US2377023A - Shipping structure - Google Patents
Shipping structure Download PDFInfo
- Publication number
- US2377023A US2377023A US456964A US45696442A US2377023A US 2377023 A US2377023 A US 2377023A US 456964 A US456964 A US 456964A US 45696442 A US45696442 A US 45696442A US 2377023 A US2377023 A US 2377023A
- Authority
- US
- United States
- Prior art keywords
- shipping
- shipping structure
- floor
- car
- wheel
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 230000000712 assembly Effects 0.000 description 11
- 238000000429 assembly Methods 0.000 description 11
- 238000000034 method Methods 0.000 description 9
- 125000006850 spacer group Chemical group 0.000 description 5
- 229910000746 Structural steel Inorganic materials 0.000 description 4
- 230000006378 damage Effects 0.000 description 4
- 235000000396 iron Nutrition 0.000 description 4
- 230000001681 protective effect Effects 0.000 description 3
- WSNMPAVSZJSIMT-UHFFFAOYSA-N COc1c(C)c2COC(=O)c2c(O)c1CC(O)C1(C)CCC(=O)O1 Chemical compound COc1c(C)c2COC(=O)c2c(O)c1CC(O)C1(C)CCC(=O)O1 WSNMPAVSZJSIMT-UHFFFAOYSA-N 0.000 description 1
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 1
- 208000027418 Wounds and injury Diseases 0.000 description 1
- 230000001133 acceleration Effects 0.000 description 1
- 230000004308 accommodation Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 208000014674 injury Diseases 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 238000010561 standard procedure Methods 0.000 description 1
- 238000010257 thawing Methods 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/50—Handling or transporting aircraft components
Definitions
- This invention relates to a method and device for transporting articles such as airplane wings and other airplane parts, which. are of light weight and large size, and which are readily daniaged by impact with surrounding objects, and particularly to a method and device for transporting articles of this character without the use i of protecting boxing or crating.
- One object of this invention is to provide a method and device for transporting articles of the general character above set forth without the use of boxing or crating which shall protect the transported article from injury or damage.
- Another object of the invention is to provide'a means and method for transporting articles "of the character described without boxing or crating, by which the article will be held immovable with respect to the transporting vehicle and out of contact with any part of the vehicle or with any other object' It is another object of the invention to provide a device and method for transporting articles of the character described which will be economical of shipping space and will lend itself to the loading of a maximum number of articles in a transporting vehicle.
- Another object of the invention is to provide a method and device for transporting a wing panel assembly which includes a nacelle body, without the use of enclosed protective boxing or crating and which is especially adapted to such an assembly.
- Figure 1 is a perspective view showing a shipping structure embodying the invention and having mounted thereon an inboard wing panel assembly including a nacelle body, the panel being shown in phantom lines.
- Figure 2 is a side elevational view of the ping structure shown in Figure 1.
- Figure 3 is a plan view of the shipping structure.
- Figure 4 is a rear elevatlonal view of the shipping structure.
- Figure 5 is an enlarged sectional view taken as indicated by the line 5-5 in Figure 3.
- Figure 6 is an enlarged sectional view taken as indicated by the line 6-45 of Figure 3.
- FIG 1 an inboard wing panel I! of an airplane is shown supported upon a floor H) of a transporting vehicle, such as a freight box car, by means of a shipping structure II.
- the wing panel [2, as will appear hereinafter, is secured to the shipping structure H at only four reinforced contact areas of small size, and the structure is in turn secured to the car floor.
- the dimensions of the wing panel and of the shipping structure and their relative positions are such that no part of the wing panel contacts the floor, side walls or roof of the car, or any other object; except only the four above mentioned areas at which it is secured to the shipping structure.
- the wing panel is thus held both immovable under the shocks and vibrations to which it is subjected during transit, and out of contact with any surrounding objects, impact with which might dent or other wise deform it.
- the wing panel assembly I! is carried with its leading edge l4 adjacent the floor, and its trailing edge 15 directed toward the roof, the body of the panel l3 being horizontally offset with respect to the shipping structure I I and the nacelle shipbody It being vertically above the shipping structure with its lower rim ll directed downward.
