IP Library Granted Patent US 10,843,783
Granted Patent B1
US 10,843,783 · App. 15/843,540 · Granted Nov 24, 2020

Hexakis icosahedron frame-skin vacuum lighter than air vehicle

Inventors: Brian Cranston (Dayton, OH); Anthony Palazotto (Dayton, OH)
Assignee: United States of America as represented by the Secretary of the Air Force
B64B1/08B64B1/16B64B1/62B32B27/08B32B27/32B32B2262/0253B32B2605/18B64B1/12B64B1/20B64B1/30B64D27/24B64D2211/00
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Quick Facts
Patent No.
US 10,843,783
App. No.
15/843,540
Granted
Nov 24, 2020
Kind
B1
Abstract

A vacuum lighter than air vehicle (VLTAV) includes a rigid frame of rods connected together to form a hexakis icosahedron. A membrane skin covers the rigid frame and defines therewith a vessel configured to hold an internal vacuum that allows the vessel to float in the air. The plurality of rods and membrane skin have weights and dimensions that result in a neutral and/or positive buoyancy for the vessel while preventing geometric instability.

Claims (22)

1. A vacuum lighter than air vehicle (VLTAV) comprising:

a plurality of rods connected together to form a hexakis icosahedron rigid frame; and

a membrane skin covering the rigid frame and defining therewith a vessel configured to hold an internal vacuum that allows the vessel to float in the air;

wherein materials of the rods and membrane skin result in the vessel having a weight and buoyant force that results in positive buoyancy while preventing geometric instability;

wherein the rods comprise a carbon fiber composite material having a specific modulus of at least approximately 1.29*108 m2/s2 and a specific yield strength of at least approximately 1.80*106 m2/s2 as a zero-degree layup;

wherein the rods of the rigid frame are connected together at 62 vertices with 180 edges defining 120 about equal size scalene triangle faces;

wherein the membrane skin comprises a fiber matrix reinforced laminate membrane skin material having a specific modulus of at least approximately 9.52*107 m2/s2 and specific yield strength of at least approximately 1.43*106 m2/s2 for a 0.4 mm thick segment; and

wherein the rigid frame comprises joint members connecting the rods at vertices.

2. A vacuum lighter than air vehicle (VLTAV) comprising:

a plurality of rods connected together by a plurality of joint members to form a hexakis icosahedron rigid frame, the rods connected together at 62 vertices with 180 edges defining 120 about equal size scalene triangle faces; and

a laminate membrane skin covering the rigid frame and defining therewith a vessel configured to hold an internal vacuum that allows the vessel to float in the air;

wherein materials of the rods and membrane skin result in a positive buoyancy for the vessel while preventing geometric instability;

wherein the rods comprise a material having a specific modulus of at least approximately 1.29*10 8 m 2 /s 2 and a specific yield strength of at least approximately 1.80*10 6 m 2 /s 2 as a zero-degree layup; and

wherein the laminate membrane comprises a material having a specific modulus of at least approximately 9.52*10 7 m 2 /s 2 and specific yield strength of at least approximately 1.43*10 6 m 2 /s 2 for a 0.4 mm thick segment.

3. A method of making a vacuum lighter than air vehicle (VLTAV), the method comprising:

constructing a rigid frame by connecting a plurality of rods together to form a hexakis icosahedron; and

covering the rigid frame with a membrane skin to define a vessel configured to hold an internal vacuum that allows the vessel to float in the air

selecting weights and dimensions of the rods and membrane skin to result in one of a neutral buoyancy and a positive buoyancy for the vessel while preventing geometric instability;

wherein the rods comprise a material having a specific modulus of at least approximately 1.29*108 m2/s2 and a specific yield strength of at least approximately 1.80*106 m2/s2 as a zero-degree layup;

wherein the rods of the rigid frame are connected together at 62 vertices with 180 edges defining 120 about equal size scalene triangle faces;

wherein the membrane skin comprises a material having a specific modulus of at least approximately 9.52*107 m2/s2 and specific yield strength of at least approximately 1.43*106 m2/s2 for a 0.4 mm thick segment; and

wherein the rigid frame comprises joint members connecting the rods at vertices.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 15, 2017
From: PALAZOTTO, ANTHONY, DR; CRANSTON, BRIAN, DR
To: GOVERNMENT OF THE UNITED STATES, AS REPRESENTED BY THE SECRETARY OF THE AIR FORCE
Reel/Frame 044408/0562 →
Continuity (2)
Provisional Application 62440003 · Dec 29, 2016
Provisional Application 62439994 · Dec 29, 2016
Cited By (2)
US 12,630,282 US 12,654,835