Method of manufacturing a spring with improved thermal stabilization

Abstract

A method for manufacturing a spring is disclosed that comprises: forming the spring from a material; heat treating the spring; performing a first machining step to the ends of the spring; subjecting the spring to a first stress relief heat treatment; performing a second machining step to the ends of the spring; and subjecting the spring to a second stress relief heat treatment step. A spring that is manufactured by this method is also described. This spring may then be used in a pressure relief valve, as well as in other assemblies.

Claims

1. A method for manufacturing a spring comprises: forming the spring from a material; heat treating the spring; performing a first machining step to the ends of the spring; subjecting the spring to a first stress relief heat treatment; performing a second machining step to the ends of the spring; subjecting the spring to a second stress relief heat treatment step, wherein said second machining step is a finer machining step than said first machining step to produce a less coarse surface of the spring ends.

2. The method of claim 1, wherein said first and second machining steps comprise grinding.

3. The method of claim 1, wherein said heat treating of said spring comprises heat treating the spring according to condition C, AMS 5699.

4. The method of claim 1, wherein said first stress relief heat treatment comprises compressing the spring to a length that is reduced compared to the spring's original uncompressed length, via the application of a load and whilst also applying heat.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) Preferred embodiments will now be described by way of example only, with reference to the accompanying drawings.

(2) FIG. 1 is a flow diagram of a method of manufacturing a spring using thermal stabilisation.

(3) FIG. 2 depicts a perspective view of a spring positioned within a pressure relief valve.

DETAILED DESCRIPTION

(4) Although the examples described herein with reference to the drawings may be used for, and are described relating to, the manufacture of an Inconel X750 spring for a high temperature pressure relief valve spring, the improved spring manufacturing techniques described herein may also be used with, or for, any other type of suitable material, spring size, and/or use. The examples described herein with reference to the drawings should therefore not be limited to the specific Inconel X750 spring described below, or its features and/or properties. For example, the material used to form the spring may be another precipitation hardenable Nickel-Chromium alloy with high strength temperatures and high oxidation resistance. Other materials may also be used that are not nickel-chromium alloys.

(5) For reference purposes only, the examples described below involved the formation and modification of a one type of Inconel X750 spring that had a free length of 17.34 mm, a wire diameter of 1.9 mm, an outer diameter of 13.8 mm, a stiffness of 19.29 N/mm, a reference assembly load of 25N, a reference assembly working length of 16 mm, faces perpendicularity (with respect to spring axis) of 0.15 mm, faces planarity of 0.2 mm and a face roughness 0.8 m.

(6) FIG. 2 depicts a spring 200 that is installed within a pressure relief valve 230. Although this FIG. 2 depicts an example of anti-ice valve 240, i.e. a pressure regulating and shut-off valve spring 200, the examples of improved springs described herein could of course also be used in other assemblies and are not limited to this specific relief valve or anti-ice valve arrangement. Such anti-ice valves are known in the art. Indeed, the proposed manufacturing methodology can be applied to springs installed for any application where constant load and precise spring geometry are required.

(7) A new and improved method 100 for manufacturing a spring 200 (e.g. for use in a high temperature pressure relief valve) will now be described with reference to the figures. This new manufacturing method relieves the stress that may be induced during spring end-coil grinding operations, resulting in the guarantee of tight geometric characteristics during the service life of the spring.

(8) The method 100 comprises the steps of first forming 105 the spring 200 from a suitable material. Any conventional methods of forming a spring 200, as are known in the art, may be used. The next method step comprises heat treating 110 the formed spring 200 according to the requirements of that particular material. The heat treatment is performed as prescribed by the applicable material specification. For example, for Inconel X750; condition C, this is performed according to AMS 5699, as is known in the art. No load is applied during this step. This heat treatment step should be performed prior to the step of machining 120 the ends, or end-coils 210 of the spring 200.

(9) The next step is therefore the machining 120 of the ends, or end-coils 210a, 210b of the spring 200. In some examples, this may comprise the grinding of the end-coils 210a,b using a grinding machine. In some examples, the dimensional tolerances of the spring 200 after this stage may optionally then be checked 125 to confirm that they are approximately three times the dimensional tolerances of the finished item.

(10) The spring 200 is then subjected to a first stress relief heat treatment 130. In this step 130 the spring is compressed to a reduced length via the application of a load. This load should be representative of the most severe operative conditions that the spring 200 is likely to encounter when in use within the valve. During this step 130, the oven temperature should be representative also of the temperature that the spring 200 would be operating under when in use. For example, in one specific example, i.e. in the case of the Inconel X750 spring described above, the heat treatment may be compressed from a free length of 17.34 mm to a length of approximately 16 mm at a temperature of 530 C. for 24 hours.

(11) Following this step, and after the removal of the heat and load, a second machining step 140 is then performed, wherein the end-coils 210a, b of the spring are again machined, for example, via grinding. This second machining step 140 is finer than the first machining step 120 so that the coil-ends 210a, b are not as coarse.

(12) After this second machining step 120, in some of the examples described herein, the dimensional tolerances of the spring 200 may optionally also be checked 145 to see if they are the same as for the finished spring. Following this, or following the second machining step 140, a second stress relief heat treatment step 150 is performed. The same load and temperature conditions are used as for the first machining step 120 described above; however, due to the steps performed so far, the spring may compress further under the same load than during step 130 and so the spring 200 may be compressed using the same load so that it now contracts to a length of 15.5 mm when heated to 530 C. for 24 hours. Following on from these steps, the method may then either end 160, or optionally the spring 200 may be checked to make sure the dimensional tolerances of the spring 200 are correct 160, before the method 200 then ends 160.

(13) This manufacturing technique provides numerous benefits over known methods. For example, the spring produced via this method meets the PRV performance requirements in that no hysteresis occurs. The spring also has improved reliability, in that it has a constant pressure set-point throughout its entire working life. It also deals with the issues discussed earlier in the background section of the present disclosure.

(14) Typically, if the second, fine machining step 140 is not performed, then it may not be possible to guarantee repetitive dimensional control (i.e. it would not be possible to guarantee spring faces parallelism). On the other hand, if the step of performing the second stress relief heat treatment 150 does not occur, the spring load may tend to diminish after in-service high temperature exposure (since the end-coils relieve the stress induced during the last machining operation).