1. Gas turbine system having exhaust gas recirculation

2. Blade for gas turbine

3. Adjustable diffuser for a turbine, turbine for an exhaust gas turbocharger and exhaust gas turbocharger

4. Split-flow recirculating gas turbine

5. Burner for a gas turbine and method for reducing thermo-acoustic oscillations in a gas turbine

6. Gas turbine compressor cleaning units

7. Gas turbine engine fuel air mixer

8. Adjustable diffuser for a turbine of an exhaust-gas turbocharger, and turbine for an exhaust-gas turbocharger

9. A gas turbine engine system includes a gas turbine engine (10) having aerodynamic drag that retards movement.

10. Gas turbine, particularly an aircraft engine

11. Gas turbine aero engine afterbody assembly

12. Combustion chamber arrangement for damping thermo-acoustic oscillations, gas turbine and method of operating such a gas turbine

13. Blade tip sealing apparatus for gas turbine

14. The present invention relates to a gas turbine.

15. Accessory mechanical drive for a gas turbine engine

16. Gas turbine engine component having vascular engineered lattice structure

17. As turbine-driven air compressors driven by an exhaust-gas turbine, they fall in heading 8414.

18. Gas turbine engine with air-oil cooler oil tank

19. Gas turbine burner assembly equipped with a helmholtz resonator

20. Aero gas turbine engines having any of the following:

21. The gas turbine also keeps the batteries topped up.

22. 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.

23. Turbine system with exhaust gas recirculation and absorption refrigeration system

24. Turbine blade which can be exposed to a hot gas flow

25. Closed-loop control for a gas turbine with actively stabilized compressor

26. Acoustic damping system for a combustor of a gas turbine engine

27. The invention relates to a gas turbine, especially an aircraft engine.

28. Aftermarket services for gas turbine engines, namely, overhaul repair maintenance services

29. Gas turbine engine combustor circumferential acoustic reduction using flame temperature nonuniformities

30. 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.

31. Gas turbine including blade tip gap adjusting means and control method therefor

32. An accessory drive system for an aircraft gas turbine engine is disclosed.

33. It manufactures power turbines for electricity and heat generation, gas compressor units and marine gas-turbine units.

34. The present invention relates to an airfoil (100) for a gas turbine.

35. They were the first gas turbine powered ships in the Soviet navy.

36. Turbine having an axially displaceable adjusting element for an exhaust-gas turbocharger

37. Gas turbine engine two degree of freedom variable bleed valve for ice extraction

38. Partial-load operation of a gas turbine with an adjustable bypass flow channel

39. Gas turbine engine with system to adjust clearance between rotating and stationary components

40. Centrifugal compressors are used in small gas turbine engines or as the final compression stage of medium-sized gas turbines.

41. The batteries are charged on-board by a small gas turbine auxiliary propulsion unit.

42. A method for making a gas turbine engine ceramic matrix composite airfoil is disclosed.

43. Method for mounting a mixing housing in a gas turbine, and adjusting device therefor

44. The Gas Turbine Research Establishment was to indigenously develop the Kaveri engine to power the LCA .

45. 9A001 Aero gas turbine engines incorporating any of the "technologies" specified in 9E003.a., as follows:

46. specially designed to predict aero thermal, aeromechanical and combustion conditions in aero gas turbine engines; and

47. The invention relates to a device for the adjustment of guide blades of a gas turbine.

48. Non-civil certified aircraft; all aero gas turbine engines; unmanned aerial vehicles; and parts and components

49. NRC Aerospace engineers, pilots and technicians test structures and components, new materials and gas turbine engines.

50. Specially designed to predict aero thermal, aeromechanical and combustion conditions in aero gas turbine engines; and

51. The pressure of the gas or fluid changes as it passes through the turbine rotor blades.

52. The no machining directional solidification hollow turbine blades, hollow guide vans and complex structure parts used in aero engine and gas turbine made by vacuum precision investment casting.

53. Method and device for operating a burner of a heat engine, especially a gas turbine plant

54. Note: 9A001.a. does not control aero gas turbine engines which meet all of the following:

55. Note 1: 9A001.a. does not control aero gas turbine engines which meet all of the following:

56. The Gas Turbine Research Establishment was entrusted with the task of designing the engine for the LCA .

57. The contract pertained to the repair, overhaul and modification of Allison T56 gas turbine engines for aircraft.

58. But not including aircraft engines, gas turbine engines for aircraft, and parts and fittings for these goods

59. The invention relates to a turbine blade (9) which can be exposed to a hot gas flow.

60. Apparatus for acoustic damping and operational control of damping, cooling, and emissions in a gas turbine engine

61. 1. Specially designed to predict aero thermal, aeromechanical and combustion conditions in aero gas turbine engines; and

62. Process and tool for aligning a seal housing assembly with a casing of a gas turbine engine

63. Turbine blades and turbine vanes

64. An exhaust gas treatment system for a turbine unit, wherein an exhaust gas recirculation line comprises a gas cooling and cleaning device having a packed bed for contacting the exhaust gas with a cooling and absorption liquid.

65. 1. being specially designed to predict aero thermal, aeromechanical and combustion conditions in aero gas turbine engines; and

66. Said drag device (33) leads a gas turbine blade on a carrier arm (41) through the abrasive medium (27).

67. The invention relates to a device for adjusting guide blades of a turbo drive gear, especially a gas turbine.

68. Wärtsilä’s Competitors in power generation comprise equipment manufacturers of internal combustion engine and gas turbine technologies

69. To improve the reliability of gas turbines for power generation was the aim of the EU-funded 'Limit cycles of thermo-acoustic oscillations in gas turbine combustors' (LIMOUSINE) project.

70. Vapour Aluminising or out-of-pack Aluminising is a major production technique for producing aluminide coatings on gas turbine parts

71. Turbine blade for a water turbine with bi-directional flow

72. The burner permits the reduction of thermo-acoustic oscillations in a combustion chamber on a gas turbine in an alternative way.

73. Method for optimizing the contact surfaces of shroud segments, which abut against one another, of adjacent blades of a gas turbine

74. The invention relates to a method for repairing turbine vanes of a gas turbine, said method comprising the following steps: a) a turbine vane comprising, at least in sections, a PtAl coating to be repaired, is provided, b) the turbine vane is cleaned in at least the region of the PtAl coating to be repaired, c) and the turbine vane is alited only in the region of the cleaned PtAl coating.

75. The Capitol Power Plant's Cogeneration system will use natural gas in a combustion turbine to generate electricity and heat, increasing system

76. In modern gas-turbine helicopters, much of this work has been reduced by the introduction of an engine speed governing system.

77. AEROPLANES TURBINE (**)

78. Turbine failure?

79. Wind turbine device

80. Almost all of the modern gas turbine engines use Annular combustors; likewise, most combustor research and development focuses on improving this type