- the base of the shipping structure I l consists of four angle irons, welded together to form a rectangular frame having a front bar 24, side bars and a rear bar 26.
- the angle irons forming the base are disposed with one flange lying horizontal in" contact with the floor and the other flange standing vertically upward therefrom.
- Two' upright angle irons 2'! are welded to the rectangular base at the two rear corners thereof, and two other shorter upright angle irons 28 are similarly welded to the rectangular base at the front corners thereof.
- Horizontal channel-iron bars 30 extend from the upper-end of the front being secured to these uprights by welding.
- a front supporting bar 32 connects the upper ends of the front uprights 28 and a rear supporting bar 34 similarly connects the upper ends of the rear uprights 21-.
- The-shipping structure is braced by crossed diagonal angle iron bars-40 and inclined angle iron -.-ba 1's 38, shown.
- the brace bars 40 are reinforced, at their intersection, by a gusset 39 and .the two end portions of each brace bar 38 are reinforced at their connections with the asso- -ciated horizontal side bar 30 by a gusset 31.
- Each of -,the sidebars 25 of the base of the shipping structure is formed with bolt holes 42 to receive bolts for fastening the shipping structure to the car floor.
- the spacer sleeves 50- areshown as welded to the supportingbar 32, although if desired they "may be'separable from the shipping structure uprights 28 to the rear uprights 21 respectively,
- the shipping structure is provided with a detachable wheel 71 at each of its four lower corners.”
- the housing for each front wheel comprises an outside plate Bil and top plate 6! suitably secured to adjacent elements of the framework of the shipping structure.
- a cross angle iron bar 41 connecting the front uprights 28 at a level just above the top plate 6i of the front wheel housings provides additional means for mounting these housings upon the framework of the shipping structure.
- each front wheel housing is centrally apertured at 80 to align with a similar central aperture 8! in the wheel supporting plate 15.
- the wheel assembly is in stalled in the housing by sliding the plate 15 in the guideway 64 from the inner ends of the guideway, and, upon the apertures 80 and BI coming into alignment, by inserting from above a fas- To prevent misplacement of the fastening pin 18, it may be attached'to the frame structure by a fastening chain, as shown in the drawings.
- the rear wheel assemblies are identical with the front wheel assemblies.
- the rear wheel housings comprise an inner sid plate 85, an outer side plate 84 and a top plate-83, welded at suitable points to the frame members of the I shipping structure, as shown in the drawings.
- rear wheel assemblies are installed and secured in the same manner as has already been set forth in describing the front wheel-construction.
- each side bar 25 of the rectangular base of the shipping structure is bent upwardly at 86 to provide a recess for inserting a crow bar or other toolfor prying the shipping structure and wing panel upward from the floor a distance sufficient to permit the installation of the wheel assemblies.
- the wingpanel assembly In loading-a freight car or other transporting vehicle the wingpanel assembly is first bolted to a shipping structure with wheels in place. The wing panel assembly and shipping structure is then placed on a truck and delivered to the car door. The shipping structure with the wing panel assembly is rolled into the car and moved into position for securement to the car floor. A crow bar is inserted in one of the recesses 86 and operated to lift the shipping structure sufficiently to' remove the wheel assemblies from place at "one end of-the shipping structure.
- wheel assemblies do not accompany the shipment in the freight car.
- the positions of securement of the mountedwing assemblies to the floor of the car are selected to place them close to each other and to the side walls of the car in such relative positions with respect to each other and to the car walls, as determined by their overall horizontal dimensions and shape, that as many articles as possible may be shipped in the car.
- the immovability of the wing assemblies, the absence of enclosing box or crate side walls and the position of the shipping structure vertically beneath a portion of the article are all factors contributing to the realization of this result.
