Difference between revisions of "BETA AIR, LLC patent applications published on November 30th, 2023"
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| + | '''Summary of the patent applications from BETA AIR, LLC on November 30th, 2023''' | ||
| + | |||
| + | BETA AIR, LLC has recently filed several patents related to various aspects of electric aircraft technology. These patents cover areas such as battery venting, active cooling systems, ground control systems, determination of limiting parameters, battery energy monitoring, flight mode guidance, recharging stations, and thermal energy management. | ||
| + | |||
| + | In summary, the patents filed by BETA AIR, LLC include: | ||
| + | |||
| + | - A venting assembly for battery ejecta in an electric aircraft, consisting of multiple battery packs and vents attached to each pack. | ||
| + | - An apparatus for actively cooling a battery pack, utilizing an active cooling system with coolant channels and passive heat transfer elements. | ||
| + | - An apparatus for automated ground control of an electric vertical takeoff and landing aircraft, involving a flight controller and a remote device for transmitting location data. | ||
| + | - An apparatus for determining the most limiting parameter of an electric aircraft, using a processor and memory to analyze aircraft data from a sensing device. | ||
| + | - An apparatus for determining the remaining energy of a battery pack in an electric aircraft, calculating reserve energy and resource remaining data based on aircraft data and flight mode. | ||
| + | - An apparatus for guiding the transition between flight modes of an electric aircraft, utilizing a sensor, flight controller, and pilot indicator to display movement and guidance data. | ||
| + | - An apparatus for determining the remaining energy of a battery in an electric aircraft, involving a processor and memory to analyze data from a sensing device. | ||
| + | - An apparatus and method for a recharging station for electric aircraft, featuring a landing pad, rechargeable component, and power delivery unit with multiple charging units. | ||
| + | - An apparatus for managing the thermal energy of an electric aircraft energy source, utilizing fins, a coolant system, and channels for heat dissipation. | ||
| + | |||
| + | Notable applications: | ||
| + | |||
| + | * Battery venting assembly for safe operation of electric aircraft. | ||
| + | * Active cooling system for efficient cooling of battery packs. | ||
| + | * Automated ground control system for easy navigation and charging. | ||
| + | * Determination of limiting parameters for enhanced safety and performance. | ||
| + | * Battery energy monitoring for efficient battery usage. | ||
| + | * Flight mode guidance for smooth transitions and pilot assistance. | ||
| + | * Recharging station for convenient and versatile aircraft charging. | ||
| + | * Thermal energy management for optimal performance and safety. | ||
| + | |||
| + | |||
| + | |||
| + | |||
==Patent applications for BETA AIR, LLC on November 30th, 2023== | ==Patent applications for BETA AIR, LLC on November 30th, 2023== | ||
