US20230202685A1 - Vehicle with a propulsion system enclosed in a sealed container - Google Patents

Vehicle with a propulsion system enclosed in a sealed container Download PDF

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Publication number
US20230202685A1
US20230202685A1 US17/822,471 US202217822471A US2023202685A1 US 20230202685 A1 US20230202685 A1 US 20230202685A1 US 202217822471 A US202217822471 A US 202217822471A US 2023202685 A1 US2023202685 A1 US 2023202685A1
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United States
Prior art keywords
sealed container
vehicle
propulsion system
intake
stream
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Abandoned
Application number
US17/822,471
Inventor
Alfred Dennis Belen, III
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Individual
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Individual
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Priority to US17/822,471 priority Critical patent/US20230202685A1/en
Priority to PCT/US2022/042844 priority patent/WO2023129216A1/en
Publication of US20230202685A1 publication Critical patent/US20230202685A1/en
Priority to US18/406,367 priority patent/US20240140620A1/en
Abandoned legal-status Critical Current

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/42Arrangements or adaptations of power supply systems
    • B64G1/44Arrangements or adaptations of power supply systems using radiation, e.g. deployable solar arrays
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40Arrangements or adaptations of propulsion systems
    • B64G1/409Unconventional spacecraft propulsion systems
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40Arrangements or adaptations of propulsion systems
    • B64G1/411Electric propulsion
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/60Crew or passenger accommodations
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03HPRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03H99/00Subject matter not provided for in other groups of this subclass

