VANE ROTARY TYPE COMPRESSOR
PROBLEM TO BE SOLVED: To further increase the maximum application limit number of revolutions of a compact low-capacity compressor for exhibiting performance as a substitute for a large-capacity compressor. SOLUTION: When a high strength spacer 5 is inserted in a groove part of a rotor 2, strength o...
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Main Authors | , |
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Format | Patent |
Language | English |
Published |
24.07.2008
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Subjects | |
Online Access | Get full text |
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Summary: | PROBLEM TO BE SOLVED: To further increase the maximum application limit number of revolutions of a compact low-capacity compressor for exhibiting performance as a substitute for a large-capacity compressor. SOLUTION: When a high strength spacer 5 is inserted in a groove part of a rotor 2, strength of a rotor jaw part is increased. Alternatively, an L-shaped spacer is inserted to the rotor jaw part. A plurality of vane groove parts of the rotor are integrated together, and a material composition for the rotor consists of a plurality of materials. In this way, strength of the rotor jaw part is increased, and the maximum application limit number of revolutions is increased further. Thus, performance as a substitute for a high-capacity compressor is provided, and reduction in size and weight as requirements of a vehicle manufacturer is provided. COPYRIGHT: (C)2008,JPO&INPIT |
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Bibliography: | Application Number: JP20070005628 |