Aircraft wing horizontal stabilizer measuring device

The utility model provides an aircraft wing horizontal stabilizer measuring device, and belongs to the technical field of aviation wing angle measuring devices. The device comprises a clamping plate assembly, a scale, a supporting threaded sleeve, a lining and a pointer assembly. The device is simpl...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: MOU JINYAO, SU JIUDONG, SHAO HONGZE
Format: Patent
Sprache:chi ; eng
Schlagworte:
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page
container_issue
container_start_page
container_title
container_volume
creator MOU JINYAO
SU JIUDONG
SHAO HONGZE
description The utility model provides an aircraft wing horizontal stabilizer measuring device, and belongs to the technical field of aviation wing angle measuring devices. The device comprises a clamping plate assembly, a scale, a supporting threaded sleeve, a lining and a pointer assembly. The device is simple and practical in structure, has very high practicability, rapidness, accuracy and safety compared with the prior art that corresponding detection means and standard tools are selected only by manpower, can provide powerful guarantee for an airplane to quickly find an optimal included angle, and reduces the probability that a worker selects tools difficultly and the measurement means do not reach the standard, so that the working efficiency of the airplane is greatly improved. The problems of inaccurate measurement, unclear angle value and rework caused by the fact that a linkage device is adjusted according to experience in the prior art are solved, the repair and maintenance of the whole equipment are influenced
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN220568128UU</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN220568128UU</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN220568128UU3</originalsourceid><addsrcrecordid>eNrjZDBxzCxKLkpMK1Eoz8xLV8jIL8qsys8rScxRKC5JTMrMyaxKLVLITU0sLi0CyaeklmUmp_IwsKYl5hSn8kJpbgYlN9cQZw_d1IL8-NTigsTk1LzUknhnPyMjA1MzC0Mji9BQY6IUAQDS7i4y</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Aircraft wing horizontal stabilizer measuring device</title><source>esp@cenet</source><creator>MOU JINYAO ; SU JIUDONG ; SHAO HONGZE</creator><creatorcontrib>MOU JINYAO ; SU JIUDONG ; SHAO HONGZE</creatorcontrib><description>The utility model provides an aircraft wing horizontal stabilizer measuring device, and belongs to the technical field of aviation wing angle measuring devices. The device comprises a clamping plate assembly, a scale, a supporting threaded sleeve, a lining and a pointer assembly. The device is simple and practical in structure, has very high practicability, rapidness, accuracy and safety compared with the prior art that corresponding detection means and standard tools are selected only by manpower, can provide powerful guarantee for an airplane to quickly find an optimal included angle, and reduces the probability that a worker selects tools difficultly and the measurement means do not reach the standard, so that the working efficiency of the airplane is greatly improved. The problems of inaccurate measurement, unclear angle value and rework caused by the fact that a linkage device is adjusted according to experience in the prior art are solved, the repair and maintenance of the whole equipment are influenced</description><language>chi ; eng</language><subject>AIRCRAFT ; AVIATION ; COSMONAUTICS ; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR ; GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT ; GYROSCOPIC INSTRUMENTS ; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR ; MEASURING ; MEASURING DISTANCES, LEVELS OR BEARINGS ; NAVIGATION ; PERFORMING OPERATIONS ; PHOTOGRAMMETRY OR VIDEOGRAMMETRY ; PHYSICS ; SURVEYING ; TESTING ; TRANSPORTING</subject><creationdate>2024</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20240308&amp;DB=EPODOC&amp;CC=CN&amp;NR=220568128U$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20240308&amp;DB=EPODOC&amp;CC=CN&amp;NR=220568128U$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>MOU JINYAO</creatorcontrib><creatorcontrib>SU JIUDONG</creatorcontrib><creatorcontrib>SHAO HONGZE</creatorcontrib><title>Aircraft wing horizontal stabilizer measuring device</title><description>The utility model provides an aircraft wing horizontal stabilizer measuring device, and belongs to the technical field of aviation wing angle measuring devices. The device comprises a clamping plate assembly, a scale, a supporting threaded sleeve, a lining and a pointer assembly. The device is simple and practical in structure, has very high practicability, rapidness, accuracy and safety