Variable switched dc-to-dc voltage converter
US-2015015340-A1 · Jan 15, 2015 · US
US10050522B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10050522-B2 |
| Application number | US-201514861058-A |
| Country | US |
| Kind code | B2 |
| Filing date | Sep 22, 2015 |
| Priority date | Feb 15, 2015 |
| Publication date | Aug 14, 2018 |
| Grant date | Aug 14, 2018 |
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According to some implementation, a charge pump includes a boost charge pump circuit and a buck charge pump circuit sharing a common flying capacitance. In some implementations, the boost pump circuit includes an input node and a boosted-voltage output node, and the buck charge pump circuit includes the input node and a divided-voltage output node. In some implementations, the charge pump of claim 3 wherein the boosted-voltage includes 2×Vin, and the divided-voltage includes Vin/2, Vin being an input voltage at the input node. In some implementations, the boost pump circuit further includes a first holding capacitance that couples the boosted-voltage output node to a ground. In some implementations, the buck pump circuit further includes a second holding capacitance that couples the divided-voltage output node to the ground.
Opening claim text (preview).
What is claimed is: 1. A charge pump comprising a boost charge pump circuit including an input node and a boosted-voltage output node, and a buck charge pump circuit including the input node and a divided-voltage output node sharing a common flying capacitance, the common flying capacitance configured to be partially charged to less than an input voltage during a phase of output voltage generation and configured to undergo truncated charging to limit a ripple effect in a hysteretic feedback loop, the boost charge pump circuit including a first holding capacitance that couples the boosted-voltage output node to a ground, the boost charge pump circuit and the buck charge pump circuit each including a plurality of switches implemented to incorporate the common flying capacitance and generate output voltages having magnitudes 2×Vbatt and Vbatt/2 respectively. 2. The charge pump of claim 1 wherein said plurality of switches includes a first switch (S 1 ) and a second switch (S 2 ) arranged in parallel between the input node and respective ends of the flying capacitance. 3. The charge pump of claim 2 wherein said plurality of switches includes a third switch (S 3 ) between the second end of the flying capacitance and the ground. 4. The charge pump of claim 3 wherein said plurality of switches includes a fourth switch (S 4 ) between the first end of the flying capacitance and the boosted-voltage output node. 5. The charge pump of claim 4 wherein said plurality of switches includes a fifth switch (S 5 ) between the first end of the flying capacitance and the divided-voltage output node. 6. The charge pump of claim 1 wherein the buck pump circuit further includes a second holding capacitance that couples the divided-voltage output node to the ground. 7. The charge pump of claim 5 wherein said plurality of switches includes a sixth switch (S 6 ) between the second end of the flying capacitance and the divided-voltage output node. 8. The charge pump of claim 7 wherein the switches S 1 , S 2 , S 3 , S 4 , S 5 and S 6 are configured to operate in four phases to yield the output voltages having magnitudes 2×Vbatt and Vbatt/2. 9. The charge pump of claim 8 wherein the first phase includes closed S 1 and S 6 and open S 2 to S 5 , the second phase includes closed S 3 and S 5 and open S 1 , S 2 , S 4 and S 6 , the third phase includes closed S 1 and S 3 and open S 2 and S 4 to S 6 , and the fourth phase includes closed S 2 and S 4 and open S 1 , S 3 , S 5 and S 6 . 10. The charge pump of claim 8 wherein the first phase includes closed S 1 and S 6 and open S 2 to S 5 , the second phase includes closed S 3 and S 5 and open S 1 , S 2 , S 4 and S 6 , the third phase includes closed S 1 and S 6 and open S 2 to S 5 , and the fourth phase includes closed S 2 and S 4 and open S 1 , S 3 , S 5 and S 6 . 11. The charge pump of claim 10 wherein the third phase includes partial charging of the flying capacitance to improve charge preservation. 12. The charge pump of claim 8 wherein the first phase includes closed S 1 and S 6 and open S 2 to S 5 , the second phase includes closed S 3 and S 5 and open S 1 , S 2 , S 4 and S 6 , the third phase includes closed S 1 and S 6 and open S 2 to S 5 , and the fourth phase includes closed S 3 and S 5 and open S 1 , S 2 , S 4 and S 6 . 