Definitions

  • the present invention relates to a vehicle with a propulsion system and, more particularly, to a vehicle with a propulsion system enclosed in a sealed container.
  • a propeller or jet turbine type propulsion system generates a force, such as thrust.
  • the thrust is formed as an air stream or matter is ejected or propelled away from a vehicle. The air stream or matter ejected is not recycled and is lost to the vehicle's system.
  • a vehicle comprises a sealed container, a propulsion system with an intake and an exhaust affixed to an interior of the sealed container, an exhaust stream emitted from the exhaust of the propulsion system, a thrust corridor within the sealed container, positioned adjacent to the exhaust of the propulsion system configured to channel the exhaust stream, and a return corridor within the sealed container, positioned adjacent to the intake of the propulsion system configured to channel an intake stream into the intake of the propulsion system wherein the exhaust stream transforms into the intake stream after traveling a sufficient distance within the sealed container wherein the exhaust stream and intake stream generate a pressure differential within the sealed container wherein the pressure differential is sufficient to result in a movement of the vehicle relative to the vehicle's surroundings.
  • the FIGURE is a schematic view of a vehicle in a sealed container according to an embodiment of the present invention.
  • an embodiment of the present invention provides a propulsion system enclosed in a sealed container.
  • the propulsion of the present invention may be a propeller or a turbine.
  • a main or primary fuel source for the system may be electricity so as to remove the need for costly and expendable chemical reactions and/or fossil fuels. Said electricity may be generated by solar power.
  • An electric turbine, an electric propellor, and/or an electric motor may enable thrust production via electrical means instead of chemical fuels.
  • the propulsion system is enclosed in and affixed to an interior of a sealed or airtight container.
  • the sealed container may form, enclose, and/or encompass a vehicle system.
  • a steering mechanism may be equipped to the container to direct or steer the container.
  • Such steering mechanism may be a rudder.
  • the atmosphere within the container forms streams including at least one exhaust stream and at least one return stream.
  • the return stream may also be referred to as an intake stream.
  • the exhaust stream may be ejected from a rear end of the propulsion system or an exhaust end.
  • the exhaust stream may be redirected or deflected by a wall or a chamber to a front end of the propulsion system.
  • the walls may form a thrust corridor, for the exhaust stream to exit to propulsion system, and a return corridor, for the exhaust stream to return an entrance of the propulsion system. By traveling through the return corridor, the exhaust stream may then re-enter the propulsion system at an intake section.
  • the sealed container of the present invention enables the exhaust stream to be recycled and reused indefinitely without the exhaust stream escaping the sealed container.
  • the propulsion system may include an intake and an exhaust.
  • the exhaust may emit or release an exhaust stream.
  • the exhaust stream may be an expanded or expanding gas. After traveling a sufficient distance, the exhaust stream may circulate, circle, navigate, or travel the sealed container and transform to the intake stream.
  • the thrust corridor may simultaneously transform to the return corridor when the exhaust stream transforms into the intake stream. This may be when the expanding gas is no longer expanding or when a pressure differential caused by the exhaust stream changes sufficiently.
  • the intake stream may re-enter the propulsion system. In some embodiments, no portion of the intake stream or the exhaust stream exits the sealed container or the vehicle system.
  • the walls may be affixed to an interior of the sealed container.
  • the propulsion system including the motor may be affixed to the sealed container.
  • the propulsion system may be affixed to the sealed container by the walls.
  • the walls and motor may form an H structure within the sealed container.
  • the walls may channel or guide the intake stream and exhaust stream in navigating the interior of the sealed container.
  • a propulsion system generating thrust may be placed within the airtight container.
  • the propulsion system may comprise an electrical motor connected to a propeller blade.
  • the propulsion system may be activated.
  • the airtight container will then travel across or through a medium.
  • the container may travel through a body of space, air, or water.
  • the present invention may travel across a surface of water.
  • the atmosphere enclosed in the sealed container may be dense atmosphere relative to Earth's atmosphere.
  • the dense atmosphere may be composed of a noble gas such as Argon.
  • the atmosphere may be oxygen rich or an oxygen-nitrogen mixture.
  • the atmosphere may be similar to Earth's atmosphere and be a breathable atmosphere.
  • the sealed container may house passengers and/or cargo.
  • a portion of the container may be dedicated for passengers and/or cargo. Said portion may be protected from the exhaust stream.
  • the sealed container may be sufficiently large enough to contain and house passengers or at least one person for a sufficient period of time in a comfortable fashion.
  • the sealed container may provide a sleeping area, a bathroom, and/or a dining area as would be appropriate for an extended period of travel ranging from hours to days or weeks.
  • the sealed container may provide enough space and adequate facilities to sustain and support at least one passenger for said periods of time.
  • the solar charging unit may be electronically wired to a motor of the propulsion system and power the motor.
  • the solar charging unit may be positioned on an outside of the sealed container or on an inside of the sealed container.
  • the sealed container or portions thereof are transparent. The transparency of the container may enable charging of the solar charging unit as the sealed container may be configured to provide or expose the solar charging unit to solar energy emanating from an outside of the sealed container.
  • the propulsion system may be mechanical/caloric.
  • a shape of the container is not particularly limited.
  • the container may be any shape suitable for housing a propulsion system such as a sphere, cylinder, or heart shape.
  • the propulsion system may be at an apex of the heart shape whereas return corridors or thrust corridors are formed by segments of the heart.
  • the thrust corridor comprises gasses being release from the propulsion system or expanding.
  • the return corridor comprises gasses being compressed or collected by the propulsion system.
  • the thrust corridor may be adjacent to the exhaust of the propulsion system.
  • the return corridor may be adjacent to the intake of the propulsion system.
  • a relative change in pressure or pressure differential, resulting from the propulsion system, an expansion/compression of gasses thereby, and/or the intake and exhaust stream may result in a movement of the vehicle system and the sealed container relative to its surroundings.
  • the pressure differential inside of the sealed container may be sufficient enough to cause the vehicle movement.
  • the movement may be in a direction opposite of the exhaust stream and controller by a steering mechanism or rudder.
  • gasses within the thrust corridor may expand without hinderance or resistance from a shape of the corridor.
  • the thrust corridor may be of a sufficient length to not impede a flow of the movement of the gases in the thrust corridor.
  • Nozzles may be incorporated to modify gas flow.
  • the return corridor also referred to as an atmosphere return corridor, may be a distance from the propulsion system.
  • the return corridor may direct gas within the sealed container to the propulsion system for compression. This process may repeat as long as a sufficient fuel source is present.
  • FIGURE shows a schematic view of a vehicle system 10 enclosed by a container 18 according to an embodiment of the present invention.
  • An electric motor 12 drives a turbine engine 11 .
  • the turbine engine 11 forces an exhaust stream 20 down a thrust corridor 14 to a first end 30 of the container 18 .
  • the exhaust stream 20 may be a fluid such as air.
  • the exhaust stream 20 is guided by a wall of the container 18 to a return corridor 16 where it is further guided to a second end 32 of the container 18 .
  • the exhaust stream 20 re-enters the turbine engine 11 where it is once again forced down the thrust corridor 14 .

