Missile wing mounting angle detection device and method

The invention discloses a missile wing mounting angle detection device and method, the device comprises a fitting clamping piece, a fitting block and a positioning rule, the fitting block comprises a first fitting surface, and the first fitting surface is respectively located on the top surface and...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	SHI JINKE, ZHANG YUE, WANG WANLI, XU XIAOJIE, YANG QIAN, WANG CHONG, YU LEI, CHEN YANXI, REN WEN, QIN WEIBO, ZHAO KE, ZHANG YANGMING, LIAO TIANHE, CAO TAO, YING JIAQI, LIU LIN, BIAN CHENGFEI
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	MEASURING MEASURING ANGLES MEASURING AREAS MEASURING IRREGULARITIES OF SURFACES OR CONTOURS MEASURING LENGTH, THICKNESS OR SIMILAR LINEARDIMENSIONS PHYSICS TESTING
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Beschreibung
Zusammenfassung:	The invention discloses a missile wing mounting angle detection device and method, the device comprises a fitting clamping piece, a fitting block and a positioning rule, the fitting block comprises a first fitting surface, and the first fitting surface is respectively located on the top surface and the bottom surface of the fitting block; a through groove is formed in the fitting clamping piece, the top surface of the through groove is a second fitting surface, the bottom surface of the fitting clamping piece is a second matching surface, the fitting block is assembled in the through groove of the fitting clamping piece, the missile wing is clamped between the first fitting surface and the second fitting surface, and the position of the fitting block is fixed through matching of the fixing device and the first matching surface; the first fitting surface and the second fitting surface are curved surfaces matched with the two sides of the missile wing in shape respectively, and the first fitting surface and the