Turbine overspeed protection
US-2024368999-A1 · Nov 7, 2024 · US
US9322332B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9322332-B2 |
| Application number | US-201313788906-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 7, 2013 |
| Priority date | Mar 21, 2012 |
| Publication date | Apr 26, 2016 |
| Grant date | Apr 26, 2016 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
This invention relates to an internal combustion engine having a cavity for inspection, comprising: an inspection device mounted within a housing, the housing at least partially located within the cavity to be inspected and having a shutter which is actuable between a closed configuration and an open configuration; and an actuation mechanism for moving the shutter between the closed configuration and the open configuration.
Opening claim text (preview).
The invention claimed is: 1. An internal combustion engine having a cavity for inspection, comprising: an inspection device mounted within a housing, the housing at least partially located adjacent the cavity to be inspected and having a shutter which is actuable between a closed configuration and an open configuration, wherein the inspection device is retractable between a stowed position and an inspection position; and an actuation mechanism for moving the shutter between the closed configuration and the open configuration, wherein the shutter is configured to be actuated by the inspection device when the inspection device is moved between the stowed and inspection positions. 2. An internal combustion engine as claimed in claim 1 , wherein the inspection device is configured to allow visual inspection of the cavity. 3. An internal combustion engine as claimed in claim 1 , wherein the shutter is retractably stowed within the housing when in the closed configuration and actuated into the cavity so as to expose the inspection device when in the open configuration. 4. An internal combustion engine as claimed in claim 1 , wherein the shutter includes a cleaning device for cleaning the inspection device. 5. An internal combustion engine as claimed in claim 1 , wherein the shutter and inspection device are simultaneously actuable. 6. An internal combustion engine as claimed in claim 1 , wherein the actuation mechanism is one taken from the group including pneumatic, hydraulic or electrical. 7. An internal combustion engine as claimed in claim 1 , wherein the housing is at least partially formed within a wall of the cavity. 8. An internal combustion engine as claimed in claim 1 , wherein the cavity includes moving parts of the internal combustion engine. 9. An internal combustion engine as claimed in claim 1 , wherein the shutter includes a cup shaped shield, the cup shaped shield having an internal chamber which fits over and receives the inspection device when in the stowed position. 10. An internal combustion engine as claimed in claim 1 , wherein the shutter includes at least one shutter plate which is biased against a restraining element so as to retain the shutter plate in place when in a closed configuration, and where actuating the shutter from the closed configuration to the open configuration includes moving the shutter plate relative to the restraining element such that the bias results in the inspection device being exposed to the cavity. 11. An internal combustion engine as claimed in claim 1 , wherein the shutter includes first and second shutter plates. 12. An internal combustion engine as claimed in claim 1 , wherein the internal combustion engine is a gas turbine engine. 13. An aircraft having the internal combustion engine as claimed in claim 1 . 14. An aircraft as claimed in claim 13 , wherein the actuation mechanism is operable from the cockpit of an aircraft or as part of an engine health monitoring system. 15. An internal combustion engine having a cavity for inspection, comprising: an inspection device mounted within a housing, the housing at least partially located adjacent the cavity to be inspected and having a shutter which is actuable between a closed configuration and an open configuration, wherein the inspection device is retractable between a stowed position and an inspection position; and an actuation mechanism for moving the shutter between the closed configuration and the open configuration, wherein the shutter includes a cup shaped shield, the cup shaped shield having an internal chamber which fits over and receives the inspection device when in the stowed position.
Diagnostics · CPC title
Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants (controlling F02C9/00) · CPC title
Arrangements for testing or measuring (for measuring vibrations G01H) · CPC title
Optical devices · CPC title
Inspecting the inner surface of hollow bodies, e.g. bores · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.