- a frame device for-shipping without protective boxing an article of extensive dimensions relative to said device and readily damaged by impact with surrounding objects, the combination of: base members having horizontal surfaces for contactual engagement with the floor of the transporting vehicle, and having bolt holes intersecting said surfaces for the accommodation of bolts to secure the device rigidly to the floor; a superstructure rigidly secured to said base members; supporting members carried by said superstructure at levels substantially above said base members and having surfaces for contact with surfaces on the article when said article is spaced out of contact with the floor, said surfaces being the only surfaces on said device disposed for contact with the article, and said supporting members having all told at least three bolt holes intersecting said surfaces of said supporting members for disposition therein or bolt means for reception within bolt holes in the article to rigidly secure the article to said device; bracing means on said superstructure for bracing it against stresses acting in every direction,
- each mount including a horizontal apertured plate spaced substantially above said horizontal floor contacting surfaces and a pair of parallel horizontal guideway means proximately beneath said plate; a wheel assembly including a horizontal wheel hanger plate for laterally close-fitting, slidable, disposition in said guideway means, having an aperture registrable with said plate aperture; and a drop pin for engagement with said apertures to prevent relative movement of said plates.
- a device for shipping a relatively longarticle having a flexible frame substantially covered .by an imperforate skin comprising: base members adapted to rest on the floor of the transporting vehicle, said base members having passages therethrough for receiving bolts to secure the device rigidly to said floor; a unitary superstructure rigidly secured to said base members, said base members and superstructure constituting a compact openwork frame assembly of small size relative to the Width and length of said article; supporting members carried by said superstructure at levels remotely above said base members and having surfaces adapted to
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- Engineering & Computer Science (AREA)
- Transportation (AREA)
- Manufacturing & Machinery (AREA)
- Aviation & Aerospace Engineering (AREA)
- Packaging Of Machine Parts And Wound Products (AREA)
Description
May 29, 1945. P; w. MILBURN ET AL SHIPPING STRUCTURE Filed Sept. 1, 1942 2 Sheets-Sheet 1 PAUL W. MILBUQN WILLKAM D. ADAMSOM IN V EN TORS y 1945- P. w. MILBURN ET AL 2,377,023
SHIPPING STRUCTURE Filed Sept. 1, 1942 2 Sheets-Sheet 2 PAUL W. MILBUIZN WILLIAM D. ADAMSON INVENTORS BY I (7 0 I ,4 7'7'U/P/VEY Patented May 29, 1945 Paul W. Milburn, Los Angeles,v and William D.
Adamson, West Los Angeles, Calif., assignors to Douglas Aircraft Company, Inc., Santa Monica,
Calif.
Application September 1, 1942, Serial No. 456,964
2 Claims.
This invention relates to a method and device for transporting articles such as airplane wings and other airplane parts, which. are of light weight and large size, and which are readily daniaged by impact with surrounding objects, and particularly to a method and device for transporting articles of this character without the use i of protecting boxing or crating.
It is common practice in the airplane industry,
as in other industries, to fabricate some of the wise damaged upon. contact with surrounding objects. The standard method of transporting wing structures has been within enclosing boxes or crates. One objection to this method is the relatively large volume of car space occupied per article shipped. and another objection is the difficulty of so securing the wing panels within the box that they will not become loosened in transit and be damaged by contact with the box wall and the securing devices within the box.
One object of this invention is to provide a method and device for transporting articles of the general character above set forth without the use of boxing or crating which shall protect the transported article from injury or damage.
Another object of the invention is to provide'a means and method for transporting articles "of the character described without boxing or crating, by which the article will be held immovable with respect to the transporting vehicle and out of contact with any part of the vehicle or with any other object' It is another object of the invention to provide a device and method for transporting articles of the character described which will be economical of shipping space and will lend itself to the loading of a maximum number of articles in a transporting vehicle.
It is another object of the invention to pro- Sill vide a device and method for transporting articles of the character described by which the articles are supported inthe transporting vehicle without contact of any kind with any object except at points on'the article at which thelarticle is particularly adapted to receive stresses without an resulting damage. i
It is another object of the invention to provide a method and device for loading, transporting and unloading articles of the character described without the use of enclosed protective boxing or crating.
