IP Library Granted Patent US 12,187,614
Granted Patent B2
US 12,187,614 · App. 17/475,365 · Granted Jan 7, 2025

Composite graphite material and method for preparation thereof, secondary battery, and apparatus

Inventors: Chengdu Liang (Ningde, CN); Yuzhen Zhao (Ningde, CN); Yan Wen (Ningde, CN); Qisen Huang (Ningde, CN)
Assignee: CONTEMPORARY AMPEREX TECHNOLOGY (HONG KONG) LIMITED
C01B32/205C01B32/20C01B32/21H01M4/133H01M4/366H01M4/625H01M10/0525C01P2002/74C01P2002/82C01P2004/61C01P2006/10C01P2006/11C01P2006/12C01P2006/40
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Quick Facts
Patent No.
US 12,187,614
App. No.
17/475,365
Granted
Jan 7, 2025
Kind
B2
Abstract

The present application discloses a composite graphite material and a method for preparing the same, a secondary battery, and an apparatus. The composite graphite material includes a core material and a coating layer that coats at least a portion of the surface of the core material, the core material including graphite, and the coating layer including a coating material containing a cyclic structure moiety, wherein the composite graphite material has a weight-loss rate of from 0.1% to 0.55% when the composite graphite material is heated in an atmosphere of an inert non-oxidative gas at a temperature rising from 40° C. to 800° C. The composite graphite material can enhance the gram capability and reduce the expansion rate of an electrode plate, and more preferably, can improve the cycle performance and kinetic performance of a battery as well.

Claims (50)

1. A composite graphite material, comprising a core material and a coating layer that coats at least a portion of the surface of the core material, characterized in that the core material comprises graphite, and the coating layer comprises a coating material containing a cyclic structure moiety, wherein the composite graphite material has a weight-loss rate of from 0.1% to 0.55% when the composite graphite material is heated at a heating rate of 10° C./min or lower in an atmosphere of an inert non-oxidative gas at a temperature rising from 40° C. to 800° C., and wherein the cyclic structure moiety comprises one or more of Formulae 1 to 3:

2. The composite graphite material according to claim 1 , characterized in that the composite graphite material has a weight-loss rate of from 0.1% to 0.4%, when the composite graphite material is heated at a heating rate of 10° C./min or lower in the atmosphere of an inert non-oxidative gas at a temperature rising from 40° C. to 800° C.

3. The composite graphite material according to claim 1 , characterized in that the composite graphite material has a sulfur content of less than 0.02 wt. %.

4. The composite graphite material according to claim 1 , characterized in that the core material is artificial graphite.

5. The composite graphite material according to claim 4 , characterized in that the composite graphite material has a D-peak intensity I D and a G-peak intensity I G , and the ratio of I D /I G is from 0.4 to 1.0.

6. The composite graphite material according to claim 4 , characterized in that the composite graphite material satisfies a ratio of the peak area C 004 of 004 crystal plane to the peak area C 110 of 110 crystal plane of the composite graphite material C 004 /C 110 ≤15, when the composite graphite material is in an electrode plate with a compaction density of from 1.6 g/cm 3 to 1.7 g/cm 3 .

7. The composite graphite material according to claim 4 , characterized in that the composite graphite material further satisfies one or more of the following (1) to (6):

(1) the composite graphite material has a D v 50 of from 15 μm to 20 μm;

(2) the composite graphite material has a D v 10 of at least 6 μm;

(3) the composite graphite material has a D n 10 of from 1.0 μm to 3.0 μm;

(4) the composite graphite material has a specific surface area of from 0.5 m 2 /g to 1.2 m 2 /g;

(5) the composite graphite material has a compaction density under a pressure of 5 tons of from 1.80 g/cm 3 to 2.10 g/cm 3 ; and

(6) the composite graphite material has a tap density of from 0.8 g/cm 3 to 1.15 g/cm 3 .

8. The composite graphite material according to claim 4 , characterized in that the composite graphite material further satisfies one or more of the following (1) to (6):

(1) the composite graphite material has a D v 50 of from 15 μm to 18 μm;

(2) the composite graphite material has a D v 10 of from 6.5 μm to 10.5 μm;

(3) the composite graphite material has a D n 10 of from 1.2 μm to 2.0 μm;

(4) the composite graphite material has a specific surface area of from 0.6 m 2 /g to 1.0 m 2 /g;

(5) the composite graphite material has a compaction density under a pressure of 5 tons of from 1.93 g/cm 3 to 2.05 g/cm 3 ; and

(6) the composite graphite material has a tap density of from 0.9 g/cm 3 to 1.05 g/cm 3 .