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)

Abstract

A vehicle including a sealed container, a propulsion system with an intake and an exhaust affixed to an interior of the sealed container, an exhaust stream emitted from the exhaust, a thrust corridor within the sealed configured to channel the exhaust stream, and a return corridor configured to channel an intake stream into the intake of the propulsion system wherein the exhaust stream transforms into the intake stream after traveling a sufficient distance within the sealed container and the exhaust stream and intake stream generate a pressure differential within the sealed container wherein the pressure differential is sufficient to result in a movement of the vehicle relative to the vehicle's surroundings.

Description

    CROSS-REFERENCE TO RELATED APPLICATION
  • This application claims the benefit of priority of U.S. provisional application No. 63/266,118, filed Dec. 29, 2021, the contents of which are herein incorporated by reference.
  • BACKGROUND OF THE INVENTION
  • The present invention relates to a vehicle with a propulsion system and, more particularly, to a vehicle with a propulsion system enclosed in a sealed container.
  • Current propulsion systems are expensive due to fuel consumption, as fuel in the system is not recyclable. Presently, a propeller or jet turbine type propulsion system generates a force, such as thrust. The thrust is formed as an air stream or matter is ejected or propelled away from a vehicle. The air stream or matter ejected is not recycled and is lost to the vehicle's system.
  • Traveling between solar bodies such as in interplanetary travel, would be more efficient if resources were not being ejected into space. Current propulsion systems used in space rely on an ejection of matter to propel a spacecraft. Once ejected, the matter is lost in space. If this matter could be recycled, it would make interplanetary travel more efficient. However, no systems for recycling matter or an air stream with a propulsion system currently exist. Enclosing the propulsion system within a sealed, even airtight, container may enable propulsion in space or underwater.
  • As can be seen, there is a need for a propulsion system in an enclosed container that enables recycling of ejected matter while propelling a vehicle.
  • SUMMARY OF THE INVENTION
  • In one aspect of the present invention, a vehicle comprises a sealed container, a propulsion system with an intake and an exhaust affixed to an interior of the sealed container, an exhaust stream emitted from the exhaust of the propulsion system, a thrust corridor within the sealed container, positioned adjacent to the exhaust of the propulsion system configured to channel the exhaust stream, and a return corridor within the sealed container, positioned adjacent to the intake of the propulsion system configured to channel an intake stream into the intake of the propulsion system wherein the exhaust stream transforms into the intake stream after traveling a sufficient distance within the sealed container wherein the exhaust stream and intake stream generate a pressure differential within the sealed container wherein the pressure differential is sufficient to result in a movement of the vehicle relative to the vehicle's surroundings.
  • These and other features, aspects and advantages of the present invention will become better understood with reference to the following drawings, description, and claims.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • The FIGURE is a schematic view of a vehicle in a sealed container according to an embodiment of the present invention.
  • DETAILED DESCRIPTION OF THE INVENTION
  • The following detailed description is of the best currently contemplated modes of carrying out exemplary embodiments of the invention. The description is not to be taken in a limiting sense but is made merely for the purpose of illustrating the general principles of the invention, since the scope of the invention is best defined by the appended claims.
  • A general overview of the various features of the invention will be provided, with a detailed description following. Broadly, an embodiment of the present invention provides a propulsion system enclosed in a sealed container.
  • The propulsion of the present invention may be a propeller or a turbine. A main or primary fuel source for the system may be electricity so as to remove the need for costly and expendable chemical reactions and/or fossil fuels. Said electricity may be generated by solar power. An electric turbine, an electric propellor, and/or an electric motor may enable thrust production via electrical means instead of chemical fuels.
  • The propulsion system is enclosed in and affixed to an interior of a sealed or airtight container. The sealed container may form, enclose, and/or encompass a vehicle system.
  • A steering mechanism may be equipped to the container to direct or steer the container. Such steering mechanism may be a rudder.
  • In some embodiments of the present invention, the atmosphere within the container forms streams including at least one exhaust stream and at least one return stream. The return stream may also be referred to as an intake stream. The exhaust stream may be ejected from a rear end of the propulsion system or an exhaust end. The exhaust stream may be redirected or deflected by a wall or a chamber to a front end of the propulsion system. The walls may form a thrust corridor, for the exhaust stream to exit to propulsion system, and a return corridor, for the exhaust stream to return an entrance of the propulsion system. By traveling through the return corridor, the exhaust stream may then re-enter the propulsion system at an intake section. The sealed container of the present invention enables the exhaust stream to be recycled and reused indefinitely without the exhaust stream escaping the sealed container.