| − | ===ELECTRIC CHARGING STATION FOR AN ELECTRIC VEHICLE AND A METHOD FOR ITS USE ([[US Patent Application 18130064. ELECTRIC CHARGING STATION FOR AN ELECTRIC VEHICLE AND A METHOD FOR ITS USE simplified abstract|18130064]])=== | + | ===ELECTRIC CHARGING STATION FOR AN ELECTRIC VEHICLE AND A METHOD FOR ITS USE ([[US Patent Application 18130064. ELECTRIC CHARGING STATION FOR AN ELECTRIC VEHICLE AND A METHOD FOR ITS USE simplified abstract (BETA AIR, LLC)|18130064]])=== |
| Line 9: | Line 39: | ||
| − | ===GROUND SERVICE SYSTEMS AND DEVICES FOR AN ELECTRIC AIRCRAFT ([[US Patent Application 18116020. GROUND SERVICE SYSTEMS AND DEVICES FOR AN ELECTRIC AIRCRAFT simplified abstract|18116020]])=== | + | ===GROUND SERVICE SYSTEMS AND DEVICES FOR AN ELECTRIC AIRCRAFT ([[US Patent Application 18116020. GROUND SERVICE SYSTEMS AND DEVICES FOR AN ELECTRIC AIRCRAFT simplified abstract (BETA AIR, LLC)|18116020]])=== |
| Line 17: | Line 47: | ||
| − | ===SYSTEMS AND METHODS FOR AN ELECTRIC VERTICAL TAKEOFF AND LANDING AIRCRAFT BRAKING SYSTEM ([[US Patent Application 18203857. SYSTEMS AND METHODS FOR AN ELECTRIC VERTICAL TAKEOFF AND LANDING AIRCRAFT BRAKING SYSTEM simplified abstract|18203857]])=== | + | ===SYSTEMS AND METHODS FOR AN ELECTRIC VERTICAL TAKEOFF AND LANDING AIRCRAFT BRAKING SYSTEM ([[US Patent Application 18203857. SYSTEMS AND METHODS FOR AN ELECTRIC VERTICAL TAKEOFF AND LANDING AIRCRAFT BRAKING SYSTEM simplified abstract (BETA AIR, LLC)|18203857]])=== |
| Line 25: | Line 55: | ||
| − | ===SYSTEMS AND DEVICES FOR PARKING A PROPULSOR TEETER ([[US Patent Application 18140247. SYSTEMS AND DEVICES FOR PARKING A PROPULSOR TEETER simplified abstract|18140247]])=== | + | ===SYSTEMS AND DEVICES FOR PARKING A PROPULSOR TEETER ([[US Patent Application 18140247. SYSTEMS AND DEVICES FOR PARKING A PROPULSOR TEETER simplified abstract (BETA AIR, LLC)|18140247]])=== |
| Line 33: | Line 63: | ||
| − | ===SYSTEMS AND METHODS FOR PROPULSOR SYNCHRONIZATION ([[US Patent Application 17752020. SYSTEMS AND METHODS FOR PROPULSOR SYNCHRONIZATION simplified abstract|17752020]])=== | + | ===SYSTEMS AND METHODS FOR PROPULSOR SYNCHRONIZATION ([[US Patent Application 17752020. SYSTEMS AND METHODS FOR PROPULSOR SYNCHRONIZATION simplified abstract (BETA AIR, LLC)|17752020]])=== |
| Line 41: | Line 71: | ||
| − | ===INTEGRATED THERMAL MANAGEMENT APPARATUS ([[US Patent Application 17827162. INTEGRATED THERMAL MANAGEMENT APPARATUS simplified abstract|17827162]])=== | + | ===INTEGRATED THERMAL MANAGEMENT APPARATUS ([[US Patent Application 17827162. INTEGRATED THERMAL MANAGEMENT APPARATUS simplified abstract (BETA AIR, LLC)|17827162]])=== |
| Line 49: | Line 79: | ||
| − | ===APPARATUS FOR DETERMINING A MOST LIMITING PARAMETER OF AN ELECTRIC AIRCRAFT ([[US Patent Application 17824472. APPARATUS FOR DETERMINING A MOST LIMITING PARAMETER OF AN ELECTRIC AIRCRAFT simplified abstract|17824472]])=== | + | ===APPARATUS FOR DETERMINING A MOST LIMITING PARAMETER OF AN ELECTRIC AIRCRAFT ([[US Patent Application 17824472. APPARATUS FOR DETERMINING A MOST LIMITING PARAMETER OF AN ELECTRIC AIRCRAFT simplified abstract (BETA AIR, LLC)|17824472]])=== |
| Line 57: | Line 87: | ||
