Integral forming method and forming die for annular lip of aero-engine
According to the aero-engine annular lip integral forming method and forming die, a first process model of an annular lip is constructed according to a theoretical model of the annular lip, the inner side wall of the annular lip is formed through the first process model, and a second process model o...
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Format: | Patent |
Sprache: | chi ; eng |
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Zusammenfassung: | According to the aero-engine annular lip integral forming method and forming die, a first process model of an annular lip is constructed according to a theoretical model of the annular lip, the inner side wall of the annular lip is formed through the first process model, and a second process model of the annular lip is constructed according to the theoretical model of the lip and the first process model; the outer side wall of the annular lip is formed through a second process model, an inner side wall drawing die is manufactured according to the first process model, inner side wall drawing forming is conducted on the unfolded material plate through the inner side wall drawing die, the unfolded material plate protrudes upwards and deforms, and a first semi-finished product matched with the first process model is formed; an outer side wall drawing die is manufactured according to the second process model, outer side wall drawing forming is conducted on the first semi-finished product containing the prefabricat |
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