NEXT GENERATION HYDROGEN FUEL CELL SYSTEMS

is developing the next generation hydrogen fuel cell system with
zero CO2 emissions and game-changing energy performance
for the air transportation and urban air mobility market.
HyPoint, Inc.
is developing the next generation hydrogen fuel cell system with zero CO2 emissions and game-changing energy performance for the air transportation and urban air mobility market.
HyPoint, Inc.
Our Solution
Utilization rate
10X
Faster charge
TCO
90%
specific power
3X
power output
4X
20X
lifespan
4X
0%
CO2 emissions
vs. existing hydrogen FC
Turbo Air-Cooled Systems
Our Solution
Utilization rate
10X
Faster charge
TCO
90%
specific power
3X
power output
4X
20X
lifespan
4X
0%
CO2 emissions
vs. existing hydrogen FC
Turbo Air-Cooled Systems
Our Solution
Utilization rate
10X
Faster charge
specific power
3X
power output
4X
20X
lifespan
4X
0%
CO2 emissions
vs. existing hydrogen FC
Turbo Air-Cooled Systems
Now the main powertrains for prototyping of eVTOLs are built on Li-ion batteries, which have a fundamental barrier at a chemistry level.

Hydrogen has a potential to satisfy air transportation requirements
and might be a solution.
Measurable Benefits
Utilization rate
10X
Faster charge
20X
TCO
90%
Operational time
5X
Our patented technology increases operational time and utilization rate while decreasing TCO of any flying platform.
Now the main powertrains for prototyping of eVTOLs are built on Li-ion batteries, which have a fundamental barrier at a chemistry level.

Hydrogen has a potential to satisfy air transportation requirements
and might be a solution.
Measurable Benefits
Utilization rate
10X
Faster charge
20X
TCO
90%
Operational time
5X
Our patented technology increases operational time and utilization rate while decreasing TCO of any flying platform.
Now the main powertrains for prototyping of eVTOLs are built on Li-ion batteries, which have a fundamental barrier at a chemistry level.

Hydrogen has a potential to satisfy air transportation requirements
and might be a solution.
Measurable Benefits
Utilization rate
10X
Faster charge
20X
TCO
90%
Operational time
5X
Our patented technology increases operational time and utilization rate while decreasing TCO of any flying platform.
How Is This Possible?
1
2
3
Air-Cooled Fuel Cell
3
2
6
5
HyPoint's Turbo Air-Cooled Fuel Cell Systems offer a lighter-weight, simpler design than that of liquid-cooled ones, which allows
to achieve game-changing specific power and energy density.

Details
Ambient air
Air compression system
Compressed air
4
1
4
5
6
Heated air
Heat exchanger
Air drop
This invention allows us to maximize the power output of a PEM FC stack without adding essential 'parasitic' mass related to liquid-cooling. The idea is to deploy the open-cathode PEM FC stack in an air duct where pressurized (turbo), humidified and thermally stabilized air is circulated by means of fans. The compression of air is maintained (2-3 bars) inside an air duct by means of a compression system. The air duct is provided with a controlled throttle valve for partial discharge of air with reduced oxygen content (12%-16%). Discharged air is replaced with fresh compressed air with normal oxygen content. Thermal stabilization and humidification of air is provided by its recirculation. Water produced by fuel cells supports 100% relative humidity of circulated air. Condensed water is dropped out with discharged air.

Patents pending
How Is This Possible?
1
2
3
Air-Cooled Fuel Cell
3
2
6
5
HyPoint's Turbo Air-Cooled Fuel Cell Systems offer a lighter-weight, simpler design than that of liquid-cooled ones, which allows
to achieve game-changing specific power and energy density.

Details
Ambient air
Air compression system
Compressed air
4
1
4
5
6
Heated air
Heat exchanger
Air drop
This invention allows us to maximize the power output of a PEM FC stack without adding essential 'parasitic' mass related to liquid-cooling. The idea is to deploy the open-cathode PEM FC stack in an air duct where pressurized (turbo), humidified and thermally stabilized air is circulated by means of fans. The compression of air is maintained (2-3 bars) inside an air duct by means of a compression system. The air duct is provided with a controlled throttle valve for partial discharge of air with reduced oxygen content (12%-16%). Discharged air is replaced with fresh compressed air with normal oxygen content. Thermal stabilization and humidification of air is provided by its recirculation. Water produced by fuel cells supports 100% relative humidity of circulated air. Condensed water is dropped out with discharged air.

Patents pending
How Is This
Possible?
1
2
3
Air-Cooled Fuel Cell
3
2
6
5
HyPoint's Turbo Air-Cooled Fuel Cell Systems offer a lighter-weight, simpler design than that of liquid-cooled ones, which allows
to achieve game-changing specific power and energy density.

