Borescope inspection port device for gas turbine engine and gas turbine engine using same
First Claim
1. An adapter to permit borescope access inside a gas turbine engine having an outer casing and including a compressor stator having at least one compressor stator segment, the adapter comprising:
- a body portion defining a bore extending longitudinally therethrough from a first end to be disposed adjacent to outside surfaces of the outer casing to a second end to be disposed adjacent to an inside surface of the at least one compressor stator segment, the bore permitting a borescope to enter therethrough; and
an attachment portion for circumferentially coupling the at least one compressor stator segment to the outer casing.
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Accused Products
Abstract
An adapter to permit borescope access inside a gas turbine engine including a compressor stator having a plurality of compressor stator segments comprises a body portion defining a bore extending longitudinally therethrough from a first end to be disposed adjacent to outside surfaces of adjacent compressor stator segments to a second end to be disposed adjacent to inside surfaces of adjacent compressor stator segments. The bore permits a borescope to enter therethrough. The adapter further comprises an attachment portion for circumferentially coupling at least one compressor stator segment to an outer casing of the gas turbine engine.
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Citations
21 Claims
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1. An adapter to permit borescope access inside a gas turbine engine having an outer casing and including a compressor stator having at least one compressor stator segment, the adapter comprising:
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a body portion defining a bore extending longitudinally therethrough from a first end to be disposed adjacent to outside surfaces of the outer casing to a second end to be disposed adjacent to an inside surface of the at least one compressor stator segment, the bore permitting a borescope to enter therethrough; and an attachment portion for circumferentially coupling the at least one compressor stator segment to the outer casing. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10)
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11. A gas turbine engine comprising:
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a compressor section having an outer casing and including a compressor stator and rotor, the compressor stator including a plurality of compressor stator segments; a combustion section communicating with and disposed downstream of the compressor section relative to a direction of airflow; a gas turbine section communicating with and disposed downstream of the combustion section relative to a direction of airflow; and an adapter circumferentially coupling at least one of the compressor stator segments to the outer casing, the adapter including a body portion defining a bore extending therethrough from at least an outside surface to an inside surface of an associated compressor stator segment, the bore permitting a borescope to enter therethrough. - View Dependent Claims (12, 13, 14, 15, 16, 17, 18, 19, 20, 21)
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Specification