9. A method for preparing a composite graphite material, characterized in that the method comprises the steps of

(1) mixing a solution containing a cyclizable polymer with a graphite core material to obtain a slurry, wherein a mass ratio of the core material to the cyclizable polymer is from 30:1 to 400:1;

(2) drying the slurry to obtain powder;

(3) heat treating the powder at a temperature between 300° C. and 400° C. to obtain the composite graphite material comprising a core material and a coating layer that coats at least a portion of the surface of the core material,

wherein the core material comprises graphite, and the coating layer comprises a coating material containing a cyclic structure moiety, and wherein the composite graphite material has a weight-loss rate of from 0.1% to 0.55% when the composite graphite material is heated at a heating rate of 10° C./min or lower in an atmosphere of an inert non-oxidative gas at a temperature rising from 40° C. to 800° C., and wherein the cyclic structure moiety comprises one or more of Formulae 1 to 3:

10. The method according to claim 9 , characterized in that a mass ratio of the graphite core material to the cyclizable polymer, m G :m P , is from 40:1 to 200:1.

11. The method according to claim 9 , characterized in that the cyclizable polymer comprises one or more of polyacrylonitrile or copolymers thereof.

12. The method according to claim 9 , characterized in that the cyclizable polymer has a number average molecular weight of from 50,000 to 150,000 Da.

13. The method according to claim 9 , characterized in that in the step (3),

the powder is heat treated at a temperature between 350° C. and 400° C.; and/or

the heat treating time is from 3 hours to 6 hours.

14. A secondary battery comprising a negative electrode plate which comprises a negative active material, characterized in that the negative active material comprises a composite graphite material comprising a core material and a coating layer that coats at least a portion of the surface of the core material, characterized in that the core material comprises graphite, and the coating layer comprises a coating material containing a cyclic structure moiety, wherein the composite graphite material has a weight-loss rate of from 0.1% to 0.55% when the composite graphite material is heated at a heating rate of 10° C./min or lower in an atmosphere of an inert non-oxidative gas at a temperature rising from 40° C. to 800° C., and wherein the cyclic structure moiety comprises one or more of Formulae 1 to 3:

15. The secondary battery according to claim 14 , characterized in that the composite graphite material has a sulfur content of less than 0.02 wt. %.

16. The secondary battery according to claim 14 , characterized in that the core material is artificial graphite.

17. The secondary battery according to claim 16 , characterized in that the composite graphite material has a D-peak intensity I D and a G-peak intensity I G , and the ratio of I D /I G is from 0.4 to 1.0.

18. The secondary battery according to claim 16 , characterized in that the composite graphite material satisfies a ratio of the peak area C 004 of 004 crystal plane to the peak area C 110 of 110 crystal plane of the composite graphite material C 004 /C 110 ≤15, when the composite graphite material is in an electrode plate with a compaction density of from 1.6 g/cm 3 to 1.7 g/cm 3 .

19. The secondary battery according to claim 16 , characterized in that the composite graphite material further satisfies one or more of the following (1) to (6):

(1) the composite graphite material has a D v 50 of from 15 μm to 20 μm;

(2) the composite graphite material has a D v 10 of at least 6 μm;

(3) the composite graphite material has a D n 10 of from 1.0 μm to 3.0 μm;

(4) the composite graphite material has a specific surface area of from 0.5 m 2 /g to 1.2 m 2 /g;

(5) the composite graphite material has a compaction density under a pressure of 5 tons of from 1.80 g/cm 3 to 2.10 g/cm 3 ; and

(6) the composite graphite material has a tap density of from 0.8 g/cm 3 to 1.15 g/cm 3 .

20. The secondary battery according to claim 16 , characterized in that the composite graphite material further satisfies one or more of the following (1) to (6):

(1) the composite graphite material has a D v 50 of from 15 μm to 18 μm;

(2) the composite graphite material has a D v 10 of from 6.5 μm to 10.5 μm;

(3) the composite graphite material has a D n 10 of from 1.2 μm to 2.0 μm;

(4) the composite graphite material has a specific surface area of from 0.6 m 2 /g to 1.0 m 2 /g;

(5) the composite graphite material has a compaction density under a pressure of 5 tons of from 1.93 g/cm 3 to 2.05 g/cm 3 ; and

(6) the composite graphite material has a tap density of from 0.9 g/cm 3 to 1.05 g/cm 3 .

