http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-209396064-U

Outgoing Links

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filingDate 2018-11-15-04:00^^<http://www.w3.org/2001/XMLSchema#date>
grantDate 2019-09-17-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_fddcc615b9692aa1d831f71c70890211
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publicationDate 2019-09-17-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber CN-209396064-U
titleOfInvention A kind of aircraft front-wheel deflection angle measuring device
abstract A kind of aircraft front-wheel deflection angle measuring device, belongs to test, field of measuring technique.The aircraft front-wheel deflection angle measuring device includes pedestal, shaft, bearing, rotary bracket, pointer and angle board;The pedestal is placed on level ground, and bearing mounting groove is arranged in pedestal one end setting angle plate, and in the centre of pedestal;The bearing is placed in bearing mounting groove;The shaft is mounted on the base by bearing, installs rotary bracket in the upper end of shaft;The rotary bracket is equipped with the cavity for accommodating aircraft front-wheel, installs pointer on the outer wall of rotary bracket one end.The utility model provides exact value by the measurement to aircraft front-wheel actual deflection angle, to compare with manipulation instruction deflection angle, has achieved the purpose that make aircraft front-wheel deflection executing agency's Reliability of Microprocessor and accurately judge.
isCitedBy http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-111891381-A
priorityDate 2018-11-15-04:00^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

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Total number of triples: 23.