Lifting method and apparatus
10266376 ยท 2019-04-23
Assignee
Inventors
Cpc classification
International classification
Abstract
A lifting apparatus and method. The lifting apparatus comprising a lower bar assembly, an upper frame assembly, and a plurality of straps. The lower bar assembly comprises a first bar and a second bar. The upper frame assembly comprises a first upper frame bar, a second upper frame bar substantially parallel to the first upper frame bar, and a cross piece connecting the first upper frame bar to the second upper frame bar and substantially perpendicular to the first upper frame bar and the second upper frame bar. The plurality of straps are fixedly attached to the lower bar assembly and slidably attached to the upper frame assembly.
Claims
1. A lifting apparatus, comprising: a lower bar assembly; an upper frame assembly, wherein the upper frame assembly comprises: a first upper frame bar, wherein the first upper frame bar comprises a first attachment structure and a second attachment structure, wherein a first strap runs through the first attachment structure and is slidably attached to the upper frame assembly and a second strap runs through the second attachment structure and is slidably attached to the upper frame assembly, wherein the first and second strap are both fixedly attached to the lower bar assembly, and a second upper frame bar, wherein the second upper frame bar comprises a third attachment structure and a fourth attachment structure, wherein a third strap runs through the third attachment structure and is slidably attached to the upper frame assembly and a fourth strap runs through the fourth attachment structure and is slidably attached to the upper frame assembly, wherein the third and fourth strap are both fixedly attached to the lower bar assembly.
2. The lifting apparatus of claim 1, wherein the lower bar assembly comprises a first lower bar and a second lower bar.
3. The lifting apparatus of claim 1 further comprising padding on the lower bar assembly.
4. The lifting apparatus of claim 1, wherein the upper frame assembly comprises: the second upper frame bar substantially parallel to the first upper frame bar; and a cross piece connects the first upper frame bar to the second upper frame bar and the cross piece is substantially perpendicular to the first upper frame bar and the second upper frame bar.
5. The lifting apparatus of claim 1 further comprising a stop on each strap configured to prevent each strap from becoming disconnected from the upper frame assembly.
6. The lifting apparatus of claim 1 further comprising a payload between the lower bar assembly and the upper frame assembly.
7. The lifting apparatus of claim 6, wherein the payload comprises an aircraft component.
8. A lifting apparatus, comprising: a lower bar assembly comprising a first lower bar and a second lower bar; an upper frame assembly comprising a first upper frame bar, a second upper frame bar substantially parallel to the first upper frame bar, and a cross piece connecting the first upper frame bar to the second upper frame bar and substantially perpendicular to the first upper frame bar and the second upper frame bar; wherein the first upper frame bar comprises a first attachment structure and a second attachment structure, wherein a first strap runs through the first attachment structure and is slidably attached to the upper frame assembly and a second strap runs through the second attachment structure and is slidably attached to the upper frame assembly, wherein the first and second strap are both fixedly attached to the lower bar assembly; and wherein the second upper frame bar comprises a third attachment structure and a fourth attachment structure, wherein a third strap runs through the third attachment structure and is slidably attached to the upper frame assembly and a fourth strap runs through the fourth attachment structure and is slidably attached to the upper frame assembly, wherein both the third and fourth strap are both fixedly attached to the lower bar assembly.
9. The lifting apparatus of claim 8 further comprising padding on the lower bar assembly.
10. The lifting apparatus of claim 8 further comprising a stop on each strap configured to prevent each strap from becoming disconnected from the upper frame assembly.
11. The lifting apparatus of claim 8 further comprising a payload between the lower bar assembly and the upper frame assembly.
12. The lifting apparatus of claim 11, wherein the payload comprises an aircraft component.
13. A method of lifting a payload, comprising: placing a lower bar assembly under the payload; placing an upper frame assembly over the payload, wherein the upper frame assembly comprises a first upper frame bar and a second upper frame bar, wherein the first upper frame bar comprises a first attachment structure and a second attachment structure, wherein a first strap runs through the first attachment structure and is slidably attached to the upper frame assembly and a second strap slidably runs through the second attachment structure and is slidably attached to the upper frame assembly, wherein the second upper frame bar comprises a third attachment structure and a fourth attachment structure, wherein a third strap runs through the third attachment structure and is slidably attached to the upper frame assembly and a fourth strap runs through the fourth attachment structure and is slidably attached to the upper frame assembly; fixedly attaching each strap to the lower bar assembly; and pulling upward on each strap to hold the payload between the lower bar assembly and the upper frame assembly and lift the payload.
14. The method of claim 13, wherein the lower bar assembly comprises a first lower bar and a second lower bar.
15. The method of claim 14 further comprising padding on the first lower bar between the first lower bar and the payload and padding on the second lower bar between the second lower bar and the payload.
16. The method of claim 13, wherein the upper frame assembly comprises: the second upper frame bar substantially parallel to the first upper frame bar; and a cross piece connecting the first upper frame bar to the second upper frame bar and substantially perpendicular to the first upper frame bar and the second upper frame bar.
17. The method of claim 13 further comprising a stop on each strap configured to prevent each strap from becoming disconnected from the upper frame assembly.
