US3747944A - Dry lubricated materials, members and systems with boron nitride and graphite - Google Patents

Dry lubricated materials, members and systems with boron nitride and graphite Download PDF

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US3747944A
US3747944A US00212414A US3747944DA US3747944A US 3747944 A US3747944 A US 3747944A US 00212414 A US00212414 A US 00212414A US 3747944D A US3747944D A US 3747944DA US 3747944 A US3747944 A US 3747944A
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working surface
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graphite
boron nitride
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A Roy
J Geyman
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    • CCHEMISTRY; METALLURGY
    • C10PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10MLUBRICATING COMPOSITIONS; USE OF CHEMICAL SUBSTANCES EITHER ALONE OR AS LUBRICATING INGREDIENTS IN A LUBRICATING COMPOSITION
    • C10M7/00Solid or semi-solid compositions essentially based on lubricating components other than mineral lubricating oils or fatty oils and their use as lubricants; Use as lubricants of single solid or semi-solid substances
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C33/00Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/02Parts of sliding-contact bearings
    • F16C33/04Brasses; Bushes; Linings
    • F16C33/06Sliding surface mainly made of metal
    • F16C33/12Structural composition; Use of special materials or surface treatments, e.g. for rust-proofing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16NLUBRICATING
    • F16N15/00Lubrication with substances other than oil or grease; Lubrication characterised by the use of particular lubricants in particular apparatus or conditions
    • CCHEMISTRY; METALLURGY
    • C10PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10MLUBRICATING COMPOSITIONS; USE OF CHEMICAL SUBSTANCES EITHER ALONE OR AS LUBRICATING INGREDIENTS IN A LUBRICATING COMPOSITION
    • C10M2201/00Inorganic compounds or elements as ingredients in lubricant compositions
    • CCHEMISTRY; METALLURGY
    • C10PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10MLUBRICATING COMPOSITIONS; USE OF CHEMICAL SUBSTANCES EITHER ALONE OR AS LUBRICATING INGREDIENTS IN A LUBRICATING COMPOSITION
    • C10M2201/00Inorganic compounds or elements as ingredients in lubricant compositions
    • C10M2201/04Elements
    • C10M2201/041Carbon; Graphite; Carbon black
    • CCHEMISTRY; METALLURGY
    • C10PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10MLUBRICATING COMPOSITIONS; USE OF CHEMICAL SUBSTANCES EITHER ALONE OR AS LUBRICATING INGREDIENTS IN A LUBRICATING COMPOSITION
    • C10M2201/00Inorganic compounds or elements as ingredients in lubricant compositions
    • C10M2201/04Elements
    • C10M2201/041Carbon; Graphite; Carbon black
    • C10M2201/042Carbon; Graphite; Carbon black halogenated, i.e. graphite fluoride
    • CCHEMISTRY; METALLURGY
    • C10PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10MLUBRICATING COMPOSITIONS; USE OF CHEMICAL SUBSTANCES EITHER ALONE OR AS LUBRICATING INGREDIENTS IN A LUBRICATING COMPOSITION
    • C10M2201/00Inorganic compounds or elements as ingredients in lubricant compositions
    • C10M2201/04Elements
    • C10M2201/05Metals; Alloys
    • CCHEMISTRY; METALLURGY
    • C10PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10MLUBRICATING COMPOSITIONS; USE OF CHEMICAL SUBSTANCES EITHER ALONE OR AS LUBRICATING INGREDIENTS IN A LUBRICATING COMPOSITION
    • C10M2201/00Inorganic compounds or elements as ingredients in lubricant compositions
    • C10M2201/06Metal compounds
    • C10M2201/061Carbides; Hydrides; Nitrides
    • CCHEMISTRY; METALLURGY
    • C10PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10MLUBRICATING COMPOSITIONS; USE OF CHEMICAL SUBSTANCES EITHER ALONE OR AS LUBRICATING INGREDIENTS IN A LUBRICATING COMPOSITION
    • C10M2201/00Inorganic compounds or elements as ingredients in lubricant compositions
    • C10M2201/06Metal compounds
    • C10M2201/062Oxides; Hydroxides; Carbonates or bicarbonates
    • CCHEMISTRY; METALLURGY
    • C10PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10MLUBRICATING COMPOSITIONS; USE OF CHEMICAL SUBSTANCES EITHER ALONE OR AS LUBRICATING INGREDIENTS IN A LUBRICATING COMPOSITION
    • C10M2201/00Inorganic compounds or elements as ingredients in lubricant compositions
    • C10M2201/08Inorganic acids or salts thereof
    • CCHEMISTRY; METALLURGY
    • C10PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10MLUBRICATING COMPOSITIONS; USE OF CHEMICAL SUBSTANCES EITHER ALONE OR AS LUBRICATING INGREDIENTS IN A LUBRICATING COMPOSITION
    • C10M2201/00Inorganic compounds or elements as ingredients in lubricant compositions
    • C10M2201/08Inorganic acids or salts thereof
    • C10M2201/081Inorganic acids or salts thereof containing halogen
    • CCHEMISTRY; METALLURGY
    • C10PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10MLUBRICATING COMPOSITIONS; USE OF CHEMICAL SUBSTANCES EITHER ALONE OR AS LUBRICATING INGREDIENTS IN A LUBRICATING COMPOSITION
    • C10M2201/00Inorganic compounds or elements as ingredients in lubricant compositions
    • C10M2201/08Inorganic acids or salts thereof
    • C10M2201/082Inorganic acids or salts thereof containing nitrogen
    • CCHEMISTRY; METALLURGY
    • C10PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10MLUBRICATING COMPOSITIONS; USE OF CHEMICAL SUBSTANCES EITHER ALONE OR AS LUBRICATING INGREDIENTS IN A LUBRICATING COMPOSITION
    • C10M2201/00Inorganic compounds or elements as ingredients in lubricant compositions
    • C10M2201/08Inorganic acids or salts thereof
    • C10M2201/084Inorganic acids or salts thereof containing sulfur, selenium or tellurium
    • CCHEMISTRY; METALLURGY
    • C10PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10MLUBRICATING COMPOSITIONS; USE OF CHEMICAL SUBSTANCES EITHER ALONE OR AS LUBRICATING INGREDIENTS IN A LUBRICATING COMPOSITION
    • C10M2201/00Inorganic compounds or elements as ingredients in lubricant compositions
    • C10M2201/085Phosphorus oxides, acids or salts
    • CCHEMISTRY; METALLURGY
    • C10PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10MLUBRICATING COMPOSITIONS; USE OF CHEMICAL SUBSTANCES EITHER ALONE OR AS LUBRICATING INGREDIENTS IN A LUBRICATING COMPOSITION
    • C10M2201/00Inorganic compounds or elements as ingredients in lubricant compositions
    • C10M2201/16Carbon dioxide
    • CCHEMISTRY; METALLURGY
    • C10PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10MLUBRICATING COMPOSITIONS; USE OF CHEMICAL SUBSTANCES EITHER ALONE OR AS LUBRICATING INGREDIENTS IN A LUBRICATING COMPOSITION
    • C10M2201/00Inorganic compounds or elements as ingredients in lubricant compositions
    • C10M2201/18Ammonia
    • CCHEMISTRY; METALLURGY
    • C10PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10NINDEXING SCHEME ASSOCIATED WITH SUBCLASS C10M RELATING TO LUBRICATING COMPOSITIONS
    • C10N2050/00Form in which the lubricant is applied to the material being lubricated
    • C10N2050/08Solids
    • CCHEMISTRY; METALLURGY
    • C10PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10NINDEXING SCHEME ASSOCIATED WITH SUBCLASS C10M RELATING TO LUBRICATING COMPOSITIONS
    • C10N2050/00Form in which the lubricant is applied to the material being lubricated
    • C10N2050/10Semi-solids; greasy
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S277/00Seal for a joint or juncture
    • Y10S277/903Seal for rotating kiln or drum

