OA16411A - Method and device for inspecting a threading of a tubular connection used in the oil industry. - Google Patents

Abstract

The invention concerns a device for inspecting a threading (fc) of a tubular component for the exploration or working of hydrocarbon wells, the device comprising a threaded support (14) which can cooperate by makeup with the threading (fc) of the tubular component, means (12, fs) for blocking the advance of the threaded support (14) during makeup with the threading (fc) of the tubular component, a longitudinal rail (2) fixed to the means (12, fs) for blocking the advance of the threaded support (14) and extending in a direction belonging to a plane passing through the axis of the threading of the treaded support (14), means (9) for inspecting the treading of the tubular component (fc), and means (4) for longitudinal guidance in order to guide the means (9) for inspecting the treading in translation along the longitudinal rail (2). The invention also concerns methods using the device.

Description

ι

METHOD AND DEVICE FOR INSPECTING A THREADING OF A TUBULAR CONNECTION USED IN THE OIL INDUSTRY [0001] The présent invention relates to a device for inspecling a threading produced in the vicinily of one of the ends of a tubular component used in the exploration or working of hydrocarbon wells. The invention also relates to a method for inspecting such a threading. [0002] Scveral inspection deviccs arc known for inspecting the conformity of the threadings of tubular components used in the exploration or working of hydrocarbon wells. Because of the stresses exerted in service (whether du ring drillîng operations or during working), it is désirable for the threaded zones to be machined to spécifications and to be within tolérances. Such devices employ inspection means that can capture data relating to the geometry of the threadings. These means may be gauges which, by matching the form of the threading, can demonslrate the conformity (or non-conformity) of the width of the thread roots, the pitch, the taper of the threading, etc as a fonction of the reference value and the tolérances for that value. Those means may also be sensors that can producc a direct mcasurement of the width of the thread roots, the thread height, etc.

[0003] However, the Applicant has observed that it is often ncccssary to mark the région of the threading for carrying out the inspection and also to position the inspection means very accurately. In the case of axially tightening sclf-locking threadings as defined in documents US Re 30 647 and US Re 34 467, where the width of the thread roots reduces with distance from the face of the component, it is necessary to refer to the distance from the face of the threaded tubular component when carrying out a mcasurement of the thread roots. It will be recalled that the face of the tubular component is the distal or terminal surface of the tubular component. Similariy, when the width of the thread roots is to be measured in a conventions! threading with a constant thread width, it is conventions! to carry out the mcasurement at the thread mid-height. This therefore means that the inspection means hâve to be positioncd in a stable, précisé manner.

(0004] In general, known deviens consist of sel squares that produce a bcaring point on the face of the threaded tubular componcnt and one or two surface contact points for the threaded tubular componcnt.

However, such devices cannot be mounted on the threaded tubular componcnt in a stable manner and cannot be used to carry out measurements along an axis bclonging to the médian plane. In other words, such devices cannot be used to carry out a measurement with respect to the face of the threaded tubular component, it being certain that the segment measured between the face and the surface contact point of the threaded tubular component belongs to a plane passing through the axis of révolution of the threaded tubular component.

[0005] The Applicant has developcd a stable inspection device that in particular can be used to carry out inspections of the threading at contact points the coordinatcs of which are idcntifîed in a précise manner in a three dimcnsional reference System.

[0006] The invention provides a device for inspecling a threading of a tubular component for the exploration or working of hydrocarbon wells, the device comprising a threaded support which can cooperatc by makeup with the threading of the tubular component, means for blocking the advancc of the threaded support during makeup with the threading of the tubular component, a longitudinal rail fixed to the threaded support and extending in a direction bclonging to a plane passing through lhe axis of the threading of the threaded support, means for inspccting the threading of the tubular component, and means for longitudinal guidance in order to guide the means for inspecling the threading in translation along the longitudinal rail.

[0007] Optional characteristics, which arc complcmentary or substitutional, will be defined below. [0008] The means for blocking the advance of the threaded support during makeup with the threading of the tubular component may be an abutment fixed to the threaded support.