Details
Ambient air
Air compression system
Compressed air
4
1
4
5
6
Heated air
Heat exchanger
Air drop
This invention allows us to maximize the power output of a PEM FC stack without adding essential 'parasitic' mass related to liquid-cooling. The idea is to deploy the open-cathode PEM FC stack in an air duct where pressurized (turbo), humidified and thermally stabilized air is circulated by means of fans. The compression of air is maintained (2-3 bars) inside an air duct by means of a compression system. The air duct is provided with a controlled throttle valve for partial discharge of air with reduced oxygen content (12%-16%). Discharged air is replaced with fresh compressed air with normal oxygen content. Thermal stabilization and humidification of air is provided by its recirculation. Water produced by fuel cells supports 100% relative humidity of circulated air. Condensed water is dropped out with discharged air.

Patents pending
Detailed Benchmarking
*Estimation for 250 kg of total weight of a system including FC
and hydrogen tanks with 8% hydrogen mass ratio
Regular
Air-Cooled FC


Type
LTPEM

Specific power
[Stack] - 1200 W/kg
[System] - 800 W/kg

Energy Density
[Full System] - 500 Wh/kg

$/kW
[In mass production]
3000 $/kW
Best
Liquid-Cooled FC


Type
LTPEM

Specific power
[Stack] - 2000 W/kg
[System] - 250-800 W/kg

Energy Density
[Full System] - 530 Wh/kg*

$/kW [In mass production]
300-600 $/kW

HyPoint Demonstrated
Air-Cooled

Type
LTPEM

Specific power
[Stack] - 1500 W/kg
[System] - 1000 W/kg

Energy Density
[Full System] - 530 Wh/kg

$/kW
[In mass production]
800-1000 $/kW
HyPoint NEW
Turbo Air-Cooled


Type
LTPEM/HTPEM

Specific power
[Stack] - 4000 W/kg
[System] - 2000 W/kg

Energy Density
[Full System] - 960 Wh/kg*

$/kW [In mass production] 100-500 $/kW

Detailed Benchmarking
*Estimation for 250 kg of total weight of a system including FC
and hydrogen tanks with 8% hydrogen mass ratio
Regular
Air-Cooled FC


Type
LTPEM

Specific power
[Stack] - 1200 W/kg
[System] - 800 W/kg

Energy Density
[Full System] - 500 Wh/kg

$/kW
[In mass production]
3000 $/kW
Best
Liquid-Cooled FC


Type
LTPEM

Specific power
[Stack] - 2000 W/kg
[System] - 250-800 W/kg

Energy Density
[Full System] - 530 Wh/kg*

$/kW [In mass production]
300-600 $/kW

HyPoint Demonstrated
Air-Cooled

Type
LTPEM

Specific power
[Stack] - 1500 W/kg
[System] - 1000 W/kg

Energy Density
[Full System] - 530 Wh/kg

$/kW
[In mass production]
800-1000 $/kW
HyPoint NEW
Turbo Air-Cooled


Type
LTPEM/HTPEM

Specific power
[Stack] - 4000 W/kg
[System] - 2000 W/kg

Energy Density
[Full System] - 960 Wh/kg*

$/kW [In mass production] 100-500 $/kW

Detailed
Benchmarking
*Estimation for 250 kg of total weight of a system including FC and hydrogen tanks with 8% hydrogen mass ratio
Range Of Product
20-50 kW
Logistic
Drones
50-120 kW
e-VTOLs,
AirTaxis
150-300 kW
e-Aircrafts
Configuration Of Systems
Customer 1
Cruise/Peak
mode power
FC Powertrain
Buffer battery
Refueled
hydrogen cylinders
Total energy
system weight
Total energy capacity
Energy density
Flight duration

45/280 kW

30 kg
30 kg

105 kg


180 kg


150 kWh

835 wh/kg
200 min
Customer 2
Cruise/Peak
mode power
FC Powertrain
Buffer battery
Refueled
hydrogen cylinders
Total energy
system weight
Total energy capacity
Energy density
Flight duration

60/144 kW

30 kg
30 kg

58 kg


124 kg


85 kWh

690 wh/kg
95 min
Customer 3
Cruise/Peak
mode power
FC Powertrain
Buffer battery
Refueled
hydrogen cylinders
Total energy
system weight
Total energy capacity
Energy density
Flight duration

125/150 kW

65 kg


395 kg


480 kg


500 kWh

1040 wh/kg
240 min
Customer 4
Cruise/Peak
mode power
FC Powertrain
Buffer battery
Refueled
hydrogen cylinders
Total energy
system weight
Total energy capacity
Energy density
Flight duration