Definitions

  • An improved gas turbine regenerator seal system having a new configuration wherein one of the rubbing seal members thereof carries a new material providing an initial working surface comprised of an iron oxide matrix containing an interspersed mixture of boron nim ew a.I-// .1 07 516- 3 I m F w 2 ⁇ l 6 m "l 9 u “9 w u :u 7 n "mml mnus "m g &3 n. ""0 nme wa L C .m .m.w UIF 111 218 555 rlZiZl.
  • This invention relates in general to a material for dry lubricated rubbing members, such as might be used in Wankel engines, and more particularly to turbine engine regenerator members which use such materials and even more particularly to a new configuration of seal system which uses such a material.
  • Dry lubrication refers to systems wherein a member rubs against a mat- I ing member as in turbine regenerators wherein a regenerator core rotates in rubbing contact between a set of seals and cross-arms at high temperatures and in the absence of fluid lubricants.
  • This invention in its broadest sense provides a new material exhibiting desirable friction and wear characteristics for use under conditions of the type encountered under elevated temperature dry lubrication conditions.
  • the material forms a working surface for one of a pair of mating members adapted for rubbing relationship, and is particularly adapted for use at temperatures such as those which occur in certain sections of gas turbine engine regenerators, that is, temperatures in the area of about l,000 F.
  • a working surface initially generally comprises a matrix layer of iron oxide, preferably Fe 0,, carried by a substrate.
  • the iron oxide layer contains an interspersed mixture of nickel coated graphite, boron nitride (BN) and Na St) or the equivalent defined hereinbelow.
  • the graphite and boron nitride act as a solid lubricant for the members and aid in the formation of a substantially continuous highly oriented mo, crystalline surface film on the rubbing member work surface.
  • the film is highly oriented because most of the oxide particles, as a result of run-in or break-in, align themselves due to the rubbing action during break-in with their basal planes substantially parallel to the top or exterior rubbing portion of the working surface.
  • Na S0 acts as a particle trapping material in which the abraded oxide particles embed and orient themselves to sinter and form the substantially continuous film of highly oriented Fe 0 I
  • the invention also provides anew hot rim and regenerator design configuration containing a novel debris groove arrangement which uses this material.
  • FIG. 1 is a schematic showing of a part of a gas turbine engine comprising the regenerator portion or system.
  • FIG. 2 is an elevation showing a regenerator core.
  • FIG. 3 is an elevation showing an inner seal system from a regenerator section including hot seal rims and hot cross arms.
  • FIGS. 4a and 4b are fragmentary schematics illustrating the structure of the material according to this invention before and after break-in, respectively.
  • a regenerator core 10 rotates in rubbing contact between an outer seal system 12 also known as the cold seals, and an inner seal system 14, also known as the hot seals.
  • System 14 includes a hot rim seal 16 and a hot cross ,arm seal 18.
  • the material of this invention is particularly adapted for use as a working surface on hot rim seal 16 and will be described in that context herein although it is not necessarily limited thereto. In the environment of the hot rim seal the material is typically exposed to working tem- .peratures in the order of about 600 1,000 F.
  • the material of such a working surface prior to break-in, consists of an iron oxide matrix preferably Fe O on the surface of a substrate, such as 430, 442, and 446 stainless steel or the like, generally ferritic stainless materials.
  • a substrate such as 430, 442, and 446 stainless steel or the like, generally ferritic stainless materials.
  • the exact character of the substrate is not important so long as it possesses the necessary compatible thermal expansion coefficient and the like with the material of the working surface layer.
  • the other iron oxides FeO and Fe O or various mixtures thereof may also be used for the initial oxide matrix.
  • the iron oxide contains an interspersed mixture of boron nitride, nickel coated graphite and sodium sulfate, sodium phosphate or calcium fluoride (Na2SO4, Na PO or CaF trapping material as shown in FIG. 4a.
  • these materials are present in relative proportions of about 55 percent by weight Fefl 20 percent by weight nickel coated graphite, 20 percent by weight Na SO or equivalent and about 5 percent by weight boron nitride.
  • the initial working surface is best formed by flame or plasma spraying a particulate mixture of Fe 0 powder, nickel coated graphite, boron nitride and the-trapping material Na SO Na PO CaF or mixtures thereof onto the substrate.
  • Nicel coated graphite is used in the case of spraying because it comprises graphite particles coated with nickel to protect the graphite during spraying. It is commercially available in various compositions ranging from about 50-85 percent nickel and 50-15 percent graphite. Otherwise, ordinary graphite particulate may be used.
  • FIG. 2 shows a regenerator core having a peripheral groove 24 on the face thereof and spaced grooves 26 radiating from the peripheral groOve toward the circumference of the core.
  • FIG. 3 shows the hot rim seals 16 and cross arm 18 which mate with the regenerator core, the rims, cross-arms and core being in rubbing contact as shown above in FIG. 1 when the engine is in operation. Note from FIG. 3 that the surfaces of the seal system are smooth.