[0009] The means for blocking the advance of the threaded support during makeup with the threading of the tubular component may be comprised by the threading of the threaded support, the threading being of the axîally tightening self-locking type.

'iL· [0010] The longitudinal rail may extend in a direction parallel to the axis of the threading of the threaded support.

[0011] The longitudinal rail may extend in a direction parallel to the taper of the threading of the tlxreaded support.

[0012] The longitudinal guide means may comprise a guide bearing which can slide in the longitudinal rail.

[0013] The inspection dcvice may further comprise radial guide means which can guide the threading inspection means in a direction pcipendicular to and intersecting the axis of the threading of the threaded support.

[0014] The radial guide means may comprise a guide bearing which can slide in a radial rail fixed to the longitudinal guide means.

[0015] The radial guide means may comprise two parallel slats each fîxed at one of their ends to the longitudinal guide means, the other end being fixed to the threading inspection means.

[0016] The inspection device may further comprise means for determining the position of the means for inspecting the threading of the tubular component along the longitudinal rail.

[0017] The means for determining the position of lhe threading inspection means may comprise a graduation provided on the longitudinal rail.

[0018] The means for determining the position of the threading inspection means may be formed by a potentiometer comprising a graduation fixed to the longitudinal rail in a parallel manner as well 20 as a cursor which can slide along said graduation.

[0019] The material constîtuting the threaded support may be selected from the list constituted by bronze, or a hard polyamide type plastic, such that the surface of the threading of the support has high résistance to wear.

[0020] The means for inspecting the threading of the tubular component may comprise two arms, each provided with a first and a second end, the first ends being connccted together by means of a déformable portion that allows an angular déplacement between the second ends, the second ends each carrying a contact element, the inspection means further comprising means for delenmining the displacement.

[0021] The mcans for inspecting the threading of the tubular component may comprise a confocal sensor.

[0022] The invention also concerna a method for inspecting a threading of a tubular component for the exploration or working of hydrocarbon wclls, in which:

• the threaded support of an inspection device in accordance with the invention is made up with the threading of the tubular component until the advance of makeup is blockcd, the inspection device further being provided with radial guide means;

• the means for inspecting the threading of the tubular component are positioned at a selected position Po along the longitudinal rail, said inspection mcans comprising two arms each provided with a first and a second end, the first ends being connected together by means of a déformable portion that allows an angular displacement between the second ends, the second ends each carrying a contact element, the inspection means further comprising means for determining the displacement;

• the inspection means are positioned such that one of the contact éléments of the device is in contact with a loading flank of the threading while the other contact element is in contact with a stabbing flank of the threading, the two contact éléments being within the same thread root;

• the angular displacement e is measured;

• the angular displacement measured previously, e, is compared with a reference value e- [0023] The invention also concerna another method for inspecting a threading of a tubular component for lhe exploration or working of hydrocaibon wells, in which:

• the threaded support of an inspection device of the invention is made up with the threading of the tubular component until the advance of makeup is blocked, the

K inspection device further being provided with radial guide means and having a confocal sensor as the threading inspection means;

• the confocal sensor is displaccd along the longitudinal rail;

• the data collectcd by the confocal sensor is processed in order to establish a profile of the threading.

[0024] Other advantages and charaderistics of the invention will bccome apparent from the following detailed description of examples which are in no way limiting and from the accompanying drawings, which may not only serve to provide a better understanding of the invention, but also contribute to defining it where appropriate.

[0025] Figure 1 shows a sectional view of a connection resulting from makeup of two threaded tubular components.

[0026] Figure 2 shows a detail of a scctional view of a threading of a tubular component.

[0027] Figure 3 shows a perspective view of an embodiment of the invention.

[0028] Figure 4 is a représentation of an embodiment of the invention in exploded view.

[0029] Figure 5 is a représentation of an embodiment of the invention.

[0030] Figure 6 «présents a perspective view of a detail of the invention.

