In-cylinder imaging system using high-speed imaging device and high intensity light source for capturing images in combustion chamber
An in-cylinder imaging apparatus is provided for an internal combustion engine defining a combustion chamber. The in-cylinder imaging apparatus includes a high-speed imaging device such as a high-speed digital camera. A borescope is provided in communication with the combustion chamber and is operable to communicate images of the combustion chamber to the high-speed imaging device. A high intensity light source, for example, a xenon light source, is operable to substantially illuminate the combustion chamber. The high-speed imaging device and borescope are in axial alignment with respect to each other and are mounted with respect to the internal combustion engine. A method of imaging the combustion chamber of the internal combustion engine during engine operation employing the disclosed in-cylinder imaging apparatus is also provided.
1. An in-cylinder imaging apparatus for an internal combustion engine defining a combustion chamber, said in-cylinder imaging apparatus comprising:
a high-speed imaging device;
a borescope in optical communication with the combustion chamber and operable to communicate images of the combustion chamber to said high-speed imaging device;
a high intensity light source operable to substantially illuminate the combustion chamber; and
wherein said high-speed imaging device and said borescope are mounted with respect to the internal combustion engine.
2. The in-cylinder imaging apparatus of claim 1 , wherein said high-speed imaging device and said borescope are axially aligned.
3. The in-cylinder imaging apparatus of claim 1 , further comprising a protective window disposed between said borescope and the combustion chamber.
4. The in-cylinder imaging apparatus of claim 3 , wherein said protective window is formed from at least one of quartz, spinel, and sapphire.
5. The in-cylinder imaging apparatus of claim 1 , wherein said high-speed imaging device is a high-speed digital camera.
6. The in-cylinder imaging apparatus of claim 1 , wherein said borescope is cooled with chilled and compressed gas.
7. The in-cylinder imaging apparatus of claim 1 , further comprising a bracket operable to mount said high-speed imaging device to said engine.
8. The in-cylinder imaging apparatus of claim 7 , wherein said bracket has natural frequency modes greater than an inducing function of the internal combustion engine.
9. The in-cylinder imaging apparatus of claim 1 , wherein said high intensity light source is a xenon light source.
10. The in-cylinder imaging apparatus of claim 1 , further comprising a prism disposed between said high intensity light source and the combustion chamber, wherein said prism is operable to disperse light from said high intensity light source into the combustion chamber.
11. The in-cylinder imaging apparatus of claim 10 , wherein said prism is formed from sapphire.
12. The in-cylinder imaging apparatus of claim 10 , further comprising a fiber optic bundle disposed between said high intensity light source and said prism, said fiber optic bundle being operable to communicate said light from said high intensity light source to said prism.
13. A method of imaging a combustion chamber of an internal combustion engine during engine operation, the method comprising:
mounting a borescope with respect to the internal combustion engine and in optical communication with the combustion chamber;
mounting a high-speed imaging device with respect to the internal combustion engine and in generally axial alignment with said borescope; such that said borescope is operable to communicate images from within the combustion chamber to said high-speed imaging device;
illuminating the combustion chamber with light from a high intensity light source; and
capturing said images of the combustion chamber with said high-speed imaging device while the internal combustion engine is operating.
14. The method of claim 13 , further comprising cooling the borescope with chilled and compressed gas.
15. The method of claim 13 , wherein illuminating the combustion chamber includes employing a dispersion prism to disperse said light into the combustion chamber.
16. The method of claim 15 , further comprising communicating said light from said high intensity light source to said prism through a fiber optic bundle.
17. The method of claim 13 , further comprising protecting said borescope by placing a window between said borescope and the combustion chamber.
18. The method of claim 17 , wherein said window is selected from the group consisting of quartz, sapphire and spinel.
19. The method of claim 13 , wherein mounting said high-speed imaging device with respect to the internal combustion engine includes:
affixing a bracket to the internal combustion engine;
machining said bracket to accept said high-speed imaging device while affixed to the internal combustion engine to ensure alignment between said high-speed imaging device and said borescope; and
mounting said high-speed imaging device to said bracket.
20. The method of claim 13 , wherein mounting said high-speed imaging device with respect to the internal combustion engine includes:
affixing a bracket to the internal combustion engine;
mounting said high-speed imaging device to said bracket; and
tuning said bracket such that the natural frequency modes of said bracket are greater than an inducing function of the internal combustion engine.