Process for machining titanium parts using separate biased spraying collar
AssigneeSociete Nationale d'Etude et de Construction de Monteurs d'Aviation "SNECMA"
InventorsSerge Pierre Jean Lagrolet, Jean-Pierre Leboulanger, Serge Andre Marcel Vallet
Life of this patent
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Abstract
A process for machining titanium or titanium alloy parts with a cutting speed exceeding 150 m/min which uses spraying or sprinkling of lubricating fluid under very high pressures (60 to 400 bars). The main component is a spraying flange or collar having internal ducts making it possible to supply under high pressure one or more fluid jets in the direction of the edge of the cutting tip.
Claims8
A process for machining one of a titanium part and a titanium alloy part using a tungsten carbide tip having a cutting edge, which comprises:
- securing a collar to a tool holder having a duct formed therein by utilizing at least one eccentric securing member which biases said collar towards said duct and fluid tightly securing the collar to the tool holder with said at least one eccentric securing member;
- jetting from the duct a lubricating fluid jet towards a position just above a cutting edge of the tip at a pressure of from 60 to 340 bars and lubricating the edge to allow the edge to slide more easily with respect to the part being cut;
- supplying the lubricating fluid jet in a linear manner wherein the duct comprises a first duct and a second duct communicating with the first duct;
- inclining a longitudinal axis of the second duct with respect to the plane of a cutting face of the machining tip by an angle of inclination I such that 7.degree..ltoreq.I.ltoreq.30.degree.;
- and
- forming a reduced diameter portion between the first and second ducts, the reduced diameter portion forming a collar in the form of a reduction cone wherein the conicity C of the reduction cone is such that 0.degree..ltoreq.C.ltoreq.45.degree. and wherein each of said first and second ducts is formed so as to respectively have a substantially constant diameter.
A process for machining one of a titanium part and a titanium alloy part using a tungsten carbide tip having a cutting edge, which comprises:
- securing a collar to a tool holder having a duct formed therein by utilizing at least one eccentric securing member which biases said collar towards said duct and fluid tightly securing the collar to the tool holder with said at least one eccentric securing member;
- jetting from the duct a lubricating fluid jet towards a position just above a cutting edge of the tip at a pressure of from 60 to 340 bars and lubricating the edge to allow said edge to slide more easily with respect to the part being cut wherein a distance D between the end of the duct and the cutting edge is such that 1.2 mm.ltoreq.D.ltoreq.4 mm and wherein the duct includes a first duct and a second duct communicated with the first duct;
- inclining the axis of the second duct with respect to the plane of a cutting face of the machining tip by an angle of inclination I such that 7.degree..ltoreq.I.ltoreq.30.degree.;
- and
- jetting a plurality of lubricating fluid jets from said second duct wherein the number of jets used is determined as a function of the length of the cutting edge and the jets are angled with respect to one another so as to be oriented in a nonparallel manner.
The process for machining one of a titanium part and a titanium alloy part having a tungsten carbide tip with a cutting edge, which comprises:
- securing a collar to a tool holder having a duct formed therein by utilizing at least one eccentric securing member which biases said collar towards said duct and fluid tightly securing the collar to the tool holder with said at least one eccentric securing member;
- jetting from the duct a lubricating fluid jet towards a position just above a cutting edge of the tip at a pressure of from 60 to 340 bars and lubricating the edge to allow the edge to slide more easily with respect to the part being cut wherein the duct comprises a first duct and a second duct in communication with said first duct;
- inclining a longitudinal axis of the second duct with respect to the plane of a cutting face the machining tip by an angle of inclination I such that 7.degree..ltoreq.I.ltoreq.30.degree.;
- and
- supplying the lubricating fluid jet to the first and second ducts in a linear manner;
- setting the relationship of the diameter d of the second duct with respect to the length L of the second duct such that 6 d.ltoreq.L.ltoreq.10 d so as to avoid a pressure loss in said second duct of the lubricating fluid jet.
Dependencies are inferred from the claim text.