| − | ===RECHARGING STATION FOR ELECTRIC AIRCRAFTS AND A METHOD OF ITS USE ([[US Patent Application 18137900. RECHARGING STATION FOR ELECTRIC AIRCRAFTS AND A METHOD OF ITS USE simplified abstract|18137900]])=== | + | ===RECHARGING STATION FOR ELECTRIC AIRCRAFTS AND A METHOD OF ITS USE ([[US Patent Application 18137900. RECHARGING STATION FOR ELECTRIC AIRCRAFTS AND A METHOD OF ITS USE simplified abstract (BETA AIR, LLC)|18137900]])=== |
| Line 65: | Line 95: | ||
| − | ===APPARATUS AND A METHOD FOR DETERMINING A RESOURCE REMAINING DATUM OF AN ELECTRIC AIRCRAFT ([[US Patent Application 17824382. APPARATUS AND A METHOD FOR DETERMINING A RESOURCE REMAINING DATUM OF AN ELECTRIC AIRCRAFT simplified abstract|17824382]])=== | + | ===APPARATUS AND A METHOD FOR DETERMINING A RESOURCE REMAINING DATUM OF AN ELECTRIC AIRCRAFT ([[US Patent Application 17824382. APPARATUS AND A METHOD FOR DETERMINING A RESOURCE REMAINING DATUM OF AN ELECTRIC AIRCRAFT simplified abstract (BETA AIR, LLC)|17824382]])=== |
| Line 73: | Line 103: | ||
| − | ===APPARATUS FOR GUIDING A TRANSITION BETWEEN FLIGHT MODES OF AN ELECTRIC AIRCRAFT ([[US Patent Application 18144659. APPARATUS FOR GUIDING A TRANSITION BETWEEN FLIGHT MODES OF AN ELECTRIC AIRCRAFT simplified abstract|18144659]])=== | + | ===APPARATUS FOR GUIDING A TRANSITION BETWEEN FLIGHT MODES OF AN ELECTRIC AIRCRAFT ([[US Patent Application 18144659. APPARATUS FOR GUIDING A TRANSITION BETWEEN FLIGHT MODES OF AN ELECTRIC AIRCRAFT simplified abstract (BETA AIR, LLC)|18144659]])=== |
| Line 81: | Line 111: | ||
| − | ===APPARATUS AND A METHOD FOR DETERMINING A RESOURCE REMAINING DATUM OF AN ELECTRIC AIRCRAFT ([[US Patent Application 17889538. APPARATUS AND A METHOD FOR DETERMINING A RESOURCE REMAINING DATUM OF AN ELECTRIC AIRCRAFT simplified abstract|17889538]])=== | + | ===APPARATUS AND A METHOD FOR DETERMINING A RESOURCE REMAINING DATUM OF AN ELECTRIC AIRCRAFT ([[US Patent Application 17889538. APPARATUS AND A METHOD FOR DETERMINING A RESOURCE REMAINING DATUM OF AN ELECTRIC AIRCRAFT simplified abstract (BETA AIR, LLC)|17889538]])=== |
| Line 89: | Line 119: | ||
| − | ===APPARATUS FOR DETERMINING A MOST LIMITING PARAMETER OF AN ELECTRIC AIRCRAFT ([[US Patent Application 17824546. APPARATUS FOR DETERMINING A MOST LIMITING PARAMETER OF AN ELECTRIC AIRCRAFT simplified abstract|17824546]])=== | + | ===APPARATUS FOR DETERMINING A MOST LIMITING PARAMETER OF AN ELECTRIC AIRCRAFT ([[US Patent Application 17824546. APPARATUS FOR DETERMINING A MOST LIMITING PARAMETER OF AN ELECTRIC AIRCRAFT simplified abstract (BETA AIR, LLC)|17824546]])=== |
| Line 97: | Line 127: | ||
| − | ===APPARATUS AND METHODS FOR AUTOMATED CONTROL OF AN ELECTRIC VERTICAL TAKEOFF AND LANDING AIRCRAFT ([[US Patent Application 17751824. APPARATUS AND METHODS FOR AUTOMATED CONTROL OF AN ELECTRIC VERTICAL TAKEOFF AND LANDING AIRCRAFT simplified abstract|17751824]])=== | + | ===APPARATUS AND METHODS FOR AUTOMATED CONTROL OF AN ELECTRIC VERTICAL TAKEOFF AND LANDING AIRCRAFT ([[US Patent Application 17751824. APPARATUS AND METHODS FOR AUTOMATED CONTROL OF AN ELECTRIC VERTICAL TAKEOFF AND LANDING AIRCRAFT simplified abstract (BETA AIR, LLC)|17751824]])=== |
| Line 105: | Line 135: | ||
