Device for measuring the characteristics of an air flow

{
  "publication_number": "US10871402B2",
  "country": "US",
  "kind": "B2",
  "title": "Device for measuring the characteristics of an air flow",
  "abstract": "A device for measuring the characteristics of an air flow intended to be mounted in an annular duct having a longitudinal axis in a turbine engine, comprising supporting means which support means for measuring the characteristics of an air flow. According to the invention, the supporting means comprise at least one first support including a main branch supporting first measuring means and a second support, structurally independent of the first support and including a main branch supporting second measuring means, with the first support and the second support being so formed that the main branch of the first support extends over a distance greater than the main branch of the second support in a common direction of extension of the branches.",
  "claims": [
    "1. An assembly comprising: a device for measuring the characteristics of an air flow intended to be mounted in an annular duct having a longitudinal axis in a turbine engine, the device comprising supporting means which support means for measuring the characteristics of an air flow, wherein the supporting means comprise at least one first support including a main branch supporting first measuring means and a second support, structurally independent of the first support and including a main branch supporting second measuring means, with the first support and the second support being so formed that the main branch of the first support extends over a distance greater than the main branch of the second support in a common direction of extension of said branches; and an annular duct having a longitudinal axis radially limited outwards by a radially external annular wall configured to support the device, wherein the radially external annular wall comprises one opening through which the first support and the second support are mounted so that the first support applies onto the second support, with a longitudinal dimension of the first support and a longitudinal dimension of the second support each being smaller than a longitudinal dimension of the opening of the radially external annular wall, with the longitudinal dimension of the first support and the second support in a flow passage being greater than an axial dimension of the opening of the annular wall.",
    "2. The assembly according to claim 1, wherein the main branch of the first support supports at least one auxiliary branch provided with the first measuring means and the main branch of the second support supports at least one auxiliary branch provided with the second measuring means, with said auxiliary branches extending in a direction transverse to the direction of extension intended to correspond to a circumferential direction of the annular duct wherein the branches are mounted.",
    "3. The assembly according to claim 2, wherein the main branch of the second support is, in said direction of extension, shorter than the main branch of the first support, and the at least one auxiliary branch: extending on different radiuses, in the circumferential direction transverse to said direction of extension, and being, each, provided with measuring means able to execute pressure and/or temperature measurements at various measuring points spaced apart in said direction of extension and circumferential direction, wherein the second support and the first support are removably attached together to have only one degree of freedom relative to each other among one circumferential degree of freedom and one transversal degree of freedom relative to said direction of extension and said circumferential direction.",
    "4. The assembly according to claim 2, wherein, with the main branch of the second support being, in said flow passage, radially shorter than the main branch of the first support, and the auxiliary branches extending circumferentially on different radiuses and each being provided with measuring means able to execute pressure and/or temperature measurements at various measuring points radially spaced apart on the circumference in said flow passage, the second support and the first support are so coupled together as to have only one degree of freedom relative to each other among one degree of freedom on the circumference and one degree of freedom along said axis.",
    "5. The assembly according to claim 4, wherein the second support and first support are engaged one in the other where coupled together, with no rigid attachment therebetween, so that only one said degree of freedom exists relative to one another.",
    "6. The assembly according to claim 4, wherein, outside said flow passage, the second support and first support are rigidly attached to said annular wall, without having one degree of freedom relative to one another.",
    "7. The assembly according to claim 4, wherein, for coupling the second support and the first support, the second support comprises a pin having a radially internal free length and the first support comprises one opening receiving the radially internal free length of the pin having, as degree(s) of freedom, at least said only one degree of freedom among one degree of freedom on the circumference and one degree of freedom along said axis.",
    "8. The assembly according to claim 7, wherein, on the second support, the pin extends substantially coaxially to a radial direction along which the main branch extends, on a radially internal face of a central part of said at least one auxiliary branch, and, on the first support, the opening is located in a substantially axial rim that the main branch has, where an elbow is.",
    "9. The assembly according to claim 7, wherein the opening is defined by a groove, which is: open radially outwards so as to receive the pin, and elongated on the circumference so as to provide one said degree of freedom on the circumference, between the second and first supports.",
    "10. The assembly according to claim 7, wherein the opening is defined by a hole: wherein the radially internal free length of the pin is engaged, and which is axially elongated, so as to provide one said degree of freedom along said axis.",
    "11. The assembly according to claim 1, wherein the first support and the second support each comprise a baseplate formed at a radially external end of the respective main branch thereof, with such baseplates being mounted in the opening of the external annular wall and attached to said annular wall.",
    "12. The assembly according to claim 11, wherein the baseplates of the first and second supports are attached, on a plate integral with an intermediate part inserted between the plate and the annular wall, with said intermediate part being attached to the external annular wall.",