  • peripheral and radial grooves 29 and 26 on the regenerator core are critical to long-life operation of seal systems of this configuration.
  • the grooves function as a debris removing channel providing for the removal of any excessive amounts of abraded particles which may form, i.e., those particles not used in forming the continuous film. Excessive amounts of abraded particles which do not embed themselves in the trapping of the working surface layer cause abrasion of the mating surfaces.
  • the configuration and working surface material cooperate together to provide for the embedding of some of the abraded iron oxide particles in the working surface where during run-in they orient themselves in a self-preferred fashion with their basal planes parallel to the working surface and sinter together to form a substantially continuous highly oriented Fe O film on the seal contact surface as shown in FIG. 4b.
  • the grooves provide a means for removing those excess particles which do not embed themselves in the working surface thus avoiding having the particles trapped between the members and abrading the surface, causing damage.
  • Run-in or break-in may occur under a wide variety of conditions.
  • the following schedules show a few of the conditions which may be used ifa member intended to form a part of a regenerator system ofa gas turbine engine is to be broken in.
  • break-in may take place in a running fixture or in an actual engine.
  • T F temperature of the hot face of the regenerator as at the inner seal of the regenerator of FIG. 1.
  • a member particularly adapted for operating under dry lubrication conditions comprising a substrate having a working surface made up of an iron oxide matrix including an interspersed mixture of boron nitride, a component selected from the group consisting of graphite, nickel coated graphite and mixtures thereof and a component selected from the group consisting of sodium sulfate, sodium phosphate, clacium fluoride and mixtures thereof, the interspersed mixture being present in relative amounts sufficient to promote the formation of a substantially continuous outer layer of Fe O on the working surface during break-in.
  • the member of claim 1 wherein the interspersed mixture is present in about the proportion by weight of: 1 part boron nitride, 4 parts nickel coated graphite and 4 parts sodium sulfate, respectively.
  • a regenerator section for a gas turbine engine wherein at least two members thereof are adapted for rubbing contact during operation of the engine, one of the members having an initial working surface comprised of an iron oxide matrix containing an interspersed mixture of boron nitride, a component selected from the group consisting of graphite, nickel coated graphite and mixtures thereof, and a component selected from the group consisting of sodium sulfate, sodium phosphate, calcium fluoride and mixtures thereof, the interspersed mixture being present in relative amounts sufficient to promote a transformation in the working surface during a break-in period and form as a result a substantially continuous film of Fe,0;, on the word surface of the one member and second film of Fe O on the mating member, formed by transfer from the one member thereto.
  • the initial oxide matrix is substantially made up of Fe O 6.
  • the one member is selected from the group consisting of regenerator seal rims and cross-arms, the mating surface being provided by the regenerator core.
  • regenerator core mating surface contains a peripheral debris collecting groove and the seal rim and cross arm having a substantially smooth working surface.
  • a member particularly adapted for operating under dry lubrication conditions comprising a substrate having an initial working surface made up of an iron oxide matrix containing an interspersed mixture of about by weight 1-10 percent boron nitride; -50 percent of a component selected from the group consisting of graphite, nickel coated graphite and mixtures thereof, and about 5-30 percent of a component selected from the group consisting of sodium sulfate, sodium phosphate, calcium fluoride and mixtures thereof, the balance of the working surface being comprised of the aforesaid iron oxide matrix.
  • the iron oxide matrix is Fe O 11.
  • the working surface of the member defined comprises an initial working surface prior to any break-in, the working surface after break-in including a substantially continuous outer layer of Fe O 12.
  • the working surface is more particularly characterized as including an interspersed mixture of about 5 percent by weight of boron nitride, about 20 percent by weight of a component selected from the first mentioned group, about 20 percent by weight of a component selected from the second mentioned group, balance being comprised of the aforesaid iron oxide matrix.
  • a rubbing member comprising a substrate having a working surface inlcuding a substantially continuous outer layer and a matrix between the layer and substrate comprised of iron oxide interspersed with a mixture in about the proportion by weight of 1 part boron nitride, 4 parts of a component selected from the group consisting of graphite, nickel coated graphite and mixtures thereof and 4 parts of a component selected from the group consisting of sodium sulfate, sodium phosphate, calcium fluoride, and mixtures thereof.
  • Attesting Officer (lommissloner of Patents oem PO-105O (10-69) [1.5. GOVERNMENT PRINTING O FFICE 2 "l9 O-Bli-Sll.