[0031] Figure 1 shows a threaded connection between two substantially tubular components intended to be connected togetherby means of threadings and intended to be integrated into a working string of a hydrocarbon well. The connection, as is conventional, comprises a component provided with a male end 1 and a component provided with a female end 2, the male end 1 being capable of being connected to the female end 2. In this type of connection, the end 1 comprises a first and a second sealing surface that can respectively cooperate in an interférence fit with a first and a corresponding second sealing surface of the female end 2, in order to form a first, 5, and a second, 6, sealing zone. The end 1 also comprises a male threaded zone 3 that can be made up into a corresponding threaded zone 4 of the female end 2, the threaded zones being provided between two sealing zones 5 and 6. The ends 1 and 2 each end in respective distal surfaces 7 and 8.

[0032] Figure 2 shows details of the threaded zones 3 of a self-locking male threading. The complementary female threading is not shown in the figures. The term “self-locking” threadings means threadings comprising the fcaturcs dctailed below. The male threads, like the female threads, hâve a constant pitch. Thcir width dccreases in the direction of their respective distal surfaces 7,8 such that when making up, the male and female threads finish by locking into each other at a predetermined position.

[0033] More preciscly, the pitch of the loading flanks of the female threading is constant, like the pitch of the stabbing flanks of the female threading. The pitch of the loading flanks is greater than the pitch of the stabbing flanks.

[0034] The pitch of the stabbing flanks 31 of the male threading 3 is constant, like the pitch of the loading flanks 30 of the male threading. The pitch of the stabbing flanks 31 is less than the pitch of the loading flanks 30.

[0035] Contact is principally made between the male and female loading flanks 30, as with the male and female stabbing flanks 31. In general, a clearance is provided between the crests of the male threads and the roots of the female threads, while the roots 33 of the male threads 32 and the crests of the female threads are in contact. The clearance means that grease can be evacuated during makeup, avoiding any risk of overpressure due to the grease.

[0036] The threading has a pitch LFPp of constant width between the loading flanks, and a pitch of constant width SFP_p between the stabbing flanks, as well as increasing thread root widths from a value WIDTHmin to a value WIDTHmax in the direction of the distal surface 7 of the tubular component.

[0037] Advantageously, the male and female threads hâve a dovetail profile so that they are securely fitted into each other after makeup. This additional guarantee dispenses with risks of disengagement (also known as jump-oul), which corresponds to the male and female threads coming apart when the connection is subjected lo large bending, tensile or pressure loads. Advantageously, the threadings 1 and 2 have a tapered profile following a generatrix with a taper 100 in order to accelerate engagement of the male element into the female element.

[0038] In general, this taper generatrix forms an angle with the axis 10 in the range 1.5 degrees to 5 degrees. The taper generatrix in the présent case is defined as passing through the centre of the loading flanks.

[0039] Figures 3 and 4 show a device for inspecting a threading of a tubular component for the exploration or working of hydrocarbon wells. The device comprises a threaded support 14 which can cooperate by makeup with the threading of the tubular component. This threaded support 14 is an envelope supported by a secîor of the tapered portion. In other words, if a section of the support 14 is taken along a plane pcrpendicular to the axis of the tapered portion, an arc of a circlc is obtained. This envelope is threaded either on its internai circumfercntial surface in the case in which the device is intendcd for the inspection of a male tubular component, or on its extcmal circumfercntial surface in the case in which the device is for the inspection of a female tubular component. It should be noted that the threaded support 14 is preferably fixed to the device in a rcmovablc manner. In fact, it must be possible to change the threaded support 14 so that it can cooperate by makeup with the threading fc of the tubular component. Thus, the tapered portion which supports it must have the same taper as the component and have a diameter compatible therewith. Similarly, the threading ofthe support must be compatible with that of the tubular component. Preferably, the support extends circumfcrcntially about an arc of a circlc of less than a quarter of the circumference of the tubular component.