  • The propulsion system may include an intake and an exhaust. The exhaust may emit or release an exhaust stream. The exhaust stream may be an expanded or expanding gas. After traveling a sufficient distance, the exhaust stream may circulate, circle, navigate, or travel the sealed container and transform to the intake stream. The thrust corridor may simultaneously transform to the return corridor when the exhaust stream transforms into the intake stream. This may be when the expanding gas is no longer expanding or when a pressure differential caused by the exhaust stream changes sufficiently.
  • The intake stream may re-enter the propulsion system. In some embodiments, no portion of the intake stream or the exhaust stream exits the sealed container or the vehicle system.
  • The walls may be affixed to an interior of the sealed container. The propulsion system including the motor may be affixed to the sealed container. The propulsion system may be affixed to the sealed container by the walls. The walls and motor may form an H structure within the sealed container.
  • The walls may channel or guide the intake stream and exhaust stream in navigating the interior of the sealed container.
  • A propulsion system generating thrust may be placed within the airtight container. For example, the propulsion system may comprise an electrical motor connected to a propeller blade. The propulsion system may be activated. The airtight container will then travel across or through a medium. The container may travel through a body of space, air, or water. Alternatively, the present invention may travel across a surface of water.
  • In some embodiments of the present invention, the atmosphere enclosed in the sealed container may be dense atmosphere relative to Earth's atmosphere. The dense atmosphere may be composed of a noble gas such as Argon. The atmosphere may be oxygen rich or an oxygen-nitrogen mixture. The atmosphere may be similar to Earth's atmosphere and be a breathable atmosphere.
  • The sealed container may house passengers and/or cargo. A portion of the container may be dedicated for passengers and/or cargo. Said portion may be protected from the exhaust stream.
  • The sealed container may be sufficiently large enough to contain and house passengers or at least one person for a sufficient period of time in a comfortable fashion. For example, the sealed container may provide a sleeping area, a bathroom, and/or a dining area as would be appropriate for an extended period of travel ranging from hours to days or weeks. The sealed container may provide enough space and adequate facilities to sustain and support at least one passenger for said periods of time.
  • In some embodiments, the solar charging unit may be electronically wired to a motor of the propulsion system and power the motor. The solar charging unit may be positioned on an outside of the sealed container or on an inside of the sealed container. In some embodiments of the present invention, the sealed container or portions thereof are transparent. The transparency of the container may enable charging of the solar charging unit as the sealed container may be configured to provide or expose the solar charging unit to solar energy emanating from an outside of the sealed container.
  • In some embodiments, the propulsion system may be mechanical/caloric.
  • A shape of the container is not particularly limited. The container may be any shape suitable for housing a propulsion system such as a sphere, cylinder, or heart shape. In some embodiments, the propulsion system may be at an apex of the heart shape whereas return corridors or thrust corridors are formed by segments of the heart.
  • In some embodiments of the present invention, the thrust corridor comprises gasses being release from the propulsion system or expanding. The return corridor comprises gasses being compressed or collected by the propulsion system. The thrust corridor may be adjacent to the exhaust of the propulsion system. The return corridor may be adjacent to the intake of the propulsion system.
  • A relative change in pressure or pressure differential, resulting from the propulsion system, an expansion/compression of gasses thereby, and/or the intake and exhaust stream may result in a movement of the vehicle system and the sealed container relative to its surroundings. The pressure differential inside of the sealed container may be sufficient enough to cause the vehicle movement. The movement may be in a direction opposite of the exhaust stream and controller by a steering mechanism or rudder.
  • In some embodiments, gasses within the thrust corridor may expand without hinderance or resistance from a shape of the corridor. The thrust corridor may be of a sufficient length to not impede a flow of the movement of the gases in the thrust corridor. Nozzles may be incorporated to modify gas flow.
  • The return corridor, also referred to as an atmosphere return corridor, may be a distance from the propulsion system. The return corridor may direct gas within the sealed container to the propulsion system for compression. This process may repeat as long as a sufficient fuel source is present.
  • Referring now to the FIGURE, the FIGURE shows a schematic view of a vehicle system 10 enclosed by a container 18 according to an embodiment of the present invention. An electric motor 12 drives a turbine engine 11. The turbine engine 11 forces an exhaust stream 20 down a thrust corridor 14 to a first end 30 of the container 18. The exhaust stream 20 may be a fluid such as air. The exhaust stream 20 is guided by a wall of the container 18 to a return corridor 16 where it is further guided to a second end 32 of the container 18. The exhaust stream 20 re-enters the turbine engine 11 where it is once again forced down the thrust corridor 14.
  • It should be understood, of course, that the foregoing relates to exemplary embodiments of the invention and that modifications may be made without departing from the spirit and scope of the invention as set forth in the following claims