Abstract

An improved gas turbine regenerator seal system having a new configuration wherein one of the rubbing seal members thereof carries a new material providing an initial working surface comprised of an iron oxide matrix containing an interspersed mixture of boron nitride, nickel coated graphite and sodium sulfate - Na2SO4, sodium phosphate - Na3PO4, or calcium fluoride - CaF2.

Description

1451 July 24,1973
United States Patent 1191 Roy et al. 2
[ DRY LUBRICATED MATERIALS, MEMBERS 3,503,787 3/1970 Pendse 117/931 PF AND SYSTEMS WITH BORON NITRIDE AND 316011182 4/1971 Rao 277/96 R GRAPHITE [76] Inventors: Amedee Roy, 2661 Cheswick Dr.
, Primary Examiner-Samuel B. Rothberg Assistant Examiner-Robert 1. Smith Attorney-Oliver F. Arrett [22] Filed:
[21] Appl. No.: 212,414
An improved gas turbine regenerator seal system having a new configuration wherein one of the rubbing seal members thereof carries a new material providing an initial working surface comprised of an iron oxide matrix containing an interspersed mixture of boron nim ew a.I-// .1 07 516- 3 I m F w 2} l 6 m "l 9 u "9 w u :u 7 n "mml mnus "m g &3 n. ""0 nme wa L C .m .m.w UIF 111 218 555 rlZiZl.
tride, nickel coated graphite and sodium sulfate N21 References Cited 233mm phosphate Na PO or calcium fluoride UNITED STATES PATENTS 3,378,392 Longo.i........................ il7/93.l PF 14 Claims, 5 Drawing Figures PAIENTEU JUL24'975 3. 747. 944
SHEET 3 BF 3 DRY LUBRICATEI) MATERIALS, MEMBERS AND SYSTEMS WITH BORON NITRIDE AND GRAPHITE CROSS REFERENCE RELATED APPLICATIONS This application is related to two co-pending applications filed on even date herewith. The first application Ser. No. 212,249 is entitled Iron Oxide Material and Members for Dry Lubricated Systems Including the Method of Preparation Therefor, the inventors being Amedee Roy, Claude Belleau and James M. Geyman. The second application Ser. No. 212,413 is entitled Dry Lubricated Materials, Members and Systems with Graphite and Methods of Preparation,.the inventors being Amedee Roy and James M. Geyman. The copending applications are assigned to the same assignee as the present application and the contents thereof are incorporated herein by reference. This invention constitutes an improved variation of the inventions disclosed in the aforementioned co-pending applications.
BACKGROUND OF THE INVENTION This invention relates in general to a material for dry lubricated rubbing members, such as might be used in Wankel engines, and more particularly to turbine engine regenerator members which use such materials and even more particularly to a new configuration of seal system which uses such a material. Dry lubrication refers to systems wherein a member rubs against a mat- I ing member as in turbine regenerators wherein a regenerator core rotates in rubbing contact between a set of seals and cross-arms at high temperatures and in the absence of fluid lubricants. Heretofore, most systems of thistype have been made with sintered metallic abradable work surfaces, as referred to in the first of the above referenced co-pending applications, or have been coated with graphite and have not functioned well or were not practical for use in gas turbine engines and the like.
I SUMMARY OF THE INVENTION This invention in its broadest sense provides a new material exhibiting desirable friction and wear characteristics for use under conditions of the type encountered under elevated temperature dry lubrication conditions. The material forms a working surface for one of a pair of mating members adapted for rubbing relationship, and is particularly adapted for use at temperatures such as those which occur in certain sections of gas turbine engine regenerators, that is, temperatures in the area of about l,000 F. According to the invention, such a working surface initially generally comprises a matrix layer of iron oxide, preferably Fe 0,, carried by a substrate. The iron oxide layer contains an interspersed mixture of nickel coated graphite, boron nitride (BN) and Na St) or the equivalent defined hereinbelow. During a run-in or break-in period, as at turbine engine operating temperature, e.g., 800 l,000F., the graphite and boron nitride act as a solid lubricant for the members and aid in the formation of a substantially continuous highly oriented mo, crystalline surface film on the rubbing member work surface. The film is highly oriented because most of the oxide particles, as a result of run-in or break-in, align themselves due to the rubbing action during break-in with their basal planes substantially parallel to the top or exterior rubbing portion of the working surface. The
Na S0 acts as a particle trapping material in which the abraded oxide particles embed and orient themselves to sinter and form the substantially continuous film of highly oriented Fe 0 I The invention also provides anew hot rim and regenerator design configuration containing a novel debris groove arrangement which uses this material.
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a schematic showing of a part of a gas turbine engine comprising the regenerator portion or system.
FIG. 2 is an elevation showing a regenerator core.
FIG. 3 is an elevation showing an inner seal system from a regenerator section including hot seal rims and hot cross arms.
FIGS. 4a and 4b are fragmentary schematics illustrating the structure of the material according to this invention before and after break-in, respectively.