65/110 kW

33 kg
15 kg

77 kg


134 kg


96 kWh

715 wh/kg
90 min
Range Of Product
20-50 kW
Logistic
Drones
50-120 kW
e-VTOLs,
AirTaxis
150-300 kW
e-Aircrafts
Configuration Of Systems
Customer 1
Cruise/Peak
mode power
FC Powertrain
Buffer battery
Refueled
hydrogen cylinders
Total energy
system weight
Total energy capacity
Energy density
Flight duration

45/280 kW

30 kg
30 kg

105 kg


180 kg


150 kWh

835 wh/kg
200 min
Customer 2
Cruise/Peak
mode power
FC Powertrain
Buffer battery
Refueled
hydrogen cylinders
Total energy
system weight
Total energy capacity
Energy density
Flight duration

60/144 kW

30 kg
30 kg

58 kg


124 kg


85 kWh

690 wh/kg
95 min
Customer 3
Cruise/Peak
mode power
FC Powertrain
Buffer battery
Refueled
hydrogen cylinders
Total energy
system weight
Total energy capacity
Energy density
Flight duration

125/150 kW

65 kg


395 kg


480 kg


500 kWh

1040 wh/kg
240 min
Customer 4
Cruise/Peak
mode power
FC Powertrain
Buffer battery
Refueled
hydrogen cylinders
Total energy
system weight
Total energy capacity
Energy density
Flight duration

65/110 kW

33 kg
15 kg

77 kg


134 kg


96 kWh

715 wh/kg
90 min
Range
Of Product
20-50 kW
Logistic
Drones
50-120 kW
e-VTOLs,
AirTaxis
150-300 kW
e-Aircrafts
Configuration Of Systems
Power Team
10 years in business development in Fortune 100 companies
Sergey
Shubenkov

R&D/PhD
Sergey
Panov

CTO/PhD
Sergey
Nefedkin

Chief Scientist
Alex
Ivanenko

CEO/PhD
15 years in R&D hydrogen technologies

Worked in Ginzburg's team
Nobel Laureate in Physics
17 years experience in special power sources development
40+ years of research
in hydrogen technologies

140 scientific papers
15 patents
Advisory board
#Google #McKinsey&Co #ZeroAvia #eMotorsWerks / Enel
Val Miftakhov
PhD
#University of South Carolina
Awarded by #NASA Funded by #DOE #BASF
Brian C. Benicewicz
PhD
#Mercedes-Benz #Daimler Fuel Cell #KeraCel
Arwed Niestroj
#Admirals Bank #Soligent
#Yale University
Russell Sprole
MBA
#PlugPower
#H2Pump #Combined Energies
Rhonda Staudt
PhD
Our partners
Power Team
10 years in business development in Fortune 100 companies
Sergey
Shubenkov

R&D/PhD
Sergey
Panov

CTO/PhD
Sergey
Nefedkin

Chief Scientist
Alex
Ivanenko

CEO/PhD
15 years in R&D hydrogen technologies

Worked in Ginzburg's team
Nobel Laureate in Physics
17 years experience in special power sources development
40+ years of research
in hydrogen technologies

140 scientific papers
15 patents
Advisory board
#Google #McKinsey&Co #ZeroAvia #eMotorsWerks / Enel
Val Miftakhov
PhD
#University of South Carolina
Awarded by #NASA Funded by #DOE #BASF
Brian C. Benicewicz
PhD
#Mercedes-Benz #Daimler Fuel Cell #KeraCel
Arwed Niestroj
#Admirals Bank #Soligent
#Yale University
Russell Sprole
MBA
#PlugPower
#H2Pump #Combined Energies
Rhonda Staudt
PhD
Our partners
Power Team
Advisory board
#Google #McKinsey&Co #ZeroAvia #eMotorsWerks / Enel
Val Miftakhov
PhD
#University of South Carolina
Awarded by #NASA Funded by #DOE #BASF
Brian C. Benicewicz
PhD
#Mercedes-Benz #Daimler Fuel Cell #KeraCel
Arwed Niestroj
#Admirals Bank #Soligent
#Yale University
Russell Sprole
MBA
#PlugPower
#H2Pump #Combined Energies
Rhonda Staudt
PhD
Our partners
Contact Us
HyPoint Inc.101 Jefferson Dr., Menlo Park, CA, USA, 94025
2019-2020
Member of Class 24
Contact Us
HyPoint Inc.
101 Jefferson Dr., Menlo Park, CA, USA, 94025
2019-2020
Member of Class 24