Claims (11)

What is claimed is:
1. A vehicle comprising:
a sealed container;
a propulsion system with an intake and an exhaust affixed to an interior of the sealed container;
an exhaust stream emitted from the exhaust of the propulsion system;
a thrust corridor within the sealed container, positioned adjacent to the exhaust of the propulsion system configured to channel the exhaust stream; and
a return corridor within the sealed container, positioned adjacent to the intake of the propulsion system configured to channel an intake stream into the intake of the propulsion system;
wherein the exhaust stream transforms into the intake stream after traveling a sufficient distance within the sealed container;
wherein the exhaust stream and intake stream generate a pressure differential within the sealed container wherein the pressure differential is sufficient to result in a movement of the vehicle relative to the vehicle's surroundings.
2. The vehicle of claim 1, wherein the propulsion system comprises an electric motor and an electric turbine.
3. The vehicle of claim 2, wherein the electric motor is powered by a solar charging unit.
4. The vehicle of claim 3, wherein the solar charging unit is positioned on an outside of the sealed container and electronically wired to the electric motor.
5. The vehicle of claim 3, wherein the solar charging unit is positioned on an inside of the sealed container and electronically wired to the electric motor wherein at least a portion of the sealed container is transparent and configured to provide the solar charging unit with solar power emanating from an outside of the sealed container.
6. The vehicle of claim 1, wherein the propulsion system comprises an electric motor and an electric propeller.
7. The vehicle of claim 6, wherein the electric motor is powered by a solar charging unit.
8. The vehicle of claim 7, wherein the solar charging unit is positioned on an outside of the sealed container and electronically wired to the electric motor.
9. The vehicle of claim 7, wherein the solar charging unit is positioned on an inside of the sealed container and electronically wired to the electric motor wherein at least a portion of the sealed container is transparent and configured to provide the solar charging unit with solar power emanating from an outside of the sealed container.
10. The vehicle of claim 1, wherein the sealed container contains a breathable atmosphere.
11. The vehicle of claim 1, wherein the sealed container is sufficiently large to house and sustain at least one person for an extended period of time.
US17/822,471 2021-12-29 2022-08-26 Vehicle with a propulsion system enclosed in a sealed container Abandoned US20230202685A1 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
US17/822,471 US20230202685A1 (en) 2021-12-29 2022-08-26 Vehicle with a propulsion system enclosed in a sealed container
PCT/US2022/042844 WO2023129216A1 (en) 2021-12-29 2022-09-08 Vehicle with a propulsion system enclosed in a sealed container
US18/406,367 US20240140620A1 (en) 2021-12-29 2024-01-08 Vehicle with a propulsion system enclosed in a sealed container

