Long range hybrid electric airplane

• US 20080184906A1
• Filed: 02/07/2007
• Published: 08/07/2008
• Est. Priority Date: 02/07/2007
• Status: Abandoned Application

• Current Assignee: Joseph B. Kejha
• Original Assignee: Joseph B. Kejha
• Inventors: Kejha, Joseph B.
• Application Number:
  US11/703,362
• Publication Number:
  US 20080184906A1
• Time in Patent Office: Days
• US Class Current: 102/374
• CPC Class Codes: B64C 39/024 of the remote controlled vehicle type, i.e. RPV
• CPC Class Codes: B64D 2027/026 comprising different types of power plants, e.g. combination of an electric motor and a gas-turbines
• CPC Class Codes: B64D 27/02 Aircraft characterised by the type or position of power plants fuselages specially adapted for mounting power plants B64C1/16; wings specially adapted for power plants B64C3/32
• CPC Class Codes: B64D 27/026 comprising different types of power plants, e.g. combination of a piston engine and a gas-turbine Hybrid electric aircraft B64D27/33
• CPC Class Codes: B64D 27/24 using steam or spring force jet aircraft B64D27/16
• CPC Class Codes: B64U 10/25 Fixed-wing aircraft VTOL aircraft B64U10/20
• CPC Class Codes: B64U 50/00 Propulsion; Power supply
• CPC Class Codes: B64U 50/11 using internal combustion piston engines
• CPC Class Codes: B64U 50/13 using external fans or propellers
• CPC Class Codes: B64U 50/19 using electrically powered motors
• CPC Class Codes: B64U 50/34 In-flight charging photovoltaics B64U50/31
• CPC Class Codes: B64U 60/50 with landing legs
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft
• CPC Class Codes: Y02T 90/40 Application of hydrogen technology to transportation, e.g. using fuel cells

Abstract

An advanced internal combustion-electric hybrid airplane, having at least double the flight range and flight duration than a conventional equivalent airplane, while using the same amount of any desirable fuel. This is achieved by using 2-3× smaller and ultra-lightweight engine for cruising, and ultra-lightweight electric motor powered by lithium batteries during take-off and climbing. The electric motor becomes a generator during cruising and descent, recharging said batteries. The airplane has also temporary silent electric stealth capability and added safety by the electric back-up power. Due to its high efficiency, the operational cost is substantially reduced. Additional features include highly advanced, minimum drag and weight airframe.

Claims

1. Parallel internal combustion-electric hybrid propulsion system for airplanes, comprising:

a smaller internal combustion engine than an internal combustion engine of an equivalent internal combustion-only airplane;

an electric motor/generator in one unit;

an electric control unit for controlling said motor;

an electric clutch between said engine and said motor/generator;

at least one battery electrically connected to said motor/generator through said control unit;

a propeller which can be driven by said engine, or by said electric motor, or by both, selectively through said clutch;

and a fuel storage.

3. Internal combustion-electric hybrid airplane with a puller propeller, which airplane comprises:

an airframe with flight controls;

at least one parallel hybrid electric propulsion system as described in claim 1;

and a payload.

4. Internal combustion-electric hybrid airplane with a push propeller, which airplane comprises:

an airframe with flight controls;

at least one parallel hybrid electric propulsion system as described in claim 1;

and a payload.

7. Hybrid electric airplane as described in claim 4, in which said airplane is a bi-plane having a fuselage, first wing and second wing and a vertical tail fin, said wings are connected together with braces, and in which said engine, said clutch and said electric motor/generator with said pusher propeller are mounted on top of said vertical tail fin, together with said second wing, and said second wing includes horizontal control surfaces, said surfaces having a symmetric airfoil profile.

10. Hybrid electric airplane as described in claims 3, or 6, in which said engine is a jet engine, and in which said propeller is replaced with a ducted fan.

11. Hybrid electric airplane as descried in claim 3, or 4, or 5, or 6 in which said airframe includes at least one wing and said batteries are mounted in said wing(s).

12. Hybrid electric airplane as described in claims 3, or 4, or 5, or 6, which is a cruise missile, and in which said engine is a jet engine and in which said propeller is replaced with a ducted fan.

13. Hybrid electric propulsion system for airplanes, as described in claims 1, or 2, in which said engine includes magnesium alloy crankcase, carbon/carbon composite cylinder block and head with ceramic lining(s), titanium hollow crankshaft, and ceramic bearings;

and said electric motor and said generator include magnesium alloy casings, aluminum hollow shaft, flat aluminum wires, and ceramic bearings; and

said battery is a lithium based battery.

14. Hybrid electric propulsion system for airplanes as described in claims 1, or 2, in which said fuel is hydrogen.

2. Series internal combustion-electric hybrid propulsion system for airplanes, comprising:

a smaller internal combustion engine than an internal combustion engine of an equivalent internal combustion-only airplane, and said smaller engine drives an electric generator;

an electric motor which drives a propeller;

a first electric control unit for controlling said motor;

at least one battery electrically connected to said motor through said first control unit;

a second electric control unit for controlling said motor, electrically connected to said motor and to said generator;

and a fuel storage.

5. Internal combustion-electric hybrid airplane with a puller propeller, which airplane comprises;

an airframe with flight controls;

at least one series hybrid electric propulsion system as described in claim 2;

and a payload.

6. Internal combustion-electric hybrid airplane with a pusher propeller, which airplane comprises:

an airframe with flight controls;

at least one series hybrid electric propulsion system as described in claim 2;

and a payload.

8. Hybrid electric airplane as described in claim 6, in which said airplane is a bi-plane having a fuselage, first wing and second wing, and a vertical tail fin, said wings are connected together with braces, and in which said electric motor with said pusher propeller are mounted on top of said vertical tail fin, together with said second wing, and said engine with said generator are mounted in said fuselage, and said second wing includes horizontal control surfaces, said surfaces having a symmetric airfoil profile.

9. Hybrid electric airplane as described in claim 6, in which said airplane is a diamond wing tandem bi-plane having a fuselage with a tail end, front wing and rear wing, said wings are connected together at their tip ends, and in which said electric motor with said pusher propeller are mounted at said fuselage tail'"'"'s end, and said engine with said generator are mounted in said fuselage, and said rear wing includes horizontal control surfaces, said surfaces having a symmetric airfoil profile.