[0040] It also comprises means 9 for inspecting the threading of the tubular component. The threading inspection means 9 are fixed on the longitudinal guide means 4 which can guide said inspection means 9 in translation along a longitudinal rail 2.

tu [0041] The longitudinal rail 2 is fixed to the threaded support 14 and extends in a direction belonging to a plane passîng through the axis of the threading of the threaded support 14, [0042] In a first configuration, the longitudinal rail 2 extends in a direction which is parallcl to the axis of the tlireading of the threaded support 14, said axis being coïncident with that of the tubular component. Thus, when mounting the inspection device on the tubular component, the longitudinal rail is parallcl to the axis of the threading of the tubular component, This configuration allows the distance of the inspection means 9 with respect to the face of the tubular component to be measured directly. In fact, this distance corresponds to the portion of the longitudinal rail separating the means 9 from the face (also termed the distal surface), [0043] In a second configuration, the longitudinal rail 22 extends in a direction which is parallel to the taper of the threaded support 14, this direction also corrcsponding to the taper 100 of the tubular component. Thus, when mounting the inspection device on the tubular component, the longitudinal rail is parallel to the taper of the tubular component. This configuration means that the distance between the threading of the tubular component and the measurcment means 9 can be kept 15 constant, [0044] It also comprises means 12 for blocking the advancc of the threaded support 14 du ring makeup with the threading of the tubular component.

[0045] In a first variation shown in Figures 3 and 4, the means for blocking the advancc of the threaded support 14 during makeup with the tlireading of the tubular component are an abutment 12 20 fixed to the threaded support 14. As can be seen in Figure 5, the abutment 12 cornes to bear against the face of the tubular component (c) when the threading fs of the threaded support 14 has been made up sufficiently with the threading fc of said tubular component, [0046] ln a second variation, the means for blocking the advancc of the threaded support 14 during makeup with the threading of the tubular component arc constituted by the threading fs of the threaded support 14 which is of the axially tightening sclf-locking type, said threading fs coopcrating in makeup with an cqually axially tightcning self-locking type threading of the tubular componcnt.

[0047] Advantageously and as shown in Figures 3 and 4, the longitudinal guide means 4 are a guide bearing which can slide in the longitudinal rail 2.

[0048] Advantageously and as can be seen in Figures 3 and 4, the inspection device further comprises radial guide means 5. These latter «llow the inspection means 9 to be movcd in translation along an axis perpendicular to and intcrsccting the axis of the threading of the threaded support 14.

[0049] Advantageously and as can be seen in Figures 3 and 4, the radial guide means 5 are a guide bearing which can slide in a radial rail 6 which is fixed to the longitudinal guide means 4.

[0050] Advantageously, the radial guide means comprise two parallel stats each fixed at one of their ends to the longitudinal guide means, the other end being fixed to the threading inspection means. In this manner, it is sufficient to press on the means 9 for them to descend vertically without pivoting. The two slats romain parallel to each other and keep the means 9 vertical.

[0051] Advantageously and as can be seen in Figures 3 and 4, the inspection device further comprises means 7 for deteimining the position of the means 9 for inspecting the threading of the tubular componcnt along the longitudinal rail 2.

[0052] Advantageously, the means for dclcrmining the position of the threading inspection means 9 are a graduation provided on the rail 2.

[0053] Advantageously and as can be seen in Figures 3 and 4, the means for deteimining the position of the threading inspection means 9 are formed by a potentiometer comprising a graduation 7 fixed to the rail 2 in a parallel manner, as well as a cursor 15 that can slide along said graduation. This embodiment means that the position of the threading inspection means 9 with respect to the face of the tubular componcnt can readily be measured once the inspection device is mounted on the tubular componcnt. The graduation 7 is in fact fixed with respect to the rail which is lise If fixed with respect to the abutment 12, and so il is easy to read on the graduation of the graduation 7 a

YL· measurement corresponding to the distance of the means 9 with respect to the face of the tubular component, against which face the abutment 12 bears.

[0054] Clearly, other means employing sensors (optical, eddy current, laser etc) to mark the position of the inspection means 9 may be foreseen.

[0055] It is also possible to fbresce the provision of a graduation on the radial guide means 5. It may be possible to graduate the radial rail 6 in order to détermine the radial position of the inspection means 9 with respect to the longitudinal rail 2.