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US202163266118P 2021-12-29 2021-12-29
US17/822,471 US20230202685A1 (en) 2021-12-29 2022-08-26 Vehicle with a propulsion system enclosed in a sealed container

Related Child Applications (1)

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US18/406,367 Continuation US20240140620A1 (en) 2021-12-29 2024-01-08 Vehicle with a propulsion system enclosed in a sealed container

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US20230202685A1 true US20230202685A1 (en) 2023-06-29

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US18/406,367 Pending US20240140620A1 (en) 2021-12-29 2024-01-08 Vehicle with a propulsion system enclosed in a sealed container

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Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20060005528A1 (en) * 2004-06-28 2006-01-12 Joseph Brady Propulsion device with enclosed plenum
US7303166B2 (en) * 2003-11-04 2007-12-04 Daniel Geery Highly maneuverable powered airship
US20140158817A1 (en) * 2011-10-31 2014-06-12 Tp Aerospace, Inc. Rigid airship utilizing a rigid frame formed by high pressure inflated tubes
US20190148027A1 (en) * 2017-11-10 2019-05-16 Nugen, Llc Integrated system for converting nuclear energy into electrical, mechanical, and thermal energy and methods for using the same

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7047722B2 (en) * 2002-10-02 2006-05-23 Claudio Filippone Small scale hybrid engine (SSHE) utilizing fossil fuels
US20050210862A1 (en) * 2004-03-25 2005-09-29 Paterro Von Friedrich C Quantum jet turbine propulsion system
US8333626B2 (en) * 2009-03-26 2012-12-18 Suzuki Motor Corporation Hybrid outboard motor
WO2012091533A2 (en) * 2010-12-27 2012-07-05 Alibi Akhmejanov The device to generate lift force (options)

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7303166B2 (en) * 2003-11-04 2007-12-04 Daniel Geery Highly maneuverable powered airship
US20060005528A1 (en) * 2004-06-28 2006-01-12 Joseph Brady Propulsion device with enclosed plenum
US20140158817A1 (en) * 2011-10-31 2014-06-12 Tp Aerospace, Inc. Rigid airship utilizing a rigid frame formed by high pressure inflated tubes
US20190148027A1 (en) * 2017-11-10 2019-05-16 Nugen, Llc Integrated system for converting nuclear energy into electrical, mechanical, and thermal energy and methods for using the same

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
"The Jet Engine: A Historical Introduction, Stanford University" (Year: 2004) *
"Understanding Airplane Turbofan Engine Operation Helps Flight Crews Respond to Malfunctions, Flight Safety Digest, pp.1-2" (Year: 2001) *

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US20240140620A1 (en) 2024-05-02

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