Another object of the invention is to provide a method and device for transporting a wing panel assembly which includes a nacelle body, without the use of enclosed protective boxing or crating and which is especially adapted to such an assembly. r
Further objects and advantages of this invention will be brought out in the following description taken in connection with the accompanying drawings and appended claims. In the drawings, which are for illustrative purposes only:
Figure 1 is a perspective view showing a shipping structure embodying the invention and having mounted thereon an inboard wing panel assembly including a nacelle body, the panel being shown in phantom lines.
Figure 2 is a side elevational view of the ping structure shown in Figure 1.
Figure 3 is a plan view of the shipping structure.
Figure 4 is a rear elevatlonal view of the shipping structure.
Figure 5 is an enlarged sectional view taken as indicated by the line 5-5 in Figure 3.,
Figure 6 is an enlarged sectional view taken as indicated by the line 6-45 of Figure 3.
In Figure 1 an inboard wing panel I! of an airplane is shown supported upon a floor H) of a transporting vehicle, such as a freight box car, by means of a shipping structure II. The wing panel [2, as will appear hereinafter, is secured to the shipping structure H at only four reinforced contact areas of small size, and the structure is in turn secured to the car floor. The dimensions of the wing panel and of the shipping structure and their relative positions are such that no part of the wing panel contacts the floor, side walls or roof of the car, or any other object; except only the four above mentioned areas at which it is secured to the shipping structure. The wing panel is thus held both immovable under the shocks and vibrations to which it is subjected during transit, and out of contact with any surrounding objects, impact with which might dent or other wise deform it.
The wing panel assembly I! is carried with its leading edge l4 adjacent the floor, and its trailing edge 15 directed toward the roof, the body of the panel l3 being horizontally offset with respect to the shipping structure I I and the nacelle shipbody It being vertically above the shipping structure with its lower rim ll directed downward.
The base of the shipping structure I l consists of four angle irons, welded together to form a rectangular frame having a front bar 24, side bars and a rear bar 26. The angle irons forming the base are disposed with one flange lying horizontal in" contact with the floor and the other flange standing vertically upward therefrom.
Two' upright angle irons 2'! are welded to the rectangular base at the two rear corners thereof, and two other shorter upright angle irons 28 are similarly welded to the rectangular base at the front corners thereof. Horizontal channel-iron bars 30 extend from the upper-end of the front being secured to these uprights by welding.
A front supporting bar 32 connects the upper ends of the front uprights 28 and a rear supporting bar 34 similarly connects the upper ends of the rear uprights 21-.
The-shipping structure is braced by crossed diagonal angle iron bars-40 and inclined angle iron -.-ba 1's 38, shown. The brace bars 40are reinforced, at their intersection, by a gusset 39 and .the two end portions of each brace bar 38 are reinforced at their connections with the asso- -ciated horizontal side bar 30 by a gusset 31.
Each of -,the sidebars 25 of the base of the shipping structure is formed with bolt holes 42 to receive bolts for fastening the shipping structure to the car floor. 1 4 I The structure, constructed as above described,
4 provides a relatively small, compact sturdy frame which-may be solidly secured to the car floor and which will not have relative movement of its parts when subjected to the dynamic stresses applied to it by the weight of the wing panel assembly-when the car is stopped or started or given sudden movements of acceleration or deceleration in transit.
The two points indicated by arrows $3 0m the nacelle frame It and the-two points indicated by arrows 44 on, the front spar of the wingpanel, to
which the engine mount is secured when the plane is assembled, areutilized to secure-thawing panel assembly l2 to the shipping structure. The
points 43 are aligned with the ends of the rear supporting bar 34-and the points 44 with the ends :of the front supporting bar 32 in mounting the wing panel for shipment. Two spacer sleeves '45 Two paneLwith the bores of these sleeves in registry with two bolt holes at the ends respectively of the supporting bar 32. Bolts 46 are inserted from below through the bolt holes-in these two supporting bars and in the spacing sleeves. Nuts threaded upon the upper ends'of thebolts secure immovably to the ship- 'A' pin 41 is welded to each spacer sleeve and attached to the adjacent bracebar 4!] by achain 48 and fastener bracket 49 welded to the brace 40,
to-provide for securement of the spacer sleeves against misplacement or loss.
