A gas turbine engine (10) internal fuel manifold (22) has a plurality of airblast fuel nozzles (26) in communication with an air source such that nozzle core air does not pass through the manifold (22).
43. a. Nickel alloys (Ni-Al-X, Ni-X-Al) qualified for turbine engine parts or components, i.e. with less than 3 non-metallic particles (introduced during the manufacturing process) larger than 100 μm in 109 alloy particles;
44. Aeroshell Be it aircraft piston engine oils, turbine engine oils, greases or hydraulic fluids, Aeroshell has one of the most comprehensive and proven range of aviation lubricant products, combined with one of the best technical support in the industry.
45. Turbine engine components, namely turbine blades, fans, shafts, combustion chambers, compressors, afterburners and nozzles, exhaust nozzles and manifolds, disks, shrouds, airfoils, and impellers, engine mounts, fuel injection systems, lift fan clutches and drive shafts, nacelles, inlets, cowls, thrust reversers, exhaust nozzles, and air intake inlets
46. The speed of a high-pressure turbine of a gas turbine engine may be determined using known centrifugal pump affinity relationships for a fuel pressure apparatus, fuel pressure apparatus input and output pressures, and gear ratios for a mechanical linkage between the high-pressure turbine and the fuel pressure apparatus.
47. @article{osti_6232977, title = {Circumferentially area ruled duct}, author = {Matthews, J A and Striebel, E E and Sepulveda, D and Pane, V and Pane, Jr, F C}, abstractNote = {In combination, a gas turbine engine is described having a burner for receiving a working medium, an annular diffuser with an inner conically shaped wall and an outer conically shaped wall diverging relative to each other