Airship with internal propulsion system
View Patent ↗An airship is presented having a plurality of resilient gas bags and gas containers, a straight fuselage tubular hull, with an inner air passageway and propulsion system located therein, and, connecting air inlet, and outlet funnels fore, and aft, with air deflector cones axially positioned therein. The ship also contains propulsion, reverse, and directional rocket thrusters, in addition to typical airship components.
1. An airship comprising:
a linear fuselage containing a first end and a second end, and an interior;
a funnel-shaped inlet formed at said first end, and containing an inner wall defining a progressively smaller diameter as the inlet extends within said fuselage from said first end to said interior of said fuselage;
a funnel-shaped outlet formed at said second end, and containing a second inner wall defining a progressively smaller diameter as the outlet extends within said fuselage from said second end to said interior; and
an inner air passageway contained within said fuselage and connecting said inlet with said outlet, wherein said inner air passageway provides fluid communication between said inlet and said outlet;
a first conical air deflector fixed within and congruent to said funnel-shaped inlet, thereby providing an annular air passageway between said funnel-shaped inlet and said first conical air deflector;
a second conical air deflector fixed within said funnel-shaped inlet and having a second widest portion positioned against a corresponding first widest portion of said first conical air deflector.
2. The airship of claim 1 further comprising a propulsion system located in said inner air passageway, wherein said propulsion system draws air into the funnel-shaped inlet and pushes air out of the funnel-shaped outlet.
3. The airship of claim 1 further comprising a first horizontal control wing fixed to said funnel-shaped inlet.
4. The airship of claim 3 further comprising a second horizontal control wing fixed to said funnel-shaped outlet.
5. The airship of claim 1 further comprising a first vertical control wing fixed to said funnel-shaped inlet.
6. The airship of claim 5 further comprising a second vertical control wing fixed to said funnel-shaped outlet.
7. The airship of claim 1 further comprising a third conical air deflector fixed within and congruent to said funnel-shaped outlet, thereby providing a second annular air passageway between said funnel-shaped outlet and said third conical air deflector.
8. The airship of claim 1 further comprising a fourth conical air deflector fixed within said funnel-shaped outlet and having a fourth widest portion positioned against a corresponding third widest portion of said third conical air deflector.
9. An airship comprising:
a tubular fuselage containing a first end and a second end, and an interior;
a funnel-shaped inlet formed at said first end, and containing an inner wall defining a progressively smaller diameter as the inlet extends within said fuselage from said first end to said interior;
a funnel-shaped outlet formed at said second end, and containing a second inner wall defining a progressively smaller diameter as the outlet extends within said fuselage from said second end to said interior;
an inner air passageway connecting said inlet with said outlet, wherein said inner air passageway provides fluid communication between said inlet and said outlet; and
a propulsion system located in said inner air passageway, wherein said propulsion system draws air into the funnel-shaped inlet and pushes air out of the funnel-shaped outlet;
a first conical air deflector fixed within and congruent to said funnel-shaped inlet, thereby providing an annular air passageway between said funnel-shaped inlet and said first conical air deflector;
a second conical air deflector fixed within said funnel-shaped inlet and having a second widest portion positioned against a corresponding first widest portion of said first conical air deflector;
a third conical air deflector fixed within and congruent to said funnel-shaped outlet, thereby providing a second annular air passageway between said funnel-shaped outlet and said third conical air deflector; and
a fourth conical air deflector fixed within said funnel-shaped outlet and having a fourth widest portion positioned against a corresponding third widest portion of said third conical air deflector.
10. The airship of claim 9 further comprising:
a first horizontal control wing fixed to said funnel-shaped inlet;
a second horizontal control wing fixed to said funnel-shaped outlet;
a first vertical control wing fixed to said funnel-shaped inlet; and
a second vertical control wing fixed to said funnel-shaped outlet.
11. An airship comprising:
a linear and fuselage containing a first end and a second end, and an interior;
a funnel-shaped inlet formed at said first end, and containing an inner wall defining a progressively smaller diameter as the inlet extends within said fuselage from said first end to said interior of said fuselage;
a funnel-shaped outlet formed at said second end, and containing a second inner wall defining a progressively smaller diameter as the outlet extends within said fuselage from said second end to said interior;
an inner air passageway connecting said inlet with said outlet, wherein said inner air passageway provides fluid communication between said inlet and said outlet;
a propulsion system located in said inner air passageway, wherein said propulsion system draws air into the funnel-shaped inlet and pushes air out of the funnel-shaped outlet;
a first conical air deflector fixed within said funnel-shaped inlet;
a second conical air deflector fixed within said funnel shaped outlet;
a first horizontal control wing fixed to said funnel-shaped inlet;
a second horizontal control wing fixed to said funnel-shaped outlet;
a first vertical control wing fixed to said funnel-shaped inlet;
a second vertical control wing fixed to said funnel-shaped outlet.