# US 2014/0150863 A1 · Directionally Controlled Elastically Deployable Roll-Out Array

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- Number: US 2014/0150863 A1
- Document ID: US20140150863A1
- Status: Published application
- Kind: A1
- Application number: 14/173,252
- Filed: 2014-02-05
- Published: 2014-06-05
- Earliest claimed: 2010-01-21
- Assignees: Deployable Space Systems, Inc.
- Applicants: Deployable Space Systems, Inc.
- Inventors: Brian R. Spence; Stephen F. White
- Web page: https://patentgrep.com/patent/US20140150863A1

## CPC

- B64G 1/443: {Photovoltaic cell arrays}
- B64G 1/2225: {Rolling or unfurling (B64G1/2227 takes precedence)}
- B64G 1/2229: {characterised by the deployment actuating mechanism (inflating B64G1/2227)}
- B64G 1/2228: {characterised by the hold-down or release mechanisms}
- Y02E 10/50: Photovoltaic [PV] energy
- Y10T 428/1362: Textile, fabric, cloth, or pile containing [e.g., web, net, woven, knitted, mesh, nonwoven, matted, etc.]
- B64G: COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- Y02E: REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y10T: TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION

## Abstract

A directionally-controlled roll-out elastically deployable solar array structure is disclosed. The structure includes one or more longitudinal elastic roll out booms that may be closed section or open section to allow for efficient rolled packaging onto a lateral mandrel. A flexible photovoltaic blanket is attached to a tip structure and to a lateral base support structure, but remains uncoupled from the longitudinal booms. The solar array system may be stowed simultaneously into a rolled package comprised of the roll out booms and the flexible planar blanket together, or onto independent rolls. Alternatively, the system may be stowed by rolling the booms, and accordion Z-folding the hinged flexible photovoltaic blanket into a flat stack. Structural deployment is motivated by the elastic strain energy of the roll out booms, and several methods of deployment direction control are provided to ensure a known, controlled, and unidirectional deployment path of the elastically unrolling booms.

## Claims

### Claim 1

A deployable structure comprising:
an elastic roll out boom comprising a thin-wall tubular, elongated structure, of a fiber-composite layup material, the elastic roll out boom having a plurality of configurations ranging from a stowage configuration for transport to a deployed configuration in which the elastic roll out boom is fully extended, the elastic roll out boom having a first end, a second end opposite said first end, wherein a longitudinal axis is defined by the first end and the second end when the elastic roll out boom is in the deployed configuration, wherein internal strain energy of the fiber-composite layup material is exclusively sufficient to cause the roll out boom to extend from the stowage configuration to the deployed configuration without passive or active heating of the fiber-composite layup material.

### Claim 2 (depends on 1)

The deployable structure of claim 1 wherein the fiber-composite layup material is primarily unidirectional.

### Claim 3 (depends on 1)

The deployable structure of claim 1 further comprising a mandrel, the mandrel being a substantially cylindrical structure having a longitudinal axis upon which the mandrel is able to rotate, wherein the longitudinal axis of the elastic roll out boom is perpendicular to the longitudinal axis of the mandrel, and the elastic roll out boom can be flattened in cross-section and rolled upon the mandrel into the stowage configuration.

### Claim 4 (depends on 3)

The deployable structure of claim 3 further comprising a yoke support structure, the yoke support structure providing a fixed base for deployment of the elastic roll out boom, wherein the first end of the elastic roll out boom is attached to the mandrel and the second end is attached to the yoke support structure.

### Claim 5 (depends on 4)

The deployable structure of claim 4 further comprising a deployment control device which controls the deployment of the elastic roll out boom as it extends into the deployed configuration.

### Claim 6 (depends on 5)

The deployable structure of claim 5 wherein the deployment control device comprises (i) a stabilizer arm and a boom control roller, wherein the stabilizer arm connects the boom control roller about the longitudinal axis of the mandrel, and (ii) a rotary damping mechanism, wherein the rotary damping mechanism is connected in-line with the longitudinal axis of the mandrel, wherein the rotary damping mechanism controls the rate of mandrel rotation during deployment of the elastic roll out boom as it extends into the deployed configuration.

### Claim 7 (depends on 5)

The deployable structure of claim 5 wherein the deployment control device comprises (i) a stabilizer bar, a stabilizer arm, and a boom control roller, wherein the stabilizer arm connects the boom control roller to the longitudinal axis of the mandrel, and (ii) a deployment lanyard and a rotating pulley, wherein the deployment lanyard has a first end and a second end opposite said first end, wherein the first end of the deployment lanyard is attached to the stabilizer bar, wherein the second end of the deployment lanyard is attached to the rotating pulley, and wherein the rotating pulley is attached to the yoke support structure such that unidirectional boom deployment is effected.

### Claim 8 (depends on 4)

The deployable structure of claim 4, further comprising a flexible photovoltaic blanket, wherein the flexible photovoltaic blanket is substantially planar having a first end and a second end, wherein the flexible photovoltaic blanket is attached at the first end to the mandrel, and at the second end to the yoke support structure.