DESCRIPTION OF THE PREFERRED EMBODIMENT In the system of FIG. 1, a regenerator core 10 rotates in rubbing contact between an outer seal system 12 also known as the cold seals, and an inner seal system 14, also known as the hot seals. System 14 includes a hot rim seal 16 and a hot cross ,arm seal 18. The material of this invention is particularly adapted for use as a working surface on hot rim seal 16 and will be described in that context herein although it is not necessarily limited thereto. In the environment of the hot rim seal the material is typically exposed to working tem- .peratures in the order of about 600 1,000 F.
The material of such a working surface, prior to break-in, consists of an iron oxide matrix preferably Fe O on the surface of a substrate, such as 430, 442, and 446 stainless steel or the like, generally ferritic stainless materials. The exact character of the substrate is not important so long as it possesses the necessary compatible thermal expansion coefficient and the like with the material of the working surface layer. The other iron oxides FeO and Fe O or various mixtures thereof may also be used for the initial oxide matrix. The iron oxide contains an interspersed mixture of boron nitride, nickel coated graphite and sodium sulfate, sodium phosphate or calcium fluoride (Na2SO4, Na PO or CaF trapping material as shown in FIG. 4a. Preferably these materials are present in relative proportions of about 55 percent by weight Fefl 20 percent by weight nickel coated graphite, 20 percent by weight Na SO or equivalent and about 5 percent by weight boron nitride. The boron nitride may be varied from about I I0 percent, the trapping material from about 5-30 percent, and the nickel coated graphite from about 10-50 percent, Fe=,O., making, up the balance.
The initial working surface is best formed by flame or plasma spraying a particulate mixture of Fe 0 powder, nickel coated graphite, boron nitride and the-trapping material Na SO Na PO CaF or mixtures thereof onto the substrate. Nicel coated graphite is used in the case of spraying because it comprises graphite particles coated with nickel to protect the graphite during spraying. It is commercially available in various compositions ranging from about 50-85 percent nickel and 50-15 percent graphite. Otherwise, ordinary graphite particulate may be used.
The configuration of the regenerator section has been found important in securing the full benefit of this invention when applied to turbine engines. FIG. 2 shows a regenerator core having a peripheral groove 24 on the face thereof and spaced grooves 26 radiating from the peripheral groOve toward the circumference of the core. FIG. 3 shows the hot rim seals 16 and cross arm 18 which mate with the regenerator core, the rims, cross-arms and core being in rubbing contact as shown above in FIG. 1 when the engine is in operation. Note from FIG. 3 that the surfaces of the seal system are smooth.
The peripheral and radial grooves 29 and 26 on the regenerator core are critical to long-life operation of seal systems of this configuration. According to this aspect of the invention, the grooves function as a debris removing channel providing for the removal of any excessive amounts of abraded particles which may form, i.e., those particles not used in forming the continuous film. Excessive amounts of abraded particles which do not embed themselves in the trapping of the working surface layer cause abrasion of the mating surfaces.
The configuration and working surface material cooperate together to provide for the embedding of some of the abraded iron oxide particles in the working surface where during run-in they orient themselves in a self-preferred fashion with their basal planes parallel to the working surface and sinter together to form a substantially continuous highly oriented Fe O film on the seal contact surface as shown in FIG. 4b. The grooves provide a means for removing those excess particles which do not embed themselves in the working surface thus avoiding having the particles trapped between the members and abrading the surface, causing damage.
Also, as a result of run-in or break-in the transfer of iron oxide and trapping material from the seal system to the core surface occurs to form a mating surface thereon consisting of the same oriented Fe O,. film.
The foregoing configuration and material together have been found to provide a markedly long-lived regenerator system. Minor changes such as placing the debris grooves on the seal system rather than on the core have been found to drastically affect this improved operation detrimentally.
During ruin of a rim prepared according to this invention at a temperature in the order of about 800 F. against a mating surface, such as regenerator core 10, the Fe O and loose particles abraded therefrom and oxidized to Fe O The loose oxide particles embedded themselves in the trapping material. The result was a substantially continuous Fe O film of aligned hexagonal Fe O, cells on the material working surface with basal planes of the cells oriented substantially parallel to the working surface as shown in FIG. 4b.
Run-in or break-in may occur under a wide variety of conditions. The following schedules show a few of the conditions which may be used ifa member intended to form a part of a regenerator system ofa gas turbine engine is to be broken in. As can be seen from the schedules, break-in may take place in a running fixture or in an actual engine.
Schedule Running Fixture Condition Time, Minn. P, T F T,, "F Sched. Sched.
Engine SCHEDULE H" 1. 1 hour at idle (23,000-24,000 rpm), T -900 to 2. 1 hour at speed while matching, T l 120 to 1150 to 1200 F.
3. 1 hour at speed, T 120O F.
4. 15 minutes at speed, T -1200 F.
5. 15 minutes at speed, T 1200 F.
6. 15 minutes at 97 speed, T,,1200 F.
