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Mike Legrand Allman, 39Orem, UT

Known as:
Michael L Allman Michael W Allman
Related to:
David R Allman 58 Nathan Canen 46 Hsiaochi Wu 57 Drew Rosa 46 Kim Cody 73

Mike Allman Phones & Addresses

Orem, UT   

Pleasant Grove, UT   

1385 N 950 W, Orem, UT 84057    801-2253243   

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Mike Allman

Location:
United States
Mike Allman Photo 40

Mike Allman

Location:
United States
Mike Allman Photo 41

Mike Allman

Location:
United States
Mike Allman Photo 42

Mike Allman

Location:
United States

Publications & IP owners

Us Patents

Method Of Assembling A Single Piece Co-Cured Structure

US Patent:
7204951, Apr 17, 2007
Filed:
Jul 30, 2002
Appl. No.:
10/208241
Inventors:
Craig B. Simpson - Mapleton UT, US
Mike G. Allman - Spanish Fork UT, US
Steven T. Tuttle - Springville UT, US
Larry J. Ashton - Mapleton UT, US
Assignee:
Rocky Mountain Composites, Inc. - Spanish Fork UT
International Classification:
B29C 44/16
US Classification:
264523, 264573, 264257, 264263, 264313, 264314, 264904, 4253871, 425390
Abstract:
A method for manufacturing a composite structure is disclosed herein. The process uses a frame and selectively pressurizable forms. The forms define the interior members of the composite structure and frames define the exterior surface of the composite structure. Composite material is wrapped around the forms and the forms and composite material are placed in the frame. Selective forms are then pressurized and the composite material is co-cured together. A single piece co-cured fuselage incorporating a plurality of stiffeners is also disclosed in the application. The stiffeners are co-cured to the fuselage and may be in various patterns. The patterns may include an iso-grid pattern, and ortho-grid pattern, and a hoop-grid pattern.

Method Of Assembling A Single Piece Co-Cured Structure

US Patent:
7216832, May 15, 2007
Filed:
Dec 1, 2004
Appl. No.:
11/000721
Inventors:
Craig B. Simpson - Mapleton UT, US
Mike G. Allman - Spanish Fork UT, US
Steven T. Tuttle - Springville UT, US
Larry J. Ashton - Mapleton UT, US
Assignee:
Rocky Mountain Composites, Inc. - Spanish Fork UT
International Classification:
B64C 1/00
US Classification:
244119
Abstract:
A method for manufacturing a composite structure is disclosed herein. The process uses a frame and selectively pressurizable forms. The forms define the interior members of the composite structure and frames define the exterior surface of the composite structure. Composite material is wrapped around the forms and the forms and composite material are placed in the frame. Selective forms are then pressurized and the composite material is co-cured together. A single piece co-cured fuselage incorporating a plurality of stiffeners is also disclosed in the application. The stiffeners are co-cured to the fuselage and may be in various patterns. The patterns may include an iso-grid pattern, and ortho-grid pattern, and a hoop-grid pattern.

Process For Forming A Single Piece Co-Cure Composite Wing

US Patent:
7445744, Nov 4, 2008
Filed:
Dec 3, 2003
Appl. No.:
10/726970
Inventors:
Craig B. Simpson - Mapleton UT, US
Mike Glen Allman - Spanish Fork UT, US
Steven Taylor Tuttle - Springville UT, US
Larry J. Ashton - Mapleton UT, US
Assignee:
Rocky Mountain Composites, Inc. - Spanish Fork UT
International Classification:
B29C 44/16
US Classification:
264523, 264573, 264263, 264313, 264314, 264904, 264325
Abstract:
A single piece co-cured composite wing is disclosed. The wing has a flying surface and structural members. In one embodiment the structural members may be a plurality of spars. The spars may have various shapes to increase the buckling strength. The spars may be wave shaped, such as a sinusoidal shape. The flying surface and the structural members are co-cured in order to form a single piece, integral wing structure. A process for manufacturing a single piece co-cured wing is also disclosed. The process may include laying out composite sheets for the flying surface of the wing. Then, the composite material of the spars is arranged around a plurality of pressurizable forms. Finally, the composite material is cured in a clamshell frame.