The spacer sleeves 50- areshown as welded to the supportingbar 32, although if desired they "may be'separable from the shipping structure uprights 28 to the rear uprights 21 respectively,
and secured thereto in the same manner as spacer sleeves 45.
To facilitate loading and unloading the assembled wing panel and shipping structure and handling and storage operations about a factory or warehouse, the shipping structure is provided with a detachable wheel 71 at each of its four lower corners." Referring to Figure 5, the housing for each front wheel comprises an outside plate Bil and top plate 6! suitably secured to adjacent elements of the framework of the shipping structure.
A cross angle iron bar 41 connecting the front uprights 28 at a level just above the top plate 6i of the front wheel housings provides additional means for mounting these housings upon the framework of the shipping structure.
To the inside face of the outside plate and -to the surface of the top plate 6| are secured respectively the guideway bars 62 and 63 providing guideways 64 within which slides a rectangular wheel supporting plate 5. The wheel H is rotatably mounted between wheel hangers IE3 which are riveted at their upper edges to the wheel supporting plate 75. The top plate 3| of each front wheel housing is centrally apertured at 80 to align with a similar central aperture 8! in the wheel supporting plate 15. ,The wheel assembly is in stalled in the housing by sliding the plate 15 in the guideway 64 from the inner ends of the guideway, and, upon the apertures 80 and BI coming into alignment, by inserting from above a fas- To prevent misplacement of the fastening pin 18, it may be attached'to the frame structure by a fastening chain, as shown in the drawings.
The rear wheel assemblies are identical with the front wheel assemblies. The rear wheel housings comprise an inner sid plate 85, an outer side plate 84 and a top plate-83, welded at suitable points to the frame members of the I shipping structure, as shown in the drawings. The
rear wheel assemblies are installed and secured in the same manner as has already been set forth in describing the front wheel-construction.
The horizontal flange of each side bar 25 of the rectangular base of the shipping structure is bent upwardly at 86 to provide a recess for inserting a crow bar or other toolfor prying the shipping structure and wing panel upward from the floor a distance sufficient to permit the installation of the wheel assemblies.
In loading-a freight car or other transporting vehicle the wingpanel assembly is first bolted to a shipping structure with wheels in place. The wing panel assembly and shipping structure is then placed on a truck and delivered to the car door. The shipping structure with the wing panel assembly is rolled into the car and moved into position for securement to the car floor. A crow bar is inserted in one of the recesses 86 and operated to lift the shipping structure sufficiently to' remove the wheel assemblies from place at "one end of-the shipping structure.
the bolt holes 42.
.sembly mounted thereon is removed from the car and delivered to a place of-storage.
Preferably the wheel assemblies do not accompany the shipment in the freight car. A
proportionately small but adequate number of these wheel assemblies are kept on hand at each shipping, receiving or storage place for use in loading, unloading and moving the shipping structures with wing assemblies mounted thereon.
Thus the cost of the equipment is less and the danger of loss and damage to the wheel assemblies in transit is eliminated. v.
The positions of securement of the mountedwing assemblies to the floor of the car are selected to place them close to each other and to the side walls of the car in such relative positions with respect to each other and to the car walls, as determined by their overall horizontal dimensions and shape, that as many articles as possible may be shipped in the car. The immovability of the wing assemblies, the absence of enclosing box or crate side walls and the position of the shipping structure vertically beneath a portion of the article are all factors contributing to the realization of this result.
While there have been 'described herein certain embodiments of this invention, the invention is not to be understood as confined to these particular embodiments, but is to be given the definition and scope expressed in the following claims.