    "13. The assembly according to claim 12, wherein the baseplates of the first and second supports are attached by bolting.",
    "14. A method for assembling the assembly according to claim 11, comprising the steps of: a) introducing the main branch of the first support into the opening of the annular wall through the end thereof opposite the one supporting the baseplate and positioning said baseplate at a first circumferential end of said opening; b) introducing the main branch of the second support into the opening of the annular wall through the end thereof opposite the one supporting the baseplate, with said baseplate being positioned at a second circumferential end of said opening; and c) moving the first and second supports in a circumferential direction so that the main branches longitudinally apply on one another.",
    "15. The method according to claim 14, wherein, for coupling the second support and the first support, the second support comprises a pin having a radially internal free length and the first support comprises one opening receiving the radially internal free length of the pin of the second support, the pin of the second support having, as degree(s) of freedom, at least only one degree of freedom among one degree of freedom on the circumference and one degree of freedom along said axis, and wherein the method comprises a step consisting in removably attaching at least one radial rod to each baseplate, prior to step a), and using such rods to hold the main branches in position from outside the annular wall.",
    "16. The method according to claim 15, comprising, after step c), the following steps which are executed from outside the annular wall: mounting an intermediate part so that one central opening thereof encloses the baseplates; mounting a plate in contact with the baseplates, simultaneously holding the rods with one hand using a suitable tool, and inserting threaded rods through the plate and the screwing same into the baseplates of the first and second supports.",
    "17. An assembly comprising: a device for measuring the characteristics of an air flow intended to be mounted in an annular duct having a longitudinal axis in a turbine engine, the device comprising supporting means which support means for measuring the characteristics of an air flow, wherein the supporting means comprise at least one first support including a main branch supporting first measuring means and a second support, structurally independent of the first support and including a main branch supporting second measuring means, with the first support and the second support being so formed that the main branch of the first support extends over a distance greater than the main branch of the second support in a common direction of extension of said branches; and wherein the main branch of the first support supports at least one auxiliary branch provided with the first measuring means and the main branch of the second support supports at least one auxiliary branch provided with the second measuring means, with said auxiliary branches extending in a direction transverse to the direction of extension intended to correspond to a circumferential direction of the annular duct wherein the branches are mounted, the assembly further comprising an external annular duct having a longitudinal axis radially limited outwards by a radially external wall configured to support the device, wherein, with the main branch of the second support being, in a flow passage, radially shorter than the main branch of the first support, and the auxiliary branches extending circumferentially on different radiuses and each being provided with measuring means able to execute pressure and/or temperature measurements at various measuring points radially spaced apart on a circumference in said flow passage, the second support and the first support are so coupled together as to have only one degree of freedom relative to each other among one degree of freedom on the circumference and one degree of freedom along said axis."
  ],
  "description_excerpt": "The present invention relates to a device for measuring the characteristics of an air flow, specifically in a turbine engine, such as a turbojet engine or a turboprop engine.\n\nConventionally, a dual- flow turbofan 10, as illustrated in FIG. 1, consists of a gas turbine 12 with a revolution axis 14 driving a ducted fan wheel 16, wherein the latter is generally positioned upstream from the turbofan. The mass of air sucked in by the engine is divided into a primary air flow (arrow A) that flows through the gas turbine 12 or engine core and a secondary air flow (arrow B) originating from the fan 16 and surrounding the engine core, wherein the primary and secondary air flows are concentric and circulate in a primary annular flow passage 18 and a secondary annular flow passage 20, respectively.\n\nIn a manner well known per se, the primary air flow (arrow A) is generally compressed by a low- pressure compressor 22 and subsequently by a high- pressure compressor 24, each having vanes both fixed 26 and mobile arranged alternatively in the direction of movement of the flow. The low-pressure compressor shaft is connected to the fan wheel 16 and is driven in rotation by the shaft of a low-pressure turbine arranged downstream (not illustrated). The low-pressure compressor shaft is driven in rotation by the shaft of a high-pressure turbine arranged at the outlet of a combustion chamber and located upstream from the low-pressure turbine (both not illustrated).",
  "cpc": [
    "G01K 1/14",
    "F01D 17/08",
    "F01D 17/085",
    "F01D 25/243",
    "F01D 25/246",
    "F01D 9/065",
    "G01F 1/34",
    "G01F 1/684",
    "G01K 1/026",
    "G01K 13/02",
    "G01K 13/024",
    "G01K 2013/024",
    "G01M 15/14",
    "G01P 5/14",
    "G01P 5/165"
  ],
  "ipc": [
    "G01F 1/34",
    "G01K 1/14",
    "G01K 13/02",
    "G01M 15/14",
    "F01D 17/08",
    "G01K 1/00",
    "G01K 1/02",
    "G01K 13/00",
    "G01K 7/00",
    "G01P 5/165"
  ],
  "assignees": [
    "Safran Aircraft Engines SAS"
  ],
  "inventors": [
    "Jérémy Giordan",
    "Florian Joseph Bernard Kockenpo",
    "Thibault Xavier Alexis Berranger",
    "Pascal Léon Georges Beilvert"
  ],
  "filing_date": "2018-03-29",
  "publication_date": "2020-12-22",
  "grant_date": "2020-12-22",
  "priority_date": "2017-03-31",
  "application_number": "US-201815939449-A",
  "family_id": "63669184",
  "cited_by_count": 2,
  "citations": [
    "US2820839A",
    "US4572677A",
    "US5812588A",
    "US6776524B2",
    "US20040114665A1",
    "US20100158074A1",
    "EP2492441A2",
    "US8944678B2",
    "FR3051044A1"
  ]
}