Small-sized thermal dynamic testing device for oar-tip rotorjet
This utility model relates to a blade tip jet rotor small-sized thermal power test facilities. In order to reduce the cost of blade tip jet rotor small-sized thermal power principle test research, This utility model chooses turbojet engine (1) used by model plane. Connect one end of L type breather...
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Main Author | |
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Format | Patent |
Language | English |
Published |
17.01.2007
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Subjects | |
Online Access | Get full text |
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Abstract | This utility model relates to a blade tip jet rotor small-sized thermal power test facilities. In order to reduce the cost of blade tip jet rotor small-sized thermal power principle test research, This utility model chooses turbojet engine (1) used by model plane. Connect one end of L type breather pipe (2) with the fixed end of revolving seal joint (5), the other end of L type breather pipe (2) with the outlet of engine (1); Connect the connector of Y type breather pipe (4) with the revolving end of revolving seal joint, each branch pipe connector arranges a cone spray nozzle (3). when the tail jet flow is passing through L type breather pipe (2) and revolving seal joint (5), it is divided into two flows in the In Y type breather pipe (4) and blow out from taper spray nozzle (3) , and the reacting force generated by jet air drives the Y type breather pipe (4), cone spray nozzle and the revolving end of revolving seal joint (5) rotate at a high speed. This utility model can carry out the blade tip jet rotor small-sized thermal power principle test. has the advantages of cheap cost, low investment and less occupation of land. |
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AbstractList | This utility model relates to a blade tip jet rotor small-sized thermal power test facilities. In order to reduce the cost of blade tip jet rotor small-sized thermal power principle test research, This utility model chooses turbojet engine (1) used by model plane. Connect one end of L type breather pipe (2) with the fixed end of revolving seal joint (5), the other end of L type breather pipe (2) with the outlet of engine (1); Connect the connector of Y type breather pipe (4) with the revolving end of revolving seal joint, each branch pipe connector arranges a cone spray nozzle (3). when the tail jet flow is passing through L type breather pipe (2) and revolving seal joint (5), it is divided into two flows in the In Y type breather pipe (4) and blow out from taper spray nozzle (3) , and the reacting force generated by jet air drives the Y type breather pipe (4), cone spray nozzle and the revolving end of revolving seal joint (5) rotate at a high speed. This utility model can carry out the blade tip jet rotor small-sized thermal power principle test. has the advantages of cheap cost, low investment and less occupation of land. |
Author | ZHENGHONG,ZHAN GAO |
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Notes | Application Number: CN2005279790U |
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RelatedCompanies | NORTHWESTERN POLYTECHNIC UNIVERSITY |
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Snippet | This utility model relates to a blade tip jet rotor small-sized thermal power test facilities. In order to reduce the cost of blade tip jet rotor small-sized... |
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SubjectTerms | MEASURING PHYSICS TESTING TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR |
Title | Small-sized thermal dynamic testing device for oar-tip rotorjet |
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