13. The charge pump of claim 12 wherein the fourth phase includes truncated charging of the flying capacitance to limit ripple effect in hysteretic feedback loop. 14. A voltage supply system comprising: a boost converter configured to generate a boosted voltage based on a battery voltage Vbatt; and a charge pump having a boost charge pump circuit including an input node and a boosted-voltage output node, and a buck charge pump circuit including the input node and a divided-voltage output node sharing a common flying capacitance, the common flying capacitance configured to be partially charged to less than an input voltage during a phase of output voltage generation and configured to undergo truncated charging to limit ripple effect in a hysteretic feedback loop, the boost charge pump circuit including a first holding capacitance that couples the boosted-voltage output node to a ground, the boost charge pump circuit and the buck charge pump circuit each including a plurality of switches implemented to incorporate the common flying capacitance and generate output voltages having magnitudes 2×Vbatt and Vbatt/2 respectively. 15. The voltage supply system of claim 14 wherein the buck pump circuit further includes a second holding capacitance that couples the divided-voltage output node to the ground. 16. The voltage supply system of claim 15 wherein said plurality of switches includes a first switch (S 1 ) and a second switch (S 2 ) arranged in parallel between the input node and respective ends of the flying capacitance, a third switch (S 3 ) between the second end of the flying capacitance and the ground, a fourth switch (S 4 ) between the first end of the flying capacitance and the boosted-voltage output node, a fifth switch (S 5 ) between the first end of the flying capacitance and the divided-voltage output node, and a sixth switch (S 6 ) second end of the flying capacitance and the divided-voltage output node. 17. The voltage supply system of claim 16 wherein switches S 1 , S 2 , S 3 , S 4 , S 5 and S 6 are configured to operate in four phases to yield the output voltages having magnitudes 2×Vbatt and Vbatt/2. 18. A radio-frequency (RF) module comprising: a packaging substrate configured to receive a plurality of components; and a power amplification system implemented on the packaging substrate, the power amplification system including a voltage supply system, the voltage supply system including a charge pump having a boost charge pump circuit including an input node and a boosted-voltage output node, and a buck charge pump circuit including the input node and a divided-voltage output node sharing a common flying capacitance, the common flying capacitance configured to be partially charged to less than an input voltage during a phase of output voltage generation and configured to undergo truncated charging to limit ripple effect in a hysteretic feedback loop, the boost charge pump circuit including a first holding capacitance that couples the boosted-voltage output node to a ground, the boost charge pump circuit and the buck charge pump circuit each including a plurality of switches implemented to incorporate the common flying capacitance and generate output voltages having magnitudes 2×Vbatt and Vbatt/2 respectively. 19. The RF module of claim 18 wherein; the buck pump circuit further includes a second holding capacitance that couples the divided-voltage output node to the ground. 20. The RF module of claim 19 wherein said plurality of switches includes a first switch (S 1 ) and a second switch (S 2 ) arranged in parallel between the input node and respective ends of the flying capacitance, a third switch (S 3 ) between the second end of the flying capacitance and the ground, a fourth switch (S 4 ) between the first end of the flying capacitance and the boosted-voltage output node, a fifth switch (S 5 ) between the first end of the flying capacitance and the divided-voltage output node, and a sixth switch (S 6 ) between the second end of the flying capacitance and the divided-voltage output node.
Charge pumps of the Schenkel-type · CPC title
Electricity · mapped topic
Electricity · mapped topic
Electricity · mapped topic
the clock signals being boosted to a value being higher than the input voltage value · CPC title
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