final report submitted to: national aeronautics … · nasa-cr-197580 final report submitted to:...
TRANSCRIPT
NASA-CR-197580
FINAL REPORT SUBMITTED TO:
NATIONAL AERONAUTICS AND SPACE ADMINISTRATION (NASA)
Lewis Research Center
Report Title:
"Composites Research in Support of the NASP Institute for Composites (NIC)"NCC3-218
Period Covered:
June 1, 1991 through August 31, 1994
Submitted by:
T. Michael Knasel
Director for Research
Ohio Aerospace Institute22800 Cedar Point Road
Cleveland, OH 44142
216/962-3040
November 29, 1994
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https://ntrs.nasa.gov/search.jsp?R=19950012056 2019-03-01T18:08:26+00:00Z
NASA GRANTEE SUBCONTRACTORNEW TECHNOLOGY REPORT
NASA requires each research grantee, research contractor and research subcontractor to report new technology to theNASA Technology Utilization Office. The required reports and corresponding schedules for researach granteesu "bcontraox_ are as follows:
Title of Rcoorl Form Number .Timetable
Individual Disclosure
Interim Report
NASA 666A
LeRC-GSNTR
The grantee subcontractor discloses each discovery of new technologyindividually, at the time of its discovery.
For multi-year grant subcontracts, the subcontractor summarizes the
previous year's disclosures on an annual basis. The first Interim NewTechnology (2qT) Report is due exactly 12 months from the effectivedate of the subcontract.
Final Report
Subontractor Nameand Address:
Report Submitted by:Telephone Number:
NASA Grant Title:
NASA Grant Number:
NASA Grant Monitor:
LeRC-GSNTR The grantee subcontractor submits a cumulative summary of all
disclosed discoveries. This Final NT Report is submitted immediatelyfollowing the subcontract's technical period of performance.
Massachusetts Institute of TechnolOgy
Department of Materials Sciene_e-and Engineering
77 Massachusetts Ave,
Cambridme_ MA 02139
R, M_ Pelloux
(617) 253 - 3314
NASP Institute fo E Composites (NIC)
NC___ff__C3- 218
0AI Mike Knasel
Subcontract Completion Date: 8 / 31 / 94
Today's Date: ..__2_/22/_9__4_
New technology may be either reportable items or subject inventions.
A reportable item is any invention or discovery, whether or not patentable, that was conceived or fimt actually reduced to practice during the performance
of the contract or subcontract. Large business contractors and subcontractors must disclose reportable items as they are discovered and submit a
noncumulative list of these new technology items on an annual basis [ref: Interim NT Report] and a cumulative list at the completion of the contract (orsubcontract) period [re£: Final NT Report].
A subject invention is any invention or discovery, which is or may be patentable, that Was conceived or first actually reduced to practice during the
performance of the Contract or subcontract, Small business contractors and subcontractors must, at a minimum, disclose subject inventions as they are
discovered and submit a cumulative list of these new technology items on an annual basis [ref: Interim NT Report] and at the completion of the contract (orsubcontract) period [ref: Final NT Report].
Grantees, ':mall business contractors and subcontractor are only required to disclose and report patentable Items (subject inventions). We request, however,
that small business contractors and subcontractors disclose both patentable'sad nonpatentable (reportable) Items, both of which are stttomatlcally evaluatedfor publication as NASA tech briefs and considered for NASA Tech Brief awards.
PLEASE COM_PLETE THE ILEVERSE SIDE OF TIIIS FORM AND MAIL TO THE FOLLOWING ADDRESS:
LeRC-GSNTR
7/01/93
• ' • •i i•¸ :_ •: ': •• ¸¸ •? • "
NASA LEWIS RESEARCH CENTER
A'IWN: KATITY KERRIGAN
TECHNOLOGY UTILIZATION OFFICE; MAIL STOP 7-3CLEVELAND, OIIIO 44135
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f, ll¢O._ ,_o-m,l_$ an=• .--_ _o-rnBrmcn
New Technology Report Form Approved IO.M.B. No. 2700-0009
NT CONTROL NO, {OfftczJI USe Only/
INSTRUCTIONS
This form may be used when reporting inventions, discov-
eries, improvements or innovations to NASA. Use of this
report form is optional; provided, however, that whatever
report format is used contain the essential information requested
nerein.