compared with the prior art that corresponding detection means and standard tools are selected only by manpower, can provide powerful guarantee for an airplane to quickly find an optimal included angle, and reduces the probability that a worker selects tools difficultly and the measurement means do not reach the standard, so that the working efficiency of the airplane is greatly improved. The problems of inaccurate measurement, unclear angle value and rework caused by the fact that a linkage device is adjusted according to experience in the prior art are solved, the repair and maintenance of the whole equipment are influenced</description><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR</subject><subject>GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT</subject><subject>GYROSCOPIC INSTRUMENTS</subject><subject>HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR</subject><subject>MEASURING</subject><subject>MEASURING DISTANCES, LEVELS OR BEARINGS</subject><subject>NAVIGATION</subject><subject>PERFORMING OPERATIONS</subject><subject>PHOTOGRAMMETRY OR VIDEOGRAMMETRY</subject><subject>PHYSICS</subject><subject>SURVEYING</subject><subject>TESTING</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2024</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDBxzCxKLkpMK1Eoz8xLV8jIL8qsys8rScxRKC5JTMrMyaxKLVLITU0sLi0CyaeklmUmp_IwsKYl5hSn8kJpbgYlN9cQZw_d1IL8-NTigsTk1LzUknhnPyMjA1MzC0Mji9BQY6IUAQDS7i4y</recordid><startdate>20240308</startdate><enddate>20240308</enddate><creator>MOU JINYAO</creator><creator>SU JIUDONG</creator><creator>SHAO HONGZE</creator><scope>EVB</scope></search><sort><creationdate>20240308</creationdate><title>Aircraft wing horizontal stabilizer measuring device</title><author>MOU JINYAO ; SU JIUDONG ; SHAO HONGZE</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN220568128UU3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2024</creationdate><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR</topic><topic>GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT</topic><topic>GYROSCOPIC INSTRUMENTS</topic><topic>HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR</topic><topic>MEASURING</topic><topic>MEASURING DISTANCES, LEVELS OR BEARINGS</topic><topic>NAVIGATION</topic><topic>PERFORMING OPERATIONS</topic><topic>PHOTOGRAMMETRY OR VIDEOGRAMMETRY</topic><topic>PHYSICS</topic><topic>SURVEYING</topic><topic>TESTING</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>MOU JINYAO</creatorcontrib><creatorcontrib>SU JIUDONG</creatorcontrib><creatorcontrib>SHAO HONGZE</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>MOU JINYAO</au><au>SU JIUDONG</au><au>SHAO HONGZE</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Aircraft wing horizontal stabilizer measuring device</title><date>2024-03-08</date><risdate>2024</risdate><abstract>The utility model provides an aircraft wing horizontal stabilizer measuring device, and belongs to the technical field of aviation wing angle measuring devices. The device comprises a clamping plate assembly, a scale, a supporting threaded sleeve, a lining and a pointer assembly. The device is simple and practical in structure, has very high practicability, rapidness, accuracy and safety compared with the prior art that corresponding detection means and standard tools are selected only by manpower, can provide powerful guarantee for an airplane to quickly find an optimal included angle, and reduces the probability that a worker selects tools difficultly and the measurement means do not reach the standard, so that the working efficiency of the airplane is greatly improved. The problems of inaccurate measurement, unclear angle value and rework caused by the fact that a linkage device is adjusted according to experience in the prior art are solved, the repair and maintenance of the whole equipment are influenced</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language chi ; eng
recordid cdi_epo_espacenet_CN220568128UU
source esp@cenet
subjects AIRCRAFT
AVIATION
COSMONAUTICS
DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR
GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT
GYROSCOPIC INSTRUMENTS
HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR
MEASURING
MEASURING DISTANCES, LEVELS OR BEARINGS
NAVIGATION
PERFORMING OPERATIONS
PHOTOGRAMMETRY OR VIDEOGRAMMETRY
PHYSICS
SURVEYING
TESTING
TRANSPORTING
title Aircraft wing horizontal stabilizer measuring device
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-06T08%3A10%3A54IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=MOU%20JINYAO&rft.date=2024-03-08&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN220568128UU%3C/epo_EVB%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true