7. 15 minutes at 97 speed, T l275 F.
8. 15 minutes at 97 speed, T l350 F.
SCHEDULE CONDITIONS DEFINED P pressure in inches of Hg of cold gas entering regenerator as, at 24 in FIG. 1.
T temperature of the cold face of the regenerator as at the outer seal system of the regenerator of FIG. 1.
T F. temperature of the hot face of the regenerator as at the inner seal of the regenerator of FIG. 1.
Having described the invention, what is claimed as an exclusive right therein is as follows:
1. A member particularly adapted for operating under dry lubrication conditions comprising a substrate having a working surface made up of an iron oxide matrix including an interspersed mixture of boron nitride, a component selected from the group consisting of graphite, nickel coated graphite and mixtures thereof and a component selected from the group consisting of sodium sulfate, sodium phosphate, clacium fluoride and mixtures thereof, the interspersed mixture being present in relative amounts sufficient to promote the formation of a substantially continuous outer layer of Fe O on the working surface during break-in.
2. The member of claim 1 wherein the interspersed mixture is present in about the proportion by weight of: 1 part boron nitride, 4 parts nickel coated graphite and 4 parts sodium sulfate, respectively.
3. The rubbing member of claim 1 wherein the substrate is a stainless steel.
4. A regenerator section for a gas turbine engine wherein at least two members thereof are adapted for rubbing contact during operation of the engine, one of the members having an initial working surface comprised of an iron oxide matrix containing an interspersed mixture of boron nitride, a component selected from the group consisting of graphite, nickel coated graphite and mixtures thereof, and a component selected from the group consisting of sodium sulfate, sodium phosphate, calcium fluoride and mixtures thereof, the interspersed mixture being present in relative amounts sufficient to promote a transformation in the working surface during a break-in period and form as a result a substantially continuous film of Fe,0;, on the word surface of the one member and second film of Fe O on the mating member, formed by transfer from the one member thereto.
5. The engine according to claim 4 wherein the initial oxide matrix is substantially made up of Fe O 6. The engine of claim 4 wherein the one member is selected from the group consisting of regenerator seal rims and cross-arms, the mating surface being provided by the regenerator core.
7. The combination of claim 6 wherein the regenerator core mating surface contains a peripheral debris collecting groove and the seal rim and cross arm having a substantially smooth working surface.
8. The combination of claim 7 wherein additional spaced radial grooves are included on the core extending between the peripheral groove and the edge of the core.
9. A member particularly adapted for operating under dry lubrication conditions comprising a substrate having an initial working surface made up of an iron oxide matrix containing an interspersed mixture of about by weight 1-10 percent boron nitride; -50 percent of a component selected from the group consisting of graphite, nickel coated graphite and mixtures thereof, and about 5-30 percent of a component selected from the group consisting of sodium sulfate, sodium phosphate, calcium fluoride and mixtures thereof, the balance of the working surface being comprised of the aforesaid iron oxide matrix.
10. The memberaccording to claim 9 wherein the iron oxide matrix is Fe O 11. The member according to claim 9 wherein the working surface of the member defined comprises an initial working surface prior to any break-in, the working surface after break-in including a substantially continuous outer layer of Fe O 12. The member according to claim 9 wherein the working surface is more particularly characterized as including an interspersed mixture of about 5 percent by weight of boron nitride, about 20 percent by weight of a component selected from the first mentioned group, about 20 percent by weight of a component selected from the second mentioned group, balance being comprised of the aforesaid iron oxide matrix.
13. The member according to claim 9 wherein the component selected from the first mentioned group is nickel coated graphite and the component selected from the second mentioned group is sodium sulfate.
14. A rubbing member comprising a substrate having a working surface inlcuding a substantially continuous outer layer and a matrix between the layer and substrate comprised of iron oxide interspersed with a mixture in about the proportion by weight of 1 part boron nitride, 4 parts of a component selected from the group consisting of graphite, nickel coated graphite and mixtures thereof and 4 parts of a component selected from the group consisting of sodium sulfate, sodium phosphate, calcium fluoride, and mixtures thereof.
NITED STATES PATENT OFFICE- CERTIFICATE OF CORRECTION Patent No. 3,7L 7,9l4 14. Dated July 973 Inventor(s) Amedeye y, 61 8.1.
It is certified that error appears inthe above-identified patent and that said Letters Patent are hereby corrected as shown below:
On the cover sheet insert 'Assignee: Chrysler Corporation, Highland Park, Michigan Column 'L line 62, change "word" to T--- work line 65, change "engine" to regenerator section 7 line 67, change "engine" to regenera'tor section Signed and sealed this 26th day of February 1971 (SEAL) I n Attest:
EDWARD M.FLETCHEIR,JR. MARSHALL DANN,
Attesting Officer (lommissloner of Patents oem PO-105O (10-69) [1.5. GOVERNMENT PRINTING O FFICE 2 "l9 O-Bli-Sll.

