US4739691A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Method of and apparatus for loading/unloading a large missile into/from a horizontally positioned canister
Assignee: ATK Launch Systems LLC
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Filing: 1987-02-19
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Granted: 1988-04-26
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Expires: 2007-02-19
Abstract
Abstract Air bearing pads enable the installation of a large missile stage in a canister or removal therefrom while the canister is in a horizontal position. Each air bearing pad includes interior passages which channel air through perforated strutted elements to allow air under pressure applied to the pad to reach exit air holes in either the bottom or top thereof. The pressurized air stream into the pad produces a force in the direction of the exit air holes. The sum of this force from several pads in series and several columns of pads positioned between the missile stage and the canister inside wall at the bottom 120 degree area thereof lifts the missile stage sufficiently to allow movement thereof into or out of the canister by means of a powered winch. The number of air bearing pads required for a large number of canisters may be minimized by removal of the air bearing pads after installation of the missile stage in the canister and replacement thereof with prior art semi-solid lateral support pads.
Inventors
- 👤 Henry W. Beutler
- 👤 Roland T. Ingels
- 👤 Jack R. Kilgore
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-06 20:04
CPC Classifications
F; F42; F42B; F42B39/00; F42B39/24; B; B60; B60V; B60V3/00; B60V3/02; B60V3/025; B65; B65G; B65G7/00; B65G7/02; B65G7/06; F41; F41A; F41A9/00; F41A9/82
Claims Analysis
Total Claims: 9
Claim 1
Independent Claim
169 words
A method of loading the booster assembly of a large missile into a horizontally positioned canister, the booster assembly having a cylindrical surface and the canister having an inside wall, comprising the steps of: (a) positioning a plurality of air bearing pads such that when the booster assembly is installed in the canister said air bearing pads are located between the cylindrical surface of the booster assembly and the inside wall of the canister with said air bearing pads covering a substantial portion of the bottom surface area of the booster assembly; (b) positioning a plurality of standard lateral support pads such that when the booster assembly is installed in the canister said standard lateral support pads are located between the cylindrical surface of the booster assembly and the inside wall of the canister with said standard lateral support pads covering a substantial portion of the remaining surface area of the booster assembly; and (c) pressurizing said air bearing pads prior to installing the booster assembly in the canister.
Claim 2
Independent Claim
169 words
A method of loading the booster assembly of a large missile into a horizontally positioned canister, the booster assembly having a cylindrical surface and the canister having an inside wall, comprising the steps of: (a) positioning a plurality of air bearing pads such that when the booster assembly is installed in the canister said air bearing pads are located between the cylindrical surface of the booster assembly and the inside wall of the canister with said air bearing pads covering a substantial portion of the bottom surface area of the booster assembly; (b) positioning a plurality of standard lateral support pads such that when the booster assembly is installed in the canister said standard lateral support pads are located between the cylindrical surface of the booster assembly and the inside wall of the canister with said standard lateral support pads covering a substantial portion of the remaining surface area of the booster assembly; and (c) pressurizing said air bearing pads prior to installing the booster assembly in the canister.
Claim 3
Dependent Claim
208 words
A method as defined by claim 1 where in said air bearing pads and said lateral support pads are serially connected in longitudinal rows that are secured longitudinally with respect to the booster assembly and the canister, and including the further steps of: (d) once the booster assembly is installed in the canister, rotating the canister about the longitudinal axis thereof until a row of air bearing pads is on top; (e) attaching an end of the said top row of air bearing pads to an end of a serially connected longitudinal row of standard lateral support pads; (f) pulling out the said top row of air bearing pads from between the booster assembly and the canister and at the same time pulling the attached row of standard lateral support pads therein; (g) rotating the canister until another row of air bearing pads is on top and repeating steps (e) and (f) to replace the then top row of air bearing pads with another serially connected longitudinal row of standard lateral support pads and continuing this procedure until all of the air bearing pads have been replaced with standard lateral support pads; whereby to minimize the number of air bearing pads required for a large number of canisters.
Claim 4
Independent Claim
285 words
A method of loading the booster assembly of a large missile into a horizontally positioned canister, the booster assembly having a cylindrical surface and the canister having an inside wall, comprising the steps of: (a) positioning a plurality of air bearing pads such that when the booster assembly is installed in the canister said air bearing pads are located between the cylindrical surface of the booster assembly and the inside wall of the canister with said air bearing pads covering a substantial portion of the bottom surface area of the booster assembly, wherein each of said air bearing pads includes a bottom having exit air holes therein and further includes internal perforated strutted elements and internal passages to channel air through the strutted elements to allow air to reach the exit air holes in the bottom of said air bearing pad, whereby there is produced a force in the direction of the exit air holes, the sum of which forces from the plurality of air bearing pads lifts the booster assembly sufficiently from the inside wall of the canister to allow the booster assembly to be moved into or out of the canister; (b) positioning a plurality of standard lateral support pads such that when the booster assembly is installed in the canister said standard lateral support pads are located between the cylindrical surface of the booster assembly and the inside wall of the canister with said standard lateral support pads covering a substantial portion of the remaining surface area of the booster assembly; (c) pressurizing said air bearing pads prior to installing the booster assembly in the canister; and (d) moving the booster assembly into the canister with the aid of a powered winch.
