Engine · 277 questions
Gas Turbines - USCG Exam Questions
Gas turbine theory, construction, operation, and the support systems found in gas turbine propulsion plants.
Every question below is a real U.S. Coast Guard exam question with four choices. Answer one and the correct choice is revealed instantly, with the USCG reference and illustration where the question uses one.
All Gas Turbines questions
Questions 201–277 of 277 · page 3 of 3
- #471 In order to get a ready indication for a normal start with an GE LM2500 gas turbine engine, what permissive(s) must be met?
- #472 For the GE LM2500 gas turbine engine shown in the illustration, the HP turbine 2nd stage nozzle vanes are cooled by which of the following? Illustrati... illustration
- #473 For the GE LM2500 gas turbine engine shown in the illustration, the HP turbine 2nd stage blades are cooled by convection, with the cooling air being d... illustration
- #474 In the ignition system of a gas turbine engine, how is optimum spark achieved?
- #475 What is the power source for the ignition exciter of a gas turbine engine?
- #476 What is the most common type of spark igniter used on a gas turbine engine?
- #477 When removing the gas turbine engine as shown in the illustration, how is the engine removal accomplished? Illustration GT-0022 illustration
- #478 A gas turbine engine’s main lube oil system pump check valve serves to maintain system prime and perform what other function?
- #479 How is the lube oil supplied to each bearing in a gas turbine engine controlled?
- #480 The electrostatic vent fog precipitator removes oil mist from which of the following areas?
- #481 When the main reduction gear lube oil system is secured, which of the following components maintains the air within the casing at less than 35 percent...
- #482 For the gas turbine engine lube oil system shown in the illustration, what is the purpose of the lube oil supply check valves? Illustration GT-0024 illustration
- #483 The lube oil scavenge pressure on the marine gas turbine shown in the illustration is sensed by which of the following? Illustration GT-0017 illustration
- #484 Which of the following are the principle factors that affect the performance of a gas turbine compressor?
- #485 Compressor characteristics are normally summarized in the form of which of the following?
- #486 On a vessel equipped with propulsion gas turbines, the operators initial response to a high vibration alarm should be which of the following?
- #487 As shown in the illustration, what is the purpose of pressurizing the main bearing lube oil sumps on a typical marine gas turbine? Illustration GT-002... illustration
- #488 On the gas turbine engine lube oil system shown in the illustration, air and oil are primarily separated in the air/oil separator through the use of w... illustration
- #489 On the marine gas turbine engine shown in the illustration, the 8th stage bleed air is used for which of the following? Illustration GT-0017 illustration
- #490 The lube oil system shown in the illustration, consists of which of the following sub-systems? Illustration GT-0024 illustration
- #491 Which of the following conditions permits a gas turbine to produce 100% power?
- #492 How do you gain access to the burner units of a can-annular combustor to perform maintenance?
- #493 Boyle's law can best be defined as which of the following?
- #494 In the operation of a marine propulsion gas turbine, kinetic and thermal energy required to drive the main propeller shaft are extracted by which of t...
- #495 The effectiveness of an off-line wash wash of a LM2500 gas turbine engine can be enhanced by doing which of the following?
- #496 Zero reference for the GE LM2500 gas turbine engine is established by the use of which of the following engine components?
- #497 On an GE LM2500 gas turbine powered vessel you are conducting a borescope inspection of the compressor. What is used on each compressor stage as a ref...
- #498 What type of gas turbine cycle configuration is shown in the illustration? Illustration GT-0031 illustration
- #499 What type of metallurgical failure does Item B represent in the illustration? Illustration GT-0014 illustration
- #500 You are conducting a borescope inspection of the compressor section of a GE LM2500 gas turbine. In stage four, you see a slight tilt to one blade and...
- #501 When tip clang takes place on a gas turbine engine, the major damage occurs to what area of the blade?
- #502 What type of metallurgical failure does Item A represent in the illustration? Illustration GT-0014 illustration
- #503 You are conducting a borescope inspection of the combustor section of a GE LM2500 gas turbine engine. You observe a one square inch hole in the combus...
- #504 What does the term "lockout" of a Synchro-Self-Shifting (SSS) clutch system mean? Illustration GT-0018 illustration
- #505 How is the clutch shown in the attached illustration engaged? Illustration GT-0018 illustration
- #506 What is the primary purpose of the diffuser and distributor on the GE LM2500 gas turbine engine?
- #507 What is the purpose of the GE LM2500 gas turbine enclosure heater?
