gas turbine in English
Initially the pressure of the Zechstein gas would be sufficiently high pressure, at the well heads, to supply fuel gas for the compressor gas turbine .
Use "gas turbine" in a sentence
1. Blade for gas turbine
2. Split-flow recirculating gas turbine
3. Burner for a gas turbine and method for reducing thermo-acoustic oscillations in a gas turbine
4. Gas turbine compressor cleaning units
5. Gas turbine engine fuel air mixer
6. A gas turbine engine system includes a gas turbine engine (10) having aerodynamic drag that retards movement.
7. Gas turbine, particularly an aircraft engine
8. Gas turbine aero engine afterbody assembly
9. Combustion chamber arrangement for damping thermo-acoustic oscillations, gas turbine and method of operating such a gas turbine
10. Gas turbine system having exhaust gas recirculation
11. Blade tip sealing apparatus for gas turbine
12. The present invention relates to a gas turbine.
13. Accessory mechanical drive for a gas turbine engine
14. Gas turbine engine component having vascular engineered lattice structure
15. Gas turbine engine with air-oil cooler oil tank
16. Gas turbine burner assembly equipped with a helmholtz resonator
17. Aero gas turbine engines having any of the following:
18. The gas turbine also keeps the batteries topped up.
19. In order to reduce gas turbine disk stress, an optimal material removal area is defined according to blade and/or disk geometry to maximize a balance between stress reduction on the gas turbine disk, a useful life of the gas turbine blade, and maintaining or improving the aeromechanical behavior of the gas turbine blade.
20. Closed-loop control for a gas turbine with actively stabilized compressor
21. Acoustic damping system for a combustor of a gas turbine engine
22. The invention relates to a gas turbine, especially an aircraft engine.
23. Aftermarket services for gas turbine engines, namely, overhaul repair maintenance services
24. Gas turbine engine combustor circumferential acoustic reduction using flame temperature nonuniformities
25. A premixing injector for use in gas turbine engines assists in the lean premixed injection of a gaseous fuel/air mixture into the combustor of a gas turbine.
26. Gas turbine including blade tip gap adjusting means and control method therefor
27. An accessory drive system for an aircraft gas turbine engine is disclosed.
28. The present invention relates to an airfoil (100) for a gas turbine.
29. They were the first gas turbine powered ships in the Soviet navy.
30. Gas turbine engine two degree of freedom variable bleed valve for ice extraction
31. Partial-load operation of a gas turbine with an adjustable bypass flow channel
32. Gas turbine engine with system to adjust clearance between rotating and stationary components
33. The batteries are charged on-board by a small gas turbine auxiliary propulsion unit.
34. A method for making a gas turbine engine ceramic matrix composite airfoil is disclosed.
35. Method for mounting a mixing housing in a gas turbine, and adjusting device therefor
36. The Gas Turbine Research Establishment was to indigenously develop the Kaveri engine to power the LCA .
37. 9A001 Aero gas turbine engines incorporating any of the "technologies" specified in 9E003.a., as follows:
38. specially designed to predict aero thermal, aeromechanical and combustion conditions in aero gas turbine engines; and
39. The invention relates to a device for the adjustment of guide blades of a gas turbine.
40. Non-civil certified aircraft; all aero gas turbine engines; unmanned aerial vehicles; and parts and components
41. NRC Aerospace engineers, pilots and technicians test structures and components, new materials and gas turbine engines.
42. Specially designed to predict aero thermal, aeromechanical and combustion conditions in aero gas turbine engines; and
43. As turbine-driven air compressors driven by an exhaust-gas turbine, they fall in heading 8414.
44. Method and device for operating a burner of a heat engine, especially a gas turbine plant
45. Note: 9A001.a. does not control aero gas turbine engines which meet all of the following:
46. Note 1: 9A001.a. does not control aero gas turbine engines which meet all of the following:
47. The Gas Turbine Research Establishment was entrusted with the task of designing the engine for the LCA .
48. The contract pertained to the repair, overhaul and modification of Allison T56 gas turbine engines for aircraft.
49. But not including aircraft engines, gas turbine engines for aircraft, and parts and fittings for these goods
50. Apparatus for acoustic damping and operational control of damping, cooling, and emissions in a gas turbine engine