Claims (13)

  1. 2. The member of claim 1 wherein the interspersed mixture is present in about the proportion by weight of: 1 part boron nitride, 4 parts nickel coated graphite and 4 parts sodium sulfate, respectively.
  2. 3. The rubbing member of claim 1 wherein the substrate is a stainless steel.
  3. 4. A regenerator section for a gas turbine engine wherein at least two members thereof are adapted for rubbing contact during operation of the engine, one of the members having an initial working surface comprised of an iron oxide matrix containing an interspersed mixture of boron nitride, a component selected from the group consisting of graphite, nickel coated graphite and mixtures thereof, and a component selected from the group consisting of sodium sulfate, sodium phosphate, calcium fluoride and mixtures thereof, the interspersed mixture being present in relative amounts sufficient to promote a transformation in the working surface during a break-in period and form as a result a substantially continuous film of Fe2O3 on the word surface of the one member and second film of Fe2O3 on the mating member, formed by transfer from the one member thereto.
  4. 5. The engine according to claim 4 wherein the initial oxide matrix is substantially made up of Fe3O4.
  5. 6. The engine of claim 4 wherein the one member is selected from the group consisting of regenerator seal rims and cross-arms, the mating surface being provided by the regenerator core.
  6. 7. The combination of claim 6 wherein the regenerator core mating surface contains a peripheral debris collecting groove and the seal rim and cross arm having a substantially smooth working surface.
  7. 8. The combination of claim 7 wherein additional spaced radial grooves are included on the core extending between the peripheral groove and the edge of the core.
  8. 9. A member particularly adapted for operating under dry lubrication conditions comprising a substrate having an initial working surface made up of an iron oxide matrix containing an interspersed mixture of about by weight 1-10 percent boron nitride; 10-50 percent of a component selected from the group consisting of graphite, nickel coated graphite and mixtures thereof, and about 5-30 percent of a component selected from the group consisting of sodium sulfate, sodium phosphate, calcium fluoride and mixtures thereof, the balance of the working surface being comprised of the aforesaid iron oxide matrix.
  9. 10. The member according to claim 9 wherein the iron oxide matrix is Fe3O4.
  10. 11. The member according to claim 9 wherein the working surface of the member defined comprises an initial working surface prior to any break-in, the working surface after break-in including a substantially continuous outer layer of Fe2O3.
  11. 12. The member according to claim 9 wherein the working surface is more particularly characterized as including an interspersed mixture of about 5 percent by weight of boron nitride, about 20 percent by weight of a component selected from the first mentioned group, about 20 percent by weight of a component selected from the second mentioned group, balance being comprised of the aforesaid iron oxide matrix.
  12. 13. The member according to claim 9 wherein the component selected from the first mentioned group is nickel coated graphite and the component selected from the second mentioned group is sodium sulfate.
  13. 14. A rubbing member comprising a substrate having a working surface inlcuding a substantially continuous outer layer and a matrix between the layer and substrate comprised of iron oxide interspersed with a mixture in about the proportion by weight of 1 part boron nitride, 4 parts of a component selected from the group consisting of graphite, nickel coated graphite and mixtures thereof and 4 parts of a component selected from the group consisting of sodium sulfate, sodium phosphate, calcium fluoride, and mixtures thereof.
US00212414A 1971-12-27 1971-12-27 Dry lubricated materials, members and systems with boron nitride and graphite Expired - Lifetime US3747944A (en)