18. The method claim 13, wherein the payload comprises an aircraft component.
19. The method of claim 13, wherein pulling upward on the straps comprises pulling upward on the straps by a crane.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) The novel features believed characteristic of the illustrative embodiments are set forth in the appended claims. The illustrative embodiments, however, as well as a preferred mode of use, further objectives, and features thereof, will best be understood by reference to the following detailed description of one or more illustrative embodiments of the present disclosure when read in conjunction with the accompanying drawings, wherein:
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DETAILED DESCRIPTION
(9) The illustrative embodiments recognize and take into account different considerations. For example, the illustrative embodiments provide for safely lifting large, awkward components by a single operator. The apparatus comprises an upper frame, a pair of lower beams, and a plurality of straps fixed to the lower beams and slidably coupled to the upper frame. A payload is held between the lower beams and the upper frame when the straps are pulled upward to lift the payload.
(10) Turning to
(11) In accordance with an illustrative embodiment, lifting apparatus 100 comprises upper frame assembly 104 and lower bar assembly 106. Lower bar assembly 106 comprises lower bar 108 and lower bar 110. Lower bar 108 may be referred to as a first lower bar. Lower bar 110 may be referred to as a second lower bar.
(12) Straps 112 may be fixedly attached to lower bar 108 in lower bar assembly 106 and slidably attached to upper frame assembly 104. Straps 114 may be fixedly attached to lower bar 110 in lower bar assembly 106 and slidably attached to upper frame assembly 104.
(13) Upper ends of straps 112 and straps 114 may be attached to lifting device 120. Lifting device 120 may comprise any appropriate device or system for lifting upward on straps 112 and straps 114. For example, without limitation, lifting device 120 may comprise a crane or other appropriate device or system.
(14) In operation, payload 102 is positioned between lower bar assembly 106 and upper frame assembly 104. By pulling upward on straps 112 and straps 114 by lifting device 120, upper frame assembly 104 is forced downward against payload 102 to secure payload 102 in lifting apparatus 100 as payload 102 is moved by lifting apparatus 100.
(15) Stop 122 may be provided on each of straps 112 and straps 114. Stop 122 may comprise any structure attached to straps 112 and straps 114 to prevent straps 112 and straps 114 from sliding through upper frame assembly 104 so as to become separated from upper frame assembly 104. For example, without limitation, upper frame assembly 104 may be lifted and moved by lifting device 120 without lower bar assembly 106 and payload 102 by disconnecting straps 112 and straps 114 from lower bar assembly 106 and lifting upward on straps 112 and straps 114 until stop 122 engages upper frame assembly 104.
(16) The illustration of lifting apparatus 100 in
(17) Turning to
(18) Turning to
(19) Turning to
(20) Lower bar 400 may comprise bar structure 402, padding 404, and attachment structure 405 for fixedly attaching lower bar 400 to straps, such as straps 112 or straps 114 shown in block form in
(21) Turning to
(22) Turning to
(23) Upper frame assembly 600 may comprise upper frame bar 602 and upper frame bar 604. Upper frame bar 602 may be referred to as a first upper frame bar. Upper frame bar 604 may be referred to as a second upper frame bar. Upper frame bar 602 and upper frame bar 604 may be substantially parallel in upper frame assembly 600. Upper frame bar 602 and upper frame bar 604 may be connected to each other by cross piece 606 and cross piece 608. Cross piece 606 and cross piece 608 may be substantially parallel in upper frame assembly 600.
(24) Attachment structure 610 may be provided at each end of upper frame bar 602 and upper frame bar 604 to provide a slidable connection to straps, such as straps 112 and straps 114 shown in block form in
(25) Turning to
(26) Method 700 may begin by positioning the lower bar assembly of the lifting apparatus below a payload to be lifted (operation 702). The upper frame assembly of the lifting apparatus then may be positioned above the payload (operation 704). Straps then may be slidably attached to the upper frame assembly and fixedly attached to the lower bar assembly (operation 706). The straps then may be lifted to lift the payload (operation 708), with the process terminating thereafter.
(27) The flowcharts and block diagrams described herein illustrate the architecture, functionality, and operation of possible implementations of systems and methods according to various illustrative embodiments. It should be noted that the functions noted in a block may occur out of the order noted in the figures. For example, the functions of two blocks shown in succession may be performed substantially concurrently, or the functions of the blocks may sometimes be performed in the reverse order, depending upon the functionality involved. Furthermore, in some alternative implementations, the functions associated with some blocks in the flowcharts and block diagrams may be eliminated.
(28) The description of the different illustrative embodiments has been presented for purposes of illustration and description, and is not intended to be exhaustive or limited to the embodiments in the form disclosed. Many modifications and variations will be apparent to those of ordinary skill in the art. Further, different illustrative embodiments may provide different features as compared to other desirable embodiments. The embodiment or embodiments selected are chosen and described in order to best explain the principles of the embodiments and the practical application of such principles, and enable others of ordinary skill in the art to understand the disclosure for various embodiments with various modifications as may be suited to various uses and applications.