IP Library Granted Patent US 11,851,035
Granted Patent B2
US 11,851,035 · App. 17/197,342 · Granted Dec 26, 2023

Multi-stance aerial device control and display

Inventor: James Roger Lackore, Jr. (Big Bend, WI)
Assignee: Spartan Fire, LLC
B60S9/04G01C5/00G01F1/00G01V11/002A62C27/00A62C31/005A62C31/28E06C5/42
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Quick Facts
Patent No.
US 11,851,035
App. No.
17/197,342
Granted
Dec 26, 2023
Kind
B2
Abstract

A vehicle including a body and an aerial device operable to rotate, extend, and retract relative to the body. The vehicle further includes a control panel, an electronic display, a computer control system, and an aerial elevation sensor that senses an elevation of the aerial device, wherein the computer control system receives a piece of data corresponding with the elevation and generates a graphical representation of the current operating ability of the aerial device based on the elevation that is displayed on the electronic display of the control panel.

Claims (37)

1. A vehicle comprising:

a body;

an aerial device operable to rotate, extend, and retract relative to the body;

a stabilizer operable to extend away from the body and configured to contact a ground surface;

a control panel;

an electronic display;

a computer control system; and

a stabilizer sensor that senses an operational parameter of the stabilizer;

wherein the computer control system receives a piece of data sensed by the stabilizer sensor and generates a graphical representation of the current operating ability of the aerial device based on the operational parameter of the stabilizer and the graphical representation of the current operating ability is displayed on the electronic display of the control panel.

2. The vehicle of claim 1 , wherein the operational parameter detected by the stabilizer sensor is the spread of a stabilizer.

3. The vehicle of claim 1 , further comprising an aerial elevation sensor that senses an elevation of the aerial device, wherein the computer control system receives a piece of data corresponding with the elevation and generates the graphical representation of the current operating ability of the aerial device based on the elevation that is displayed on the electronic display of the control panel.

4. The vehicle of claim 1 , further comprising an aerial rotation sensor that senses a rotational position about a rotational axis of the aerial device, wherein the computer control system receives a piece of data corresponding with the rotational position and generates the graphical representation of the current operating ability of the aerial device based on the rotational position that is displayed on the electronic display of the control panel.

5. The vehicle of claim 1 , further comprising an aerial extension sensor that senses an extension of the aerial device along an extension axis, wherein the computer control system receives a piece of data corresponding with the extension and generates the graphical representation of the current operating ability of the aerial device based on the extension that is displayed on the electronic display of the control panel.

6. The vehicle of claim 1 , further comprising a fluid presence sensor that senses fluid presence in a piping of the aerial device, wherein the computer control system receives a piece of data corresponding with the fluid presence and generates the graphical representation of the current operating ability of the aerial device based on the fluid presence that is displayed on the electronic display of the control panel.

7. The vehicle of claim 1 , further comprising a fluid flow sensor that senses fluid flow out of a fluid monitor nozzle, wherein the computer control system receives a piece of data corresponding with the fluid flow and generates the graphical representation of the current operating ability of the aerial device based on the fluid flow that is displayed on the electronic display of the control panel.

8. The vehicle of claim 1 , wherein the graphical representation includes the operational parameter of the stabilizer and the current operating ability of the aerial device.

9. The vehicle of claim 8 , wherein the graphical representation of the current operating ability of the aerial device includes a graphical representation of a number of personnel that can use the aerial device.

10. A vehicle comprising:

a body;

an aerial device operable to rotate, extend, and retract relative to the body;

a control panel;

an electronic display;

a computer control system; and

an aerial elevation sensor that senses an elevation of the aerial device, wherein the computer control system receives a piece of data corresponding with the elevation and generates a graphical representation of the current operating ability of the aerial device based on the elevation that is displayed on the electronic display of the control panel.

11. The vehicle of claim 10 , further comprising an aerial rotation sensor that senses a rotational position about a rotational axis of the aerial device, wherein the computer control system receives a piece of data corresponding with the rotational position and generates the graphical representation of the current operating ability of the aerial device based on the rotational position that is displayed on the electronic display of the control panel.

12. The vehicle of claim 10 , further comprising an aerial extension sensor that senses an extension of the aerial device along an extension axis, wherein the computer control system receives a piece of data corresponding with the extension and generates the graphical representation of the current operating ability of the aerial device based on the extension that is displayed on the electronic display of the control panel.

13. The vehicle of claim 10 , further comprising a fluid presence sensor that senses fluid presence in a piping of the aerial device, wherein the computer control system receives a piece of data corresponding with the fluid presence and generates the graphical representation of the current operating ability of the aerial device based on the fluid presence that is displayed on the electronic display of the control panel.

14. The vehicle of claim 10 , further comprising a fluid flow sensor that senses fluid flow out of a fluid monitor nozzle, wherein the computer control system receives a piece of data corresponding with the fluid flow and generates the graphical representation of the current operating ability of the aerial device based on the fluid flow that is displayed on the electronic display of the control panel.

15. The vehicle of claim 10 , wherein the graphical representation of the current operating ability of the aerial device includes a graphical representation of a number of personnel that can use the aerial device.

16. The vehicle of claim 15 , wherein the graphical representation of the current operating ability of the aerial device includes a graphical representation of a location along the aerial device of the number of personnel.

17. A method for controlling a multi-stance aerial device comprising:

calculating a current operating ability of an aerial device with a computer control system based on a piece of data received from at least one of an aerial rotation sensor, an aerial elevation sensor, an aerial extension sensor, and a stabilizing sensor with a computer control system;

generating a graphical representation of the current operating ability of the aerial device based on the piece of data; and

displaying the graphical representation of the current operating ability of the aerial device on an electronic display.

18. The method of claim 17 , wherein displaying the graphical representation of the current operating ability of the aerial device includes displaying a graphical representation of a number of personnel that can use the aerial device on the electronic display.

19. The method of claim 18 , wherein displaying the graphical representation of the current operating ability of the aerial device includes displaying a graphical representation of a location along the aerial device of the number of personnel.

20. The method of claim 16 , wherein displaying the graphical representation of the current operating ability of the aerial device includes displaying an operational parameter of the stabilizer and the current operating ability of the aerial device.

Continuity (2)
Continuation 15885510 · Jan 31, 2018
Related Publication 20210197770A1 · Jul 1, 2021