- #508 What type of combustor is used by the GE LM2500 gas turbine engine?
- #509 Where are the CO2 nozzles located in the GE LM2500 gas turbine enclosure?
- #510 The gas generator section of the GE LM2500 gas turbine engine is composed of all of the following components EXCEPT for which of the following?
- #511 How many stages are in the HP turbine of the GE LM2500 gas turbine engine?
- #512 The struts of the compressor front frame provide passages for all of the following mediums EXCEPT for which of the following?
- #513 The power turbine (PT) of the GE LM2500 gas turbine engine has a total of how many stages?
- #514 How is the HP turbine rotor of the GE LM2500 gas turbine engine cooled?
- #515 If after reducing power to a gas turbine engine in response to a high lube oil supply temperature alarm, the temperature continues to rise, your next...
- #516 What type of main lube oil supply and scavenging pump is installed on the marine gas turbine engine shown in the illustration? Illustration GT-0017 illustration
- #517 What action should you take if full power vibration limits are exceeded on a gas turbine engine?
- #518 The build-up of contamination in a gas turbine will cause all of the following conditions EXCEPT which of the following?
- #519 Why is safety-wiring, or lock wiring of gas turbine parts required?
- #520 You are preparing for a borescope inspection of a gas turbine engine. Prior to the inspection it is recommended that you do which of the following?
- #521 To manually rotate the GE LM2500 gas turbine engine, you should use which of the following tools?
- #522 The lubrication principal used by the Kingsbury thrust bearing is which of the following?
- #523 The purpose of the main reduction gear in a marine gas turbine propulsion installation is which of the following?
- #524 On the marine gas turbine shown in the illustration, the gas generator speed sensor is located where? Illustration GT-0017 illustration
- #525 Cadmium and zinc coatings provide which of the following type of protection for the base metal?
- #526 When dissimilar metals come in contact with a conductor, which of the following types of metal deterioration takes place?
- #527 The two main types of "compressor" stalls are known as which of the following?
- #528 In cases where both the pinion and gear teeth of the main reduction gear have been slightly indented by foreign material, what action should you take?
- #529 On the marine gas turbine engine panel shown in the illustration, which of the following conditions would prevent the auto-start sequence from success... illustration
- #530 The purpose of the air shroud (swirl cup) around the tip of the fuel nozzle of an GE LM2500 gas turbine engine is which of the following?
- #531 How many fuel igniters would be installed on the marine gas turbine engine shown in the illustration? Illustration GT-0017 illustration
- #532 The fuel oil back pressure regulator on the fuel system shown in the illustration, returns fuel to the which of the following? Illustration GT-0021 illustration
- #533 The secondary passages on the gas turbine engine fuel nozzles shown in the illustration are designed to open at approximately what pressure? Illustrat... illustration
- #534 What is the primary function of the main fuel control on the GE LM2500 gas turbine engine?
- #535 As shown in the illustration of a gas turbine fuel oil system, when the engine fuel oil valves are de-energized, the remaining fuel left in the system... illustration
- #536 You are preparing for a borescope inspection of a GE LM2500 gas turbine engine. You are reviewing the correct geometric orientation nomenclature which...
- #537 When conducting a borescope inspection, you must be aware of all of the following factors EXCEPT which?
- #538 The six borescope ports located in the compressor rear frame casing of the marine propulsion gas turbine shown, can be used to inspect all EXCEPT whic... illustration
- #539 While underway on a ship with gas turbine engines, the most likely indication of an engine stall is which of the following?
- #540 To prevent overheating of the illustrated turbine blade, which of the following fluids is circulated through it via the shaped internal passages? Illu... illustration
- #541 As shown in the illustration, the HP turbine 2nd stage blades are cooled by convection, with the cooling air being discharged at which of the followin... illustration
- #542 In the marine gas turbine engine shown in the illustration, the 9th stage bleed air is used for which of the following? Illustration GT-0017 illustration
- #543 In the marine gas turbine engine shown in the illustration, the 13th stage bleed air is used for which of the following? Illustration GT-0017 illustration
- #544 In the marine gas turbine engine shown in the illustration, the HP turbine 2nd stage nozzle vanes are cooled by which of the following? Illustration G... illustration
- #545 In order to get a ready indication for a normal start with a GE LM2500 marine gas turbine, what permissive(s) must be met?
- #546 Your first step in response to a gas turbine engine high lube oil sump temperature alarm would be which of the following?
- #547 Which of the following is the most probable cause for the sump oil to be excessively aerated on an aero-derivative main propulsion gas turbine engine?
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