### Claim 9 (depends on 8)

The deployable structure of claim 8, wherein the elastic roll out boom and the flexible photovoltaic blanket may be rolled onto the mandrel simultaneously into the stowage configuration.

### Claim 10

A deployable structure comprising:
a. an elastic roll out boom comprising a thin-wall tubular, elongated structure, of a fiber-composite layup material, the elastic roll out boom having a plurality of configurations ranging from a stowage configuration for transport to a deployed configuration in which the elastic roll out boom is fully extended, the elastic roll out boom having a first end, a second end opposite said first end, wherein a longitudinal axis is defined by the first end and the second end when the elastic roll out boom is in the deployed configuration, wherein internal strain energy of the fiber-composite layup material is exclusively sufficient to cause the roll out boom to extend from the stowage configuration to the deployed configuration without passive or active heating of the fiber-composite layup material;
b. a mandrel, the mandrel being a substantially cylindrical structure having a longitudinal axis upon which the mandrel is able to rotate, wherein the longitudinal axis of the elastic roll out boom is perpendicular to the longitudinal axis of the mandrel, and the elastic roll out boom can be flattened in cross-section and rolled upon the mandrel into the stowage configuration;
c. a yoke support structure, the yoke support structure providing a fixed base for deployment of the elastic roll out boom, wherein the first end of the elastic roll out boom is attached to the mandrel and the second end is attached to the yoke support structure; and
d. a flexible photovoltaic blanket, wherein the flexible photovoltaic blanket is substantially planar having a first end and a second end, wherein the flexible photovoltaic blanket is connected at the first end to the mandrel, and at the second end to the yoke support structure, wherein the flexible photovoltaic blanket deploys simultaneously with the elastic roll out boom from the stowage configuration to the deployed configuration.

### Claim 11 (depends on 10)

The deployable structure of claim 10 wherein the flexible photovoltaic blanket is not attached to the elastic roll out boom.

### Claim 12 (depends on 10)

The deployable structure of claim 10 wherein the fiber-composite layup material is primarily unidirectional.

### Claim 13 (depends on 10)

The deployable structure of claim 10 further comprising a deployment control device which controls the deployment of the elastic roll out boom as it extends into the deployed configuration.

### Claim 14 (depends on 13)

The deployable structure of claim 13 wherein the deployment control device comprises: (i) a stabilizer arm and a boom control roller, wherein the stabilizer arm connects the boom control roller about the longitudinal axis of the mandrel, and (ii) a rotary damping mechanism, wherein the rotary damping mechanism is connected in-line with the longitudinal axis of the mandrel, wherein the rotary damping mechanism controls the rate of mandrel rotation during deployment of the elastic roll out boom as it extends into the deployed configuration.

### Claim 15 (depends on 13)

The deployable structure of claim 13 wherein the deployment control device comprises: (i) a stabilizer bar, a stabilizer arm and a boom control roller, wherein the stabilizer arm connects the boom control roller to the longitudinal axis of the mandrel, and (ii) a deployment lanyard and a rotating pulley, wherein the deployment lanyard has a first end and a second end opposite said first end, wherein the first end of the deployment lanyard is attached to the stabilizer bar and the second end of the deployment lanyard is attached to the rotating pulley, and the rotating pulley is attached to the yoke support structure.

### Claim 16 (depends on 13)

The deployable structure of claim 13 wherein the flexible photovoltaic blanket has a stowage configuration as a stowed roll, wherein the deployment control device comprises (i) a stabilizer bar, a stabilizer arm and a boom control roller, wherein the stabilizer arm connects the boom control roller to the longitudinal axis of the mandrel, (ii) a frictionless tensioned containment strap, and a strap cross bar, wherein the frictionless tensioned containment strap has a first end and a second end, the first end connected to the stabilizer bar, the second end being connected to the strap cross bar, wherein the frictionless tensioned containment strap surrounds the stowed roll, (iii) wherein the frictionless tensioned containment strap controls the stowed roll diameter during deployment to the deployed configuration.

### Claim 17 (depends on 10)

The elastic deployable structure of claim 10, further comprising a lateral blanket support structure, a base preload platen, and a tip preload platen, wherein the lateral blanket support structure is attached to the mandrel wherein the flexible photovoltaic blanket is attached at the first end to the lateral blanket support structure, and at the second end to the yoke support structure, wherein the flexible photovoltaic blanket is stowable in the stowage configuration between the tip preload platen and the base preload platen as a z-fold flat package.

### Claim 18 (depends on 17)

The elastic deployable structure of claim 17, further comprising a lateral blanket mandrel system comprising a system of lanyards and pulleys, and an auxiliary electric motor, wherein the flexible photovoltaic blanket is attached at the first end to the lateral blanket support structure and at the second end to the yoke support structure, wherein internal strain energy of the fiber-composite layup material is exclusively sufficient to cause the roll out boom to extend from the stowage configuration to the deployed configuration and the lateral blanket mandrel system powers extension of the flexible photovoltaic blanket to the deployed configuration.