| − | ===APPARATUS FOR ACTIVE BATTERY PACK COOLING ([[US Patent Application 17752117. APPARATUS FOR ACTIVE BATTERY PACK COOLING simplified abstract|17752117]])=== | + | ===APPARATUS FOR ACTIVE BATTERY PACK COOLING ([[US Patent Application 17752117. APPARATUS FOR ACTIVE BATTERY PACK COOLING simplified abstract (BETA AIR, LLC)|17752117]])=== |
| Line 113: | Line 143: | ||
| − | ===VENTING ASSEMBLY FOR BATTERY EJECTA ON A SIDE DIFFERENT FROM AN EGRESS ([[US Patent Application 18090387. VENTING ASSEMBLY FOR BATTERY EJECTA ON A SIDE DIFFERENT FROM AN EGRESS simplified abstract|18090387]])=== | + | ===VENTING ASSEMBLY FOR BATTERY EJECTA ON A SIDE DIFFERENT FROM AN EGRESS ([[US Patent Application 18090387. VENTING ASSEMBLY FOR BATTERY EJECTA ON A SIDE DIFFERENT FROM AN EGRESS simplified abstract (BETA AIR, LLC)|18090387]])=== |
Latest revision as of 06:39, 7 December 2023
Summary of the patent applications from BETA AIR, LLC on November 30th, 2023
BETA AIR, LLC has recently filed several patents related to various aspects of electric aircraft technology. These patents cover areas such as battery venting, active cooling systems, ground control systems, determination of limiting parameters, battery energy monitoring, flight mode guidance, recharging stations, and thermal energy management.
In summary, the patents filed by BETA AIR, LLC include:
- A venting assembly for battery ejecta in an electric aircraft, consisting of multiple battery packs and vents attached to each pack. - An apparatus for actively cooling a battery pack, utilizing an active cooling system with coolant channels and passive heat transfer elements. - An apparatus for automated ground control of an electric vertical takeoff and landing aircraft, involving a flight controller and a remote device for transmitting location data. - An apparatus for determining the most limiting parameter of an electric aircraft, using a processor and memory to analyze aircraft data from a sensing device. - An apparatus for determining the remaining energy of a battery pack in an electric aircraft, calculating reserve energy and resource remaining data based on aircraft data and flight mode. - An apparatus for guiding the transition between flight modes of an electric aircraft, utilizing a sensor, flight controller, and pilot indicator to display movement and guidance data. - An apparatus for determining the remaining energy of a battery in an electric aircraft, involving a processor and memory to analyze data from a sensing device. - An apparatus and method for a recharging station for electric aircraft, featuring a landing pad, rechargeable component, and power delivery unit with multiple charging units. - An apparatus for managing the thermal energy of an electric aircraft energy source, utilizing fins, a coolant system, and channels for heat dissipation.
Notable applications:
- Battery venting assembly for safe operation of electric aircraft.
- Active cooling system for efficient cooling of battery packs.
- Automated ground control system for easy navigation and charging.
- Determination of limiting parameters for enhanced safety and performance.
- Battery energy monitoring for efficient battery usage.
- Flight mode guidance for smooth transitions and pilot assistance.
- Recharging station for convenient and versatile aircraft charging.
- Thermal energy management for optimal performance and safety.