In completing each sec¢Jon, use whatever detail deemed
appropriate for a "'full and complete disclosure." as rec_uired by
the New Technology or Property Rights in Inventions clause. For
further guidance as to what constitutes a satisfactory repot.
please refer to NHB 21"70.3, Documentation. Guidelines for
New Technology Reporting.
Available additional documentation which provides a full, de-
tailed description should be attached, as well as any additional
explanatory sheets where nec=ssary.
1. TITLE Elevated Temperature Tensile and Creep Deformation of a
SiC Fiber-Reinforced Titanium Metal Matrix Composite
2. INNOVATOR(S) (Name and S_I ,.RecuriW No.) *
R. M. Pelloux - SS 534 42 3580
Rita Thursnon - SS 357 68 9567
3. EMPLCYE _ (O_anazBt/on and div*$JOnJ
Massachusetts Institute of
DepOt of Materials Science
Technology
and Engineering
4. A_=RESS [Plat# of P_o_anc_J
77 Massachusetts Ave._
Cambridge, _ 02139
SECTION I -- DESCRIPTION OF THE PROBLEM THAT MOTIVATED THE TECHNOLOGY DEVELOPMENT (Enrer,t,.--Genera/
_¢'_crimrion of ProDlern Ob/eC.tive," S.--Key or Uni¢Tue ProDletw _laracmrittJc: C --P_t HistDr3//Pmof Tecnni_Tue._: G.--iJn_trarion$ of Prior TecnnJoues}
The main goal was to measure the elevated temperature tensile and
creep properties of a SiC fiber-reinforced tiEanium metal matrix
composite.
• _i_
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" Suoplyincj mis information is voluntary, in accordance with Public Law g3-579 (Privacy Ac: of 197_,i. However. it _s required for
eligibility in the establishment of Space Act monetary awards.
,IAS.,% FORM 666A APR 85 PREVIOUS E{31TION IS OBSOLETE. I .
• ; ' _ /-_;_;_,_ •_/i __-_I
'SECTION II (Con.)
SECTION III -- UNIQUEOR NOVEL FEATURES OF THE TECHNOLOGY AND THE RESULTS (OR BENEFITS) OF ITS APPLI-CATION (Enter as appropriate A.--Novel or unique features; B. --DevelQOment or conceptual problems; t'__O_era¢in 9 characteristics, test data;D.--Analysis of capabilities; E.'Source of error; and F.--Advan_age_/shortcoming=)
Co - Test data results are given in attached report and in MS thesis.
.
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DCPD Curves for (0)4 SCS-9/Beta 21S
650°C / 276 MPa
62
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S •ormahzed DCPD Curves for (0)4 SCS-9/Beta 21S
650°C / 276 MPa
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650°C / 21 MPa
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Conclusions
At 650°C, the UTS of (0)4 and (0/90)sSCS-9/Beta 21S decreases by almost50% from the room temperature values, indicating that operating temperaturesshould be less than 650°C to take advantage of the specific strength as wellas the specific elastic modulus of these composite layups.
The tensile properties of SiC fiber-reinforced titanium composites aredependent on the properties of the fiber reinforcement as well as the fibervolume fraction.
Fracture mechanisms in (0)4SCS-9/Beta 21S are a combination of randomfiber failure throughout the specimen and matrix microyielding aroundfractured fibers.
Failure of (90)4 SCS-9/Beta 21S is dominated by the properties of the metalmatrix.
Fracture mechanisms in (0/90)s SCS-9/Beta 21S are a combination offiber-matrix debonding, random fiber fracture of the 0 ° fibers and matrixmicroyielding around debonded 90 ° fibers and fractured 0° fibers.
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