Claim 5
Independent Claim
285 words
A method of loading the booster assembly of a large missile into a horizontally positioned canister, the booster assembly having a cylindrical surface and the canister having an inside wall, comprising the steps of: (a) positioning a plurality of air bearing pads such that when the booster assembly is installed in the canister said air bearing pads are located between the cylindrical surface of the booster assembly and the inside wall of the canister with said air bearing pads covering a substantial portion of the bottom surface area of the booster assembly, wherein each of said air bearing pads includes a bottom having exit air holes therein and further includes internal perforated strutted elements and internal passages to channel air through the strutted elements to allow air to reach the exit air holes in the bottom of said air bearing pad, whereby there is produced a force in the direction of the exit air holes, the sum of which forces from the plurality of air bearing pads lifts the booster assembly sufficiently from the inside wall of the canister to allow the booster assembly to be moved into or out of the canister; (b) positioning a plurality of standard lateral support pads such that when the booster assembly is installed in the canister said standard lateral support pads are located between the cylindrical surface of the booster assembly and the inside wall of the canister with said standard lateral support pads covering a substantial portion of the remaining surface area of the booster assembly; (c) pressurizing said air bearing pads prior to installing the booster assembly in the canister; and (d) moving the booster assembly into the canister with the aid of a powered winch.
Claim 6
Independent Claim
308 words
A method of loading the booster assembly of a large missile into a horizontally positioned canister, the booster assembly having a cylindrical surface and the canister having an inside wall, comprising the steps of: (a) positioning a plurality of air bearing pads such that when the booster assembly is installed in the canister said air bearing pads are located between the cylindrical surface of the booster assembly and the inside wall of the canister with said air bearing pads covering a substantial portion of the bottom surface area of the booster assembly, wherein each of said air bearing pads includes a top having exit air holes therein and further includes internal perforated strutted elements and internal passages to channel air through the strutted elements to allow air to reach the exit air holes in the top of each air bearing pad, whereby there is produced a force in the direction of the exit air holes, the sum of which forces from the plurality, of air bearing pads lifts the booster assembly sufficiently from the inside wall of the canister to allow the booster assembly to be moved into or out of the canister, (b) positioning a plurality of standard lateral support pads such that when the booster assembly is installed in the canister said standard lateral support pads are located between the cylindrical surface of the booster assembly and the inside wall of the canister with said standard lateral support pads covering a substantial portion of the remaining surface area of the booster assembly, wherein said air bearing pads and said standard lateral support pads are each arranged in longitudinal rows and are secured to the canister; (c) pressurizing said air bearing pads prior to installing the booster assembly in the canister; and (d) moving the booster assembly into the canister with the aid of a powered winch.
Claim 7
Independent Claim
308 words
A method of loading the booster assembly of a large missile into a horizontally positioned canister, the booster assembly having a cylindrical surface and the canister having an inside wall, comprising the steps of: (a) positioning a plurality of air bearing pads such that when the booster assembly is installed in the canister said air bearing pads are located between the cylindrical surface of the booster assembly and the inside wall of the canister with said air bearing pads covering a substantial portion of the bottom surface area of the booster assembly, wherein each of said air bearing pads includes a top having exit air holes therein and further includes internal perforated strutted elements and internal passages to channel air through the strutted elements to allow air to reach the exit air holes in the top of each air bearing pad, whereby there is produced a force in the direction of the exit air holes, the sum of which forces from the plurality, of air bearing pads lifts the booster assembly sufficiently from the inside wall of the canister to allow the booster assembly to be moved into or out of the canister, (b) positioning a plurality of standard lateral support pads such that when the booster assembly is installed in the canister said standard lateral support pads are located between the cylindrical surface of the booster assembly and the inside wall of the canister with said standard lateral support pads covering a substantial portion of the remaining surface area of the booster assembly, wherein said air bearing pads and said standard lateral support pads are each arranged in longitudinal rows and are secured to the canister; (c) pressurizing said air bearing pads prior to installing the booster assembly in the canister; and (d) moving the booster assembly into the canister with the aid of a powered winch.
Claim 8
Dependent Claim
167 words
An air bearing pad for loading and unloading large cylindrical missiles into a horizontally positioned canister and for removing the missile therefrom comprising: a rubber cushion-like structure having opposing walls that are configured to conform to the curvature of the outside surface of the missile and the inside wall of the canister into which the missile is to be positioned, said cushion-like structure including exit air holes in one of the opposing walls and further including internal perforated strutted elements and internal passages to channel air through the strutted elements to allow air to reach the exit air holes in said one of said opposing walls, wherein said cushion-like structure includes a skirt around the edges of said one of said opposing walls thereof to contain the air and thereby enhance the force produced in the direction of the exit air holes, whereby, upon the introduction of air under pressure into said cushion-like structure, there is produced a force in the direction of the exit air holes.
Claim 9
Dependent Claim
167 words
An air bearing pad for loading and unloading large cylindrical missiles into a horizontally positioned canister and for removing the missile therefrom comprising: a rubber cushion-like structure having opposing walls that are configured to conform to the curvature of the outside surface of the missile and the inside wall of the canister into which the missile is to be positioned, said cushion-like structure including exit air holes in one of the opposing walls and further including internal perforated strutted elements and internal passages to channel air through the strutted elements to allow air to reach the exit air holes in said one of said opposing walls, wherein said cushion-like structure includes a skirt around the edges of said one of said opposing walls thereof to contain the air and thereby enhance the force produced in the direction of the exit air holes, whereby, upon the introduction of air under pressure into said cushion-like structure, there is produced a force in the direction of the exit air holes.
References Cited (Backward Citations)
US3094223A
Cited
US3072022A
Cited
US3513934A
Cited
US3826329A
Cited
US3857321A
Cited
US3923165A
Cited
US4172506A
Cited
US4602552A
Cited
US4604940A
Cited
US4646617A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1991-04-26 | 1991-10-26 | 1992-04-26 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1995-04-26 | 1995-10-26 | 1996-04-26 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1999-04-26 | 1999-10-26 | 2000-04-26 | $7700.00 | Window Closed / Lapsed |