[0056] Advontageously, the material constituting the support 14 is selected from the list constituted by aluminium, bronze and polyamides, such that the surface of the threading of the support 14 has high résistance to wear, so that the tubular component is not damaged. For this reason, when mounting the threaded support 14 on the tubular component to be inspected, the blocking position is not falsified by the possibility that the threading of the support could be wom.

[0057] Figure 6 shows the inspection means 9 which may be integrated into the inspection device described above. These means are in fact used to inspect the width of the threadings of tubular components.

[0058] The inspection device 9 comprises two arms 91,92. The arm 91 is provided with a first, 912, and a second, 910, end, while the arm 92 is provided with a first, 922, and a second, 920, end. The first ends 912,922 arc termed ftxed” in that they are connected together via a déformable portion 95. The déformable portion 95 can be used to produce an angular displacement “e due to pivoting of the second ends 910,920 of the arms, termed mobile ends. In other words, the second ends 910,920, termed the mobile ends, may mutually move apart or doser together along a circular arc trajectory which remains in the same plane. The second ends 910,920, termed mobile, each carry a contact element 930,940. The inspection means 9 also comprise means 90 for determining the angular displaccment e.

[0059] Advantageously, the means 90 for determining the angular displacement e comprise a sensor. As an example, it may bc possible to use a miniaturized inductive transceiver type contact sensor which corresponds to the size of the means 9, or a contactless sensor, such as a capacitativc sensor, for example, or an eddy current sensor, or a sensor using optical technology (laser, confocal). ThcsG sensors are intended to measure the distance between the contact éléments 930,940. The maximum measurement range is thus equal to the displacement e. The sensor is selected according to criteria of accuracy, bulk, measurement range, and stability under service and environmental conditions. The accuracy criteria required correspond to an order of magnitude of 0.01% of the measurement range.

[0060] Advantageously, the arms 91,92 and the déformable portion 95 are formed as a single pièce. The déformable portion 95 is flexible, meaning that its flexing can produce the angular 10 displacemcnt e between the mobile ends 910,920 of the arms. This is achievcd by using a suitable material and dimensions. In the présent case, the arms and the déformable portion are formed from steel with a smaller thickness for the déformable portion than for the aims.

[0061] Advantageously, the déformable portion 95 isnot only flexible but also elastic, so that the arms arc in a reference position when at rest, i.e. when the inspection device is not in service.

[0062] The dimensions of the inspection means 9 in the case in which the déformable portion and the arms form a single steel piece, as a function of the height, h, of the threading and the width, WIDTH, of the roots of the threading, may bc as follows:

• the diameter of the contact éléments is in the range 0.5 h to 1.2 h\ • the displacement at rest is in the range 0.1 WIDTH to 0.6 WIDTH;

the length of the contact éléments is in the range 1 mm to 2 A;

• the ratio of the arm thicknesses is greater than 2;

this différence in thickness principally restricting the movement to a single arm. Thus, the arm which romains fixed acls as a reference and it is easier to measure the displacement e of the other arm, which is in mobile.

• the thickness of the déformable portion is in the range 0.005 to 0.5 times the thickness of the thinnest arm;

the réduction in thickness of the déformable portion with respect to the thickness of the arms, and in particular with respect to the thickness of the thinnest arm, provides lhe déformable portion with the flexibility desired to produce the displacement e of the arms with respect to each other.

[0063] Other threading inspection means 9 may be mounted on the device. This is the case, for example, with gauges which comprise threading portions which are to spécification and which are used to validate whether the threading of the tubular component to be inspected is indeed complementary to that of the gaugc.

