CY1121505T1 - Κραματα αργιλιου 7χχχ υψηλης αντοχης και μεθοδοι παρασκευης αυτων - Google Patents
Κραματα αργιλιου 7χχχ υψηλης αντοχης και μεθοδοι παρασκευης αυτωνInfo
- Publication number
- CY1121505T1 CY1121505T1 CY20191100374T CY191100374T CY1121505T1 CY 1121505 T1 CY1121505 T1 CY 1121505T1 CY 20191100374 T CY20191100374 T CY 20191100374T CY 191100374 T CY191100374 T CY 191100374T CY 1121505 T1 CY1121505 T1 CY 1121505T1
- Authority
- CY
- Cyprus
- Prior art keywords
- methods
- alloys
- ingot
- aluminum
- durabily
- Prior art date
Links
- 238000000034 method Methods 0.000 title abstract 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 title 1
- 229910052782 aluminium Inorganic materials 0.000 title 1
- 229910045601 alloy Inorganic materials 0.000 abstract 3
- 239000000956 alloy Substances 0.000 abstract 3
- 229910000838 Al alloy Inorganic materials 0.000 abstract 2
- 229910052751 metal Inorganic materials 0.000 abstract 2
- 239000002184 metal Substances 0.000 abstract 2
- 238000005266 casting Methods 0.000 abstract 1
- 238000005097 cold rolling Methods 0.000 abstract 1
- 239000011888 foil Substances 0.000 abstract 1
- 238000005098 hot rolling Methods 0.000 abstract 1
Classifications
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/10—Alloys based on aluminium with zinc as the next major constituent
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62D—MOTOR VEHICLES; TRAILERS
- B62D29/00—Superstructures, understructures, or sub-units thereof, characterised by the material thereof
- B62D29/008—Superstructures, understructures, or sub-units thereof, characterised by the material thereof predominantly of light alloys, e.g. extruded
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/002—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working by rapid cooling or quenching; cooling agents used therefor
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
- C22F1/053—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon of alloys with zinc as the next major constituent
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C2001/0054—Fuselage structures substantially made from particular materials
- B64C2001/0081—Fuselage structures substantially made from particular materials from metallic materials
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Architecture (AREA)
- Structural Engineering (AREA)
- Combustion & Propulsion (AREA)
- Transportation (AREA)
- Continuous Casting (AREA)
- Metal Rolling (AREA)
- Heat Treatment Of Sheet Steel (AREA)
- Materials For Medical Uses (AREA)
- Conductive Materials (AREA)
- Heat Treatment Of Articles (AREA)
Abstract
Στο παρόν περιγράφονται καινοτόμα κράματα αργιλίου σειράς 7xxx. Τα κράματα επιδεικνύουν υψηλή αντοχή. Τα κράματα μπορεί να χρησιμοποιηθούν σε πολλές εφαρμογές, συμπεριλαμβανομένων των εφαρμογών για αυτοκίνητα, για τις μεταφορές, για ηλεκτρονικά είδη, σε αεροδιαστημικές και βιομηχανικές εφαρμογές. Επιπλέον, στο παρόν περιγράφονται μέθοδοι για την παρασκευή και την κατεργασία των κραμάτων. Περαιτέρω, στο παρόν περιγράφονται μέθοδοι παραγωγής ενός μεταλλικού φύλλου, οι οποίες περιλαμβάνουν τη χύτευση ενός κράματος αργιλίου που περιγράφεται στο παρόν για να σχηματιστεί ένα πλίνθωμα, την ομοιογενοποίηση του πλινθώματος, τη θερμή έλαση του πλινθώματος για την παραγωγή μιας θερμής ταινίας, και την ψυχρή έλαση της θερμής ταινίας σε ένα μεταλλικό φύλλο τελικού διαμετρήματος.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201562248796P | 2015-10-30 | 2015-10-30 | |
US201662326858P | 2016-04-25 | 2016-04-25 | |
PCT/US2016/059272 WO2017075319A1 (en) | 2015-10-30 | 2016-10-28 | High strength 7xxx aluminum alloys and methods of making the same |
Publications (1)
Publication Number | Publication Date |
---|---|
CY1121505T1 true CY1121505T1 (el) | 2020-05-29 |
Family
ID=57960808
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CY20191100374T CY1121505T1 (el) | 2015-10-30 | 2019-04-04 | Κραματα αργιλιου 7χχχ υψηλης αντοχης και μεθοδοι παρασκευης αυτων |
Country Status (23)
Country | Link |
---|---|
US (2) | US11421309B2 (el) |
EP (2) | EP3521466B1 (el) |
JP (2) | JP6971151B2 (el) |
KR (2) | KR102455319B1 (el) |
CN (2) | CN107406925A (el) |
AU (1) | AU2016344192B2 (el) |
BR (1) | BR112017021490B1 (el) |
CA (1) | CA2979717C (el) |
CY (1) | CY1121505T1 (el) |
DK (1) | DK3265595T3 (el) |
ES (1) | ES2719555T3 (el) |
HR (1) | HRP20190548T1 (el) |
HU (1) | HUE042400T2 (el) |
IL (1) | IL258885A (el) |
LT (1) | LT3265595T (el) |
MX (2) | MX2017011840A (el) |
PL (1) | PL3265595T3 (el) |
PT (1) | PT3265595T (el) |
RS (1) | RS58615B1 (el) |
RU (1) | RU2717434C2 (el) |
SI (1) | SI3265595T1 (el) |
WO (1) | WO2017075319A1 (el) |
ZA (1) | ZA201802759B (el) |
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WO2017218240A1 (en) * | 2016-06-14 | 2017-12-21 | Timco Aviation Services, Inc. | Seat system |
US11396687B2 (en) * | 2017-08-03 | 2022-07-26 | Hrl Laboratories, Llc | Feedstocks for additive manufacturing, and methods of using the same |
KR102647056B1 (ko) * | 2017-08-29 | 2024-03-14 | 노벨리스 인크. | 안정된 t4 템퍼의 7xxx 시리즈 알루미늄 합금 제품 및 이를 제조하는 방법 |
CN107779702A (zh) * | 2017-12-06 | 2018-03-09 | 中国航发北京航空材料研究院 | 一种含Ag和Sc的7XXX高强铝合金专用焊丝 |
CN107779701A (zh) * | 2017-12-06 | 2018-03-09 | 中国航发北京航空材料研究院 | 一种含Ag和Sc的7XXX高强可焊铝合金 |
CN108165849A (zh) * | 2017-12-08 | 2018-06-15 | 四川福蓉科技股份公司 | 一种7系铝合金及其制备方法 |
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