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Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3830280A (en) * 1971-01-25 1974-08-20 Mallory & Co Inc P R Rare earth flouride lubricant for die casting components
US3887201A (en) * 1973-11-19 1975-06-03 Ford Motor Co Rubbing seal material for ceramic heat exchanger
US3907311A (en) * 1974-04-15 1975-09-23 Ford Motor Co High temperature, low friction ceramic coating for gas turbine regenerator seals
US4205858A (en) * 1977-12-08 1980-06-03 Taiho Kogyo Co., Ltd. Shaft-sealing sliding member
US4391450A (en) * 1982-08-30 1983-07-05 Electrochemical Technology Corp. Shaft seal resistant to electrokinetic corrosion
US5165870A (en) * 1990-05-30 1992-11-24 Kabushiki Kaisha Toshiba Refrigerant compressor
US5221096A (en) * 1990-10-19 1993-06-22 Allied-Signal Inc. Stator and multiple piece seal
US6141953A (en) * 1998-03-04 2000-11-07 Solo Energy Corporation Multi-shaft reheat turbine mechanism for generating power
US6273432B1 (en) * 1997-08-09 2001-08-14 Robert Bosch Gmbh Sealing element for sensors
WO2004024994A1 (en) * 2002-09-11 2004-03-25 Moltech Invent S.A. Protection of non-carbon anodes and other oxidation resistant components with iron oxide-containing coatings
WO2009122169A2 (en) * 2008-04-04 2009-10-08 Ricardo Uk Ltd. A device including sliding surfaces, a method of operation of a device, a method of making a device, and a turbocharger bearing
CN101379313B (en) * 2006-02-06 2011-03-02 松下电器产业株式会社 Sliding member and method for manufacturing the same

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS52108323A (en) * 1976-03-10 1977-09-10 Showa Denko Kk High temperature lubricant parting agent composition
JPS57172995A (en) * 1982-03-29 1982-10-25 Taiho Kogyo Co Ltd Sliding member
JP2555465B2 (en) * 1990-03-28 1996-11-20 日本タングステン株式会社 Self-lubricating hard material
JP2881175B2 (en) * 1991-12-03 1999-04-12 アイシン・エィ・ダブリュ株式会社 Servo hydraulic controller for automatic transmission
DE4300464C1 (en) * 1993-01-11 1994-06-09 Dow Corning Gmbh Solid lubricant combination, process for their production and their use
JPH0720152U (en) * 1993-09-24 1995-04-11 武盛 豊永 Lantern type bellows cleaner tube

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US3378392A (en) * 1963-07-24 1968-04-16 Metco Inc High temperature flame spray powder and process
US3503787A (en) * 1966-02-11 1970-03-31 United States Borax Chem Method of making refractory aluminum nitride coatings
US3601182A (en) * 1969-09-02 1971-08-24 Ford Motor Co Rim construction for gas turbine rotating heat exchangers

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3378392A (en) * 1963-07-24 1968-04-16 Metco Inc High temperature flame spray powder and process
US3503787A (en) * 1966-02-11 1970-03-31 United States Borax Chem Method of making refractory aluminum nitride coatings
US3601182A (en) * 1969-09-02 1971-08-24 Ford Motor Co Rim construction for gas turbine rotating heat exchangers

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3830280A (en) * 1971-01-25 1974-08-20 Mallory & Co Inc P R Rare earth flouride lubricant for die casting components
US3887201A (en) * 1973-11-19 1975-06-03 Ford Motor Co Rubbing seal material for ceramic heat exchanger
US3907311A (en) * 1974-04-15 1975-09-23 Ford Motor Co High temperature, low friction ceramic coating for gas turbine regenerator seals
US4205858A (en) * 1977-12-08 1980-06-03 Taiho Kogyo Co., Ltd. Shaft-sealing sliding member
US4391450A (en) * 1982-08-30 1983-07-05 Electrochemical Technology Corp. Shaft seal resistant to electrokinetic corrosion
US5165870A (en) * 1990-05-30 1992-11-24 Kabushiki Kaisha Toshiba Refrigerant compressor
US5221096A (en) * 1990-10-19 1993-06-22 Allied-Signal Inc. Stator and multiple piece seal
US6273432B1 (en) * 1997-08-09 2001-08-14 Robert Bosch Gmbh Sealing element for sensors
US6141953A (en) * 1998-03-04 2000-11-07 Solo Energy Corporation Multi-shaft reheat turbine mechanism for generating power
WO2004024994A1 (en) * 2002-09-11 2004-03-25 Moltech Invent S.A. Protection of non-carbon anodes and other oxidation resistant components with iron oxide-containing coatings
CN101379313B (en) * 2006-02-06 2011-03-02 松下电器产业株式会社 Sliding member and method for manufacturing the same
WO2009122169A2 (en) * 2008-04-04 2009-10-08 Ricardo Uk Ltd. A device including sliding surfaces, a method of operation of a device, a method of making a device, and a turbocharger bearing
WO2009122169A3 (en) * 2008-04-04 2009-12-03 Ricardo Uk Ltd. A device including sliding surfaces, a method of operation of a device, a method of making a device, and a turbocharger bearing

Also Published As

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FR2166106A1 (en) 1973-08-10
SE7511169L (en) 1975-10-06
AU5032672A (en) 1974-06-20
SE387363B (en) 1976-09-06
JPS529274B2 (en) 1977-03-15
DE2263692A1 (en) 1973-07-12
AU470108B2 (en) 1974-06-20
IT970359B (en) 1974-04-10
FR2166106B1 (en) 1977-12-30
SE402619B (en) 1978-07-10
JPS4872562A (en) 1973-09-29
CA979421A (en) 1975-12-09

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