[0064] lt is possible, for example, to use a confocal sensor using chromatic confocal imaging such as the optoNCDT 2401 from Micro Epsilon. This type of sensor allows the profile of a threading to be determined by scanning said threading over a given distance. Depending on the complcxity of the profile, it may be necessary to Scan said profile several times, changing the angle of the sensor. Chromatic confocal imaging is recognized as a précisé and reliable technique for measuring thickness and distance, it forms part of the 3D metrological techniques recommended in International Standard ISO 25178. The measurement principle employs a chromatic objective projccting the image of a point source of white light W as a continuum of monochromatic images located on the optical axis (chromatic coding). The surface of a specimen placcd in this chromatic coding zone will diffuse the incident beam of light. The light diffuses back through the chromatic objective L in the reverse direction and arrives at an opening P which filters out ail of the wavelengths apart from one, λΜ. The light collected is analyzed by a spectrograph S. The position of the specimen is directly related to the detected wavelength XM. The advantages are as follows: high resolution, high signal to noise ratio, fonctions with ail types of matériels, wide choice of measurement range, compatible with local large inclinations, coaxial geometry (no shadowing), and no speckle effeel.

W (0065] The invention also concerns an inspection method employing the inspection means described in Figure 6 and defined in the following steps:

• the threaded support 14 of an inspection device further provided with radial guide means 5 is made up with the threading fc of the tubular component until the advance of makeup is blocked;

• the inspection means 9 described above are positioned at a selected position Po along the longitudinal rail 2;

• the inspection means 9 are positioned such that one of the contact éléments of the device 930,940 is in contact with a loading flank of the threading while the other contact element 940,930 is in contact with a stabbing flank of the threading, the two contact éléments being within the same thread root;

• the angular displacement e is measured;

• the angular displacement measured previously, e, is compared with a reference value eref.

[0066] The invention also concerns another inspection method using a confocal sensor and defined in the following steps;

• the threaded support 14 of an inspection device in accordance with the invention is made up with the threading fc of a tubular component until the advance of makeup is blocked;

• the confocal sensor is displaccd along the longitudinal rail 2;

« the data collected by the confocal sensor are processed in order to establish a profile of the threading fc.

[0067] The inspection device has the double advantage of positioning the threading inspection means 9 both longitudinally and radially in a précisé and rcliable manner.

[0068] The coopération between the threaded support 14 and the abutment 12 ensures reliable mounting of the inspection device on the tubular component to be inspected, meaning that it might be difficult to move the inspection device once it is in position.

[0069] Next, the longitudinal rail 2 constituas a guide allowing the inspection means 9 to be displaced prccisely along an axis parallcl to the axis of the threaded support, said axis also being the axis of révolution of the tubular component. It is thus possible to inspect the threading of a tubular component at a précisé longitudinal position. The inspection device provided with means 5 9 for measuring the thread width described in Figure 6 is applicable in the case of self-locking threadings. This type of threading, where the width of the thread roots varies throughout the length of the threading, nécessitâtes measuring the width of the thread roots at a predetermined distance from the face of the tubular component.

[0070] Finally, the radial guide means 5 mean that the inspection means 9 can be displaced prccisely in a radial direction with respect to the axis of the threaded support, said axis also being the axis of révolution of the tubular component. Thus, it is possible to inspect the threading of the tubular component at a précisé radial position. This is of advantage in the case of self-locking threadings with a dovetail shaped flank profile, and also in the case of threadings with a trapézoïdal profile, since the thread fianks are not perpendicular to the axis of rotation of the tubular component. The width of the thread roots varies depending on whether the measurement is carried out at the root root, at mid-height or at the thread crest; it is usual to refer to a measurement carried out at mid-height.

A AVR. 2013

ZENAVE M»

Claims (17)

1, A device for inspecting a threading (fc) of a tubular comportent for lhe exploration or working of hydrocarbon wells, the device comprising a threaded support (14) which can cooperate by makeup with the threading (fc) of the tubular component, means (12, fs) for

5 blocking the advanoe of the threaded support (14) during makeup with the threading (fc) of the tubular component, a longitudinal rail (2) fixed to the means (12, fs) for blocking the advance of the threaded support (14) and extending in a direction belonging to a plane passing through the axis of the threading of the threaded support (14), means (9) for inspecting the tlireading of the tubular component (fc), and means (4) for longitudinal

10 guidance in order to guide the means (9) for inspecting the threading in translation along the longitudinal rail (2).

2, An inspection device according to claim 1, characterizcd in that the means for blocking the advance of the threaded support (14) during makeup with the threading (fc) of the tubular component comprise an abutment (12) fixed to the threaded support (14).

