Injector for mixing two propellants comprising at least one injection element with a tricoaxial structure

US9528479B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9528479-B2
Application numberUS-201214003712-A
CountryUS
Kind codeB2
Filing dateMar 6, 2012
Priority dateMar 7, 2011
Publication dateDec 27, 2016
Grant dateDec 27, 2016

How to read this patent

A practical reading order for non-experts. Skip the full description unless you need deep technical detail.

  1. Title

    What the patent document calls the invention.

  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

    Who owns or filed the patent and who is credited as inventor.

  4. Key dates

    Filing, priority, publication, and grant dates set the timeline.

  5. First independent claim

    The legal scope of protection — read this for what is actually claimed.

  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

    Prior art links and similar publications in this corpus.

Abstract

Official abstract text for this publication.

An injector for mixing two propellants upstream of a combustion chamber. The injector includes: at least one injection element with a tricoaxial structure installed between two plates which between them delimit a space; and coaxial ducts including an internal coaxial duct and an external coaxial duct that are supplied in parallel with a same propellant, for example via the space.

First claim

Opening claim text (preview).

The invention claimed is: 1. An injector for mixing two propellants, comprising: several injection elements with a tricoaxial structure installed between two plates, an upstream plate and a downstream plate delimiting a space therebetween; and three coaxial ducts being defined in the injection element, including an annular middle coaxial duct for a first propellant and two coaxial ducts for a second propellant, the two coaxial ducts including an annular internal coaxial duct and external coaxial duct, respectively, wherein the internal coaxial duct and the external coaxial duct are supplied in parallel with a second propellant, wherein each injection element is rigidly fixed to the two plates, and wherein each injection element includes: a first segment directly fixed to the upstream plate and in which the internal coaxial duct is formed, a second segment directly fixed to the first segment and defining the annular middle coaxial duct therewith, and a third segment directly fixed to the second segment and defining the annular external coaxial duct therewith. 2. The injector according to claim 1 , wherein the space between the two upstream and downstream plates forms a space for introducing the second propellant and at least one injection element includes independent and calibrated passages including: at least one first passage directly connecting the introduction space to the internal coaxial duct and at least one second passage directly connecting the introduction space to the external coaxial duct. 3. The injector according to claim 1 , wherein the first segment includes holes extending between the internal coaxial duct and the space defined between the plates. 4. The injector according to claim 3 , wherein the holes of the first segment are formed at an angle relative to a radial direction. 5. The injector according to claim 1 , wherein the third segment includes holes extending between the external coaxial duct and the space defined between the plates. 6. The injector according to claim 5 , wherein the holes of the third segment are formed at an angle relative to a radial direction. 7. The injector according to claim 1 , wherein the first segment includes a central body around which the annular internal coaxial duct is formed. 8. The injector according to claim 7 , wherein the central body and the first segment form a single block, the internal coaxial duct being annularly hollowed depth wise so as to individualize the central body. 9. The injector according to claim 7 , wherein the central body is attached in an axial recess of the first segment. 10. The injector according to claim 1 , wherein fins or helical grooves are formed on a face of at least one wall delimiting one of the coaxial ducts. 11. The injector according to claim 1 , wherein the at least one injection element further includes an inner central body arranged axially inside the internal coaxial duct to give it an annular configuration, an end of an outer wall of the internal coaxial duct includes a first axial indentation relative to an end of a central body and/or an end of an inner wall of the external coaxial duct includes a second axial indentation relative to the end of the central body. 12. The injector according to claim 11 , wherein a downstream end of the central body includes an open indentation. 13. The injector according to claim 11 , wherein the first and second indentations exist and are equal. 14. The injector according to claim 11 , wherein the first and second indentations exist and are unequal. 15. The injector according to claim 14 , wherein the first indentation is larger than the second indentation. 16. The injector according to claim 14 , wherein the first indentation is smaller than the second indentation. 17. The injector according to claim 11 , wherein the central body has a tip. 18. The injector according to claim 1 , wherein each injection element is rigidly fixed to the two plates by welding or brazing. 19. The injector according to claim 1 , wherein the first segment includes a first upstream section in which an upstream basin is formed for receiving the first propellant, a second downstream cylindrical section having a smaller diameter than the first upstream section, and a shoulder separating the first and second sections, and wherein the upstream basin is introduced upstream from the upstream plate, and walls defining an interior space of the basin are fixed in a hole provided in the upstream wall. 20. The injector according to claim 1 , wherein the first segment is made of two welded coaxial parts: an outer part with a tubular shape and a central part forming a central body. 21. The injector according to claim 1 , wherein the second segment is tubular and includes a first section, a second section having a smaller diameter than the first section of the second segment, and a flat annular wall connecting the first and second sections, and wherein the third segment is tubular and includes a first section fixed to the flat annular wall of the second segment, and a second section having a smaller diameter than the first section of the third segment and being fixed to a hole provided in the downstream wall.

Assignees

Inventors

Classifications

  • F02K9/52Primary

    Injectors · CPC title

  • F02M43/04Primary

    Injectors peculiar thereto · CPC title

Patent family

Related publications grouped by family.

External sources

Frequently asked questions

Answers are generated from the same data shown on this page.

What does patent US9528479B2 cover?
An injector for mixing two propellants upstream of a combustion chamber. The injector includes: at least one injection element with a tricoaxial structure installed between two plates which between them delimit a space; and coaxial ducts including an internal coaxial duct and an external coaxial duct that are supplied in parallel with a same propellant, for example via the space.
Who is the assignee on this patent?
Le Cras Jean-Luc, Lonchard Jean-Marie, Fournet Arnaud, and 4 more
What technology area does this patent fall under?
Primary CPC classification F02K9/52. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Dec 27 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).