Contents
- 1 Patent applications for BETA AIR, LLC on November 30th, 2023
- 1.1 ELECTRIC CHARGING STATION FOR AN ELECTRIC VEHICLE AND A METHOD FOR ITS USE (18130064)
- 1.2 GROUND SERVICE SYSTEMS AND DEVICES FOR AN ELECTRIC AIRCRAFT (18116020)
- 1.3 SYSTEMS AND METHODS FOR AN ELECTRIC VERTICAL TAKEOFF AND LANDING AIRCRAFT BRAKING SYSTEM (18203857)
- 1.4 SYSTEMS AND DEVICES FOR PARKING A PROPULSOR TEETER (18140247)
- 1.5 SYSTEMS AND METHODS FOR PROPULSOR SYNCHRONIZATION (17752020)
- 1.6 INTEGRATED THERMAL MANAGEMENT APPARATUS (17827162)
- 1.7 APPARATUS FOR DETERMINING A MOST LIMITING PARAMETER OF AN ELECTRIC AIRCRAFT (17824472)
- 1.8 RECHARGING STATION FOR ELECTRIC AIRCRAFTS AND A METHOD OF ITS USE (18137900)
- 1.9 APPARATUS AND A METHOD FOR DETERMINING A RESOURCE REMAINING DATUM OF AN ELECTRIC AIRCRAFT (17824382)
- 1.10 APPARATUS FOR GUIDING A TRANSITION BETWEEN FLIGHT MODES OF AN ELECTRIC AIRCRAFT (18144659)
- 1.11 APPARATUS AND A METHOD FOR DETERMINING A RESOURCE REMAINING DATUM OF AN ELECTRIC AIRCRAFT (17889538)
- 1.12 APPARATUS FOR DETERMINING A MOST LIMITING PARAMETER OF AN ELECTRIC AIRCRAFT (17824546)
- 1.13 APPARATUS AND METHODS FOR AUTOMATED CONTROL OF AN ELECTRIC VERTICAL TAKEOFF AND LANDING AIRCRAFT (17751824)
- 1.14 APPARATUS FOR ACTIVE BATTERY PACK COOLING (17752117)
- 1.15 VENTING ASSEMBLY FOR BATTERY EJECTA ON A SIDE DIFFERENT FROM AN EGRESS (18090387)
Patent applications for BETA AIR, LLC on November 30th, 2023
ELECTRIC CHARGING STATION FOR AN ELECTRIC VEHICLE AND A METHOD FOR ITS USE (18130064)
Main Inventor
John Charles Palombini
GROUND SERVICE SYSTEMS AND DEVICES FOR AN ELECTRIC AIRCRAFT (18116020)
Main Inventor
Jake Pill
SYSTEMS AND METHODS FOR AN ELECTRIC VERTICAL TAKEOFF AND LANDING AIRCRAFT BRAKING SYSTEM (18203857)
Main Inventor
Lochie Ferrier
SYSTEMS AND DEVICES FOR PARKING A PROPULSOR TEETER (18140247)
Main Inventor
Kyle Brookes
SYSTEMS AND METHODS FOR PROPULSOR SYNCHRONIZATION (17752020)
Main Inventor
Collin Freiheit
INTEGRATED THERMAL MANAGEMENT APPARATUS (17827162)
Main Inventor
Braedon Lohe
APPARATUS FOR DETERMINING A MOST LIMITING PARAMETER OF AN ELECTRIC AIRCRAFT (17824472)
Main Inventor
Thomas Henck
RECHARGING STATION FOR ELECTRIC AIRCRAFTS AND A METHOD OF ITS USE (18137900)
Main Inventor
Jake Pill
APPARATUS AND A METHOD FOR DETERMINING A RESOURCE REMAINING DATUM OF AN ELECTRIC AIRCRAFT (17824382)
Main Inventor
Steven J. Foland
APPARATUS FOR GUIDING A TRANSITION BETWEEN FLIGHT MODES OF AN ELECTRIC AIRCRAFT (18144659)
Main Inventor
Thomas Henck
APPARATUS AND A METHOD FOR DETERMINING A RESOURCE REMAINING DATUM OF AN ELECTRIC AIRCRAFT (17889538)
Main Inventor
Steven J. Foland
APPARATUS FOR DETERMINING A MOST LIMITING PARAMETER OF AN ELECTRIC AIRCRAFT (17824546)
Main Inventor
Herman Wiegman
APPARATUS AND METHODS FOR AUTOMATED CONTROL OF AN ELECTRIC VERTICAL TAKEOFF AND LANDING AIRCRAFT (17751824)
Main Inventor
John Charles Palombini
APPARATUS FOR ACTIVE BATTERY PACK COOLING (17752117)
Main Inventor
Nathan Goldsberry
VENTING ASSEMBLY FOR BATTERY EJECTA ON A SIDE DIFFERENT FROM AN EGRESS (18090387)
Main Inventor
Braedon Lohe