15

3. An inspection device according to claim 1, characterizcd in that the means for blocking the advance of the threaded support (14) during makeup with the threading (fc) of the tubular component comprise the threading (fs) of the threaded support (14), the threading being of the axially tightening self-locking type.

4. An inspection device according to any one of the preceding daims, characterizcd in that

20 the longitudinal rail (2) extends in a direction parallel to the axis of the threading of the threaded support (14).

5. An inspection device according to any one of daims 1 to 3, characterized in that the longitudinal rail (2) extends in a direction parallel to the taper of the threading of the threaded support (14).

6. An inspection device according to any one of the preceding claims, characterized in that the longitudinal guide means (4) comprise a guide bearing which can slide in the longitudinal rail (2).

7. An inspection device according to any one of the preceding claims, characterized in that

5 it further comprises radial guide means (5) which can guide the threading inspection means (9) in a direction perpendicular to and intersecting the axis of the threading of the threaded support (14).

8. An inspection device according to claim 7, characterized in that the radial guide means (5) comprise a guide bearing which can slide in a radial rail (6) ftxed to the longitudinal guide

10 means (4).

9. An inspection device according to claim 7, characterized in that the radial guide means (5) comprise two parallel slats each fixed at one of their ends to the longitudinal guide means, the other end being fixed to the inspection nteans (9).

10. An inspection device according to any one of the preceding claims, characterized in that

15 it further comprises means for determining the position of the means (9) for inspecting the threading (fc) of the tubular component along the longitudinal rail (2).

11. An inspection device according to claim 10, characterized in that the means for determining the position of the means (9) for inspecting the threading (fc) comprise a graduation provided on the rail (2).

20

12. An inspection device according to claim 10, characterized in that the means for determining the position of the means (9) for inspecting the threading (fc) arc fbrmed by a potentiometer comprising a graduation (7) ftxed to the rail (2) in a parallel manner as well as a eu r s or (15) which can slide along said graduation (7).

13. An inspection device according to any one of the preceding claims, characterized in that

25 the material constituting the support (14) is selected from the list constitutcd by aluminium, bronze and polyamides, such that the surface of the threading (fs) of the support (14) has high résistance to wcar.

14. An inspection device according to any one of the preceding ctaims, characterized in that the means (9) for inspecting the threading (fc) of the tubular component comprise two arms (91,92), each provided with a first (912,922) and a second (910,920) end, the first ends (912,922) being connected together by means of a déformable portion (95) that allows an angular displacement (e) between the second ends (910,920), the second ends (910,920) each carrying a contact element (930,940), the inspection means further comprising means (90) for dcterminïng the displacement (e).

15. An inspection device according to any one of claims 1 to 13, characterized in that the means (9) for inspecting the threading (fc) of the tubular component comprise a confocal sensor.

16. A method for inspecting a threading (fc) of a tubular component for the exploration or working of hydrocarbon wells, characterized in that it comprises the following steps:

• threading the threaded support (14) of an inspection device in accordance with the claim 14 rattached to one of daims 7 to 9 with the threading (fc) of the tubular component until the progression of threading is blocked;

• positioning the inspection means (9) at a selected position Po along the longitudinal rail (2);

• positioning the inspection means (9) such that one of the contact éléments (930,940) of the device is in contact with a loading flank of the threading while the other contact element (940,930) is in contact with a stabbing flank of the threading, the two contact éléments being wi thin the same thread root;

• measuring the angular displacemcnt e;

• comparing the angular displacement measured prcviously, e, with a reference value e-ref.

17. A method for inspecting a threading (fc) of a tubular component for the exploration or working of hydrocarbon wells, characterized in that it comprises the following steps:

• making up the threaded support (14) of an inspection device in accordance with the claim 15 rattached to one of claims 7 to 9 with the threading (fc) of the tubular component until

5 the progression of threading is blocked;

• displacing the inspection means (9) along the longitudinal rail (2);

• processing the data collected by the confocal sensor in order to establish a profile of the threading (fc).