Single Piece Co-Cure Composite Wing

US Patent:
7681835, Mar 23, 2010
Filed:
Sep 23, 2005
Appl. No.:
11/234807
Inventors:
Craig B. Simpson - Mapleton UT, US
Larry J. Ashton - Mapleton UT, US
Mike G. Allman - Spanish Fork UT, US
Steven T. Tuttle - Springville UT, US
Assignee:
Rocky Mountain Composites, Inc. - Spanish Fork UT
International Classification:
B64C 1/00
US Classification:
2441233, 24412314, 428111, 428113, 428172
Abstract:
A single piece co-cured composite wing is disclosed. The wing has a flying surface and structural members. In one embodiment the structural members may be a plurality of spars. The spars may have various shapes to increase the buckling strength. The spars may be wave shaped, such as a sinusoidal shape. The flying surface and the structural members are co-cured in order to form a single piece, integral wing structure. A process for manufacturing a single piece co-cured wing is also disclosed. The process may include laying out composite sheets for the flying surface of the wing. Then, the composite material of the spars is arranged around a plurality of pressurizable forms. Finally, the composite material is cured in a clamshell frame. A single piece co-cured composite structure is also disclosed that includes an outer skin, and inner skin, a frame, and a stringer.

Multi Orientation Composite Material Impregnated With Non-Liquid Resin

US Patent:
2003018, Oct 2, 2003
Filed:
Jun 20, 2002
Appl. No.:
10/175964
Inventors:
Larry Ashton - Mapleton UT, US
Craig Simpson - Mapleton UT, US
Rex Kay - Goshen UT, US
Troy White - Goshen UT, US
Mike Allman - Spanish Fork UT, US
International Classification:
D04H003/00
US Classification:
428/297400
Abstract:
A composite material made of multiple filament bands is disclosed. The filament bands are wound to create a composite material. The filament bands may be impregnated with a solid or semi-solid resin. The filament bands are wound in multiple orientations to form a sheet of composite material. Additionally, the composite material may be made to have a varying number of layer and fiber orientations throughout the sheet of composite material. In another embodiment, a composite component requiring multiple layers and fiber orientations may be substantially manufactured during a filament winding process.

Single Piece Co-Cure Composite Wing

US Patent:
2003019, Oct 16, 2003
Filed:
Jun 20, 2002
Appl. No.:
10/175722
Inventors:
Craig Simpson - Mapleton UT, US
Mike Allman - Spanish Fork UT, US
Steven Tuttle - Springville UT, US
Larry Ashton - Mapleton UT, US
International Classification:
B64C001/00
B64C003/00
B64C005/00
US Classification:
244/123000
Abstract:
A single piece co-cured composite wing is disclosed. The wing has a flying surface and structural members. In one embodiment the structural members may be a plurality of spars. The spars may have various shapes to increase the buckling strength. The spars may be wave shaped, such as a sinusoidal shape. The flying surface and the structural members are co-cured in order to form a single piece, integral wing structure. A process for manufacturing a single piece co-cured wing is also disclosed. The process may include laying out composite sheets for the flying surface of the wing. Then, the composite material of the spars is arranged around a plurality of pressurizable forms. Finally, the composite material is cured in a clamshell frame.

Resin Impregnated Multi Orientation Composite Material

US Patent:
2004007, Apr 22, 2004
Filed:
Oct 14, 2003
Appl. No.:
10/684762
Inventors:
Larry Ashton - Mapleton UT, US
Craig Simpson - Mapleton UT, US
Rex Kay - Goshen UT, US
Troy White - Goshen UT, US
Mike Allman - Spanish Fork UT, US
International Classification:
B65H081/00
US Classification:
156/175000
Abstract:
A composite material made of multiple filament bands is disclosed. The filament bands are wound to create a composite material. The filament bands may be impregnated with a solid or semi-solid resin. The filament bands are wound in multiple orientations to form a sheet of composite material. Additionally, the composite material may be made to have a varying number of layer and fiber orientations throughout the sheet of composite material. In another embodiment, a composite component requiring multiple layers and fiber orientations may be substantially manufactured during a filament winding process.

Resin Impregnated Multi Orientation Composite Material

US Patent:
2013016, Jun 27, 2013
Filed:
Feb 25, 2013
Appl. No.:
13/776560
Inventors:
Larry J. Ashton - Mapleton UT, US
Craig B. Simpson - Mapleton UT, US
Rex W. Kay - Goshen UT, US
Troy L. White - Goshen UT, US
Mike Glen Allman - Spanish Fork UT, US
International Classification:
B32B 37/00
US Classification:
428112, 156169, 156175
Abstract:
A composite material made of multiple filament bands is disclosed. The filament bands are wound to create a composite material. The filament bands may be impregnated with a solid or semi-solid resin. The filament bands are wound in multiple orientations to form a sheet of composite material. Additionally, the composite material may be made to have a varying number of layer and fiber orientations throughout the sheet of composite material. In another embodiment, a composite component requiring multiple layers and fiber orientations may be substantially manufactured during a filament winding process.

Possible Relatives

David Allman  Dawn M Allman  Deborah Allman  Daniel P Allman  Danny W Allman  Dennis E Allman  Donald Allman  Mike A Johnson  Mike A Stanfill  Mike O White 

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