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 6, 2024
From: CONTEMPORARY AMPEREX TECHNOLOGY CO., LIMITED
To: CONTEMPORARY AMPEREX TECHNOLOGY (HONG KONG) LIMITED
Reel/Frame 068338/0402 →
Continuity (2)
Continuation PCTCN2019122743 · Dec 3, 2019
Related Publication 20220002160A1 · Jan 6, 2022
References Cited (44)
US 11710822B2 · Liang · 2023 [cited by examiner]
US 12021235B2 · He · 2024 [cited by examiner]
US 20090202917A1 · Sotowa · 2009 [cited by examiner]
US 20110183180A1 · Yu · 2011 [cited by examiner]
US 20120171103A1 · Zhao · 2012 [cited by examiner]
US 20120196193A1 · Sotowa · 2012 [cited by examiner]
US 20130040203A1 · Yoon · 2013 [cited by examiner]
US 20150349332A1 · Azami · 2015 [cited by examiner]
US 20150364751A1 · Wakizaka · 2015 [cited by examiner]
US 20190036121A1 · Cho et al. · 2019 [cited by applicant]
US 20190097271A1 · Wang · 2019 [cited by examiner]
US 20190214640A1 · Salem · 2019 [cited by examiner]
US 20200075941A1 · Kim · 2020 [cited by examiner]
US 20200313176A1 · Wang · 2020 [cited by examiner]
US 20210020898A1 · Lee · 2021 [cited by examiner]
US 20220123307A1 · Li · 2022 [cited by examiner]
US 20230187638A1 · Tian · 2023 [cited by examiner]
US 20240021775A1 · Cai · 2024 [cited by examiner]
US 20240113284A1 · Piao · 2024 [cited by examiner]
CN 101916846A · 2010 [cited by applicant]
CN 102299307A · 2011 [cited by applicant]
CN 103081191A · 2013 [cited by applicant]
CN 103688395A · 2014 [cited by applicant]
CN 106410200A · 2017 [cited by applicant]
CN 107743659A · 2018 [cited by applicant]
CN 106410200B · 2018 [cited by applicant]
CN 110072810A · 2019 [cited by applicant]
CN 110364690A · 2019 [cited by applicant]
EP 3872903A1 · 2021 [cited by applicant]
JP 10284080A · 1998 [cited by applicant]
JP 2013542559A · 2013 [cited by applicant]
KR 1020130046423A · 2013 [cited by applicant]
WO 2014048390A1 · 2014 [cited by applicant]
WO 2016123718A1 · 2016 [cited by applicant]
Polyaniline wikipedia entry to show bond structure (Year: 2024). [cited by examiner]
The extended European search report for EP Application No. 19954825.6, dated Mar. 2, 2022, 8 pages. [cited by applicant]
The First Office Action for JP Application No. 2022-520243, dated May 8, 2023, 6 pages. [cited by applicant]
The First Office Action for CN Application No. 201980066188.0, dated Sep. 30, 2023, 14 pages. [cited by applicant]
The Communication pursuant to Article 94(3) EPC for Europe an Application No. 19954825.6, dated Oct. 4, 2022, 6 pages. [cited by applicant]
The First Office Action forIndia Application No. 202217030957, dated Sep. 22, 2022, 6 pages. [cited by applicant]
The International search report for PCT Application No. PCT/CN2019/122743, dated Sep. 9, 2020, 13 pages. [cited by applicant]
Yao Shuhua et al. The structure property and application of conductive material of pyrolytic polyacrylonitrile. Journal of Northeast Normal University, Natural Science Edition, No. 1, vol. 33 ISSN: 1000-1832 Full Text, … [cited by applicant]
The First Office Action for the Korean Application No. 10-2022-7011947, dated Oct. 7, 2024, 19 pages. [cited by applicant]
Jeremy D.Moskowitz et al.Semibatch RAFT copolymerization of acrylonitrile and N-isopropylacrylamide: Effect of comonomer distribution on cyclization and thermal stability. Polymer 84 (2016) pp. 311˜318, dated Dec. 29, 2… [cited by applicant]