We claim:
1. In a frame device for-shipping without protective boxing, an article of extensive dimensions relative to said device and readily damaged by impact with surrounding objects, the combination of: base members having horizontal surfaces for contactual engagement with the floor of the transporting vehicle, and having bolt holes intersecting said surfaces for the accommodation of bolts to secure the device rigidly to the floor; a superstructure rigidly secured to said base members; supporting members carried by said superstructure at levels substantially above said base members and having surfaces for contact with surfaces on the article when said article is spaced out of contact with the floor, said surfaces being the only surfaces on said device disposed for contact with the article, and said supporting members having all told at least three bolt holes intersecting said surfaces of said supporting members for disposition therein or bolt means for reception within bolt holes in the article to rigidly secure the article to said device; bracing means on said superstructure for bracing it against stresses acting in every direction,
between the floor and article; at least three wheel mounts carried by said device, each mount including a horizontal apertured plate spaced substantially above said horizontal floor contacting surfaces and a pair of parallel horizontal guideway means proximately beneath said plate; a wheel assembly including a horizontal wheel hanger plate for laterally close-fitting, slidable, disposition in said guideway means, having an aperture registrable with said plate aperture; and a drop pin for engagement with said apertures to prevent relative movement of said plates.
2. A device for shipping a relatively longarticle having a flexible frame substantially covered .by an imperforate skin comprising: base members adapted to rest on the floor of the transporting vehicle, said base members having passages therethrough for receiving bolts to secure the device rigidly to said floor; a unitary superstructure rigidly secured to said base members, said base members and superstructure constituting a compact openwork frame assembly of small size relative to the Width and length of said article; supporting members carried by said superstructure at levels remotely above said base members and having surfaces adapted to
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US456964A US2377023A (en) | 1942-09-01 | 1942-09-01 | Shipping structure |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US456964A US2377023A (en) | 1942-09-01 | 1942-09-01 | Shipping structure |
Publications (1)
Publication Number | Publication Date |
---|---|
US2377023A true US2377023A (en) | 1945-05-29 |
Family
ID=23814863
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US456964A Expired - Lifetime US2377023A (en) | 1942-09-01 | 1942-09-01 | Shipping structure |
Country Status (1)
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US (1) | US2377023A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3250506A (en) * | 1964-04-14 | 1966-05-10 | Beryl E Thouvenelle | Securing support for truck trailers |
US4326726A (en) * | 1980-05-12 | 1982-04-27 | Sl Container Corporation | Storage rack |
US4830386A (en) * | 1986-09-25 | 1989-05-16 | Atlanta Motoring Accessories, Inc. | Automobile hardtop storage rack |
US4867465A (en) * | 1987-06-04 | 1989-09-19 | Troy Marketing Corporation | Storage rack |
US20050220558A1 (en) * | 2004-04-02 | 2005-10-06 | The Cretex Companies, Inc. | Support structure apparatus and method |
-
1942
- 1942-09-01 US US456964A patent/US2377023A/en not_active Expired - Lifetime
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3250506A (en) * | 1964-04-14 | 1966-05-10 | Beryl E Thouvenelle | Securing support for truck trailers |
US4326726A (en) * | 1980-05-12 | 1982-04-27 | Sl Container Corporation | Storage rack |
US4830386A (en) * | 1986-09-25 | 1989-05-16 | Atlanta Motoring Accessories, Inc. | Automobile hardtop storage rack |
US4867465A (en) * | 1987-06-04 | 1989-09-19 | Troy Marketing Corporation | Storage rack |
US20050220558A1 (en) * | 2004-04-02 | 2005-10-06 | The Cretex Companies, Inc. | Support structure apparatus and method |
US7204665B2 (en) * | 2004-04-02 | 2007-04-17 | The Cretex Companies, Inc. | Support structure apparatus and method |
US20070166119A1 (en) * | 2004-04-02 | 2007-07-19 | The Cretex Companies, Inc. | Support structure apparatus and method |
US20070166118A1 (en) * | 2004-04-02 | 2007-07-19 | The Cretex Companies, Inc. | Support structure apparatus and method |
US20070177955A1 (en) * | 2004-04-02 | 2007-08-02 | The Cretex Companies, Inc. | Support structure apparatus and method |
US7326013B2 (en) | 2004-04-02 | 2008-02-05 | The Cretex Companies, Inc. | Support structure apparatus and method |
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