WO2022266454A2 - Aerial lift slope adjustment system - Google Patents

Aerial lift slope adjustment system Download PDF

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Publication number
WO2022266454A2
WO2022266454A2 PCT/US2022/034011 US2022034011W WO2022266454A2 WO 2022266454 A2 WO2022266454 A2 WO 2022266454A2 US 2022034011 W US2022034011 W US 2022034011W WO 2022266454 A2 WO2022266454 A2 WO 2022266454A2
Authority
WO
WIPO (PCT)
Prior art keywords
angle
lower boom
chassis
maximum operating
boom
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.)
Ceased
Application number
PCT/US2022/034011
Other languages
English (en)
French (fr)
Other versions
WO2022266454A3 (en
Inventor
James Randall Christian
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Time Manufacturing Co
Original Assignee
Time Manufacturing Co
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Priority to JP2023577664A priority Critical patent/JP2024524110A/ja
Application filed by Time Manufacturing Co filed Critical Time Manufacturing Co
Priority to EP22825908.1A priority patent/EP4355683A4/en
Priority to MX2023015198A priority patent/MX2023015198A/es
Priority to BR112023026451A priority patent/BR112023026451A2/pt
Priority to CN202280051664.3A priority patent/CN118103320A/zh
Priority to CA3222999A priority patent/CA3222999A1/en
Priority to KR1020247001502A priority patent/KR20240029025A/ko
Priority to AU2022293564A priority patent/AU2022293564A1/en
Publication of WO2022266454A2 publication Critical patent/WO2022266454A2/en
Publication of WO2022266454A3 publication Critical patent/WO2022266454A3/en
Priority to US18/537,538 priority patent/US20240132335A1/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B66HOISTING; LIFTING; HAULING
    • B66FHOISTING, LIFTING, HAULING OR PUSHING, NOT OTHERWISE PROVIDED FOR, e.g. DEVICES WHICH APPLY A LIFTING OR PUSHING FORCE DIRECTLY TO THE SURFACE OF A LOAD
    • B66F17/00Safety devices, e.g. for limiting or indicating lifting force
    • B66F17/006Safety devices, e.g. for limiting or indicating lifting force for working platforms
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B66HOISTING; LIFTING; HAULING
    • B66FHOISTING, LIFTING, HAULING OR PUSHING, NOT OTHERWISE PROVIDED FOR, e.g. DEVICES WHICH APPLY A LIFTING OR PUSHING FORCE DIRECTLY TO THE SURFACE OF A LOAD
    • B66F11/00Lifting devices specially adapted for particular uses not otherwise provided for
    • B66F11/04Lifting devices specially adapted for particular uses not otherwise provided for for movable platforms or cabins, e.g. on vehicles, permitting workmen to place themselves in any desired position for carrying out required operations
    • B66F11/044Working platforms suspended from booms
    • B66F11/046Working platforms suspended from booms of the telescoping type
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B66HOISTING; LIFTING; HAULING
    • B66FHOISTING, LIFTING, HAULING OR PUSHING, NOT OTHERWISE PROVIDED FOR, e.g. DEVICES WHICH APPLY A LIFTING OR PUSHING FORCE DIRECTLY TO THE SURFACE OF A LOAD
    • B66F11/00Lifting devices specially adapted for particular uses not otherwise provided for
    • B66F11/04Lifting devices specially adapted for particular uses not otherwise provided for for movable platforms or cabins, e.g. on vehicles, permitting workmen to place themselves in any desired position for carrying out required operations
    • B66F11/044Working platforms suspended from booms

Definitions

  • the present disclosure relates generally to the field of aerial lifts, and in particular, to safe operation of such lifts. More specifically, the present disclosure provides, inter alia, slope adjustment systems and methods for preventing aerial lifts from overturning during operation.
  • Aerial lifts are commonly used in the electric utility industry to facilitate work at an elevated position in several areas such as utility pole, telephone or power lines, street lights, building walls, etc. Aerial lifts are also widely used beyond the traditional electric utility industry, for example, in construction, emergency rescue, and movie industry, etc.
  • Such aerial lifts typically boast work platforms (e.g., a workstation in the form of a bucket) coupled to wheeled vehicles through a multiple section-boom that is adapted to elevate and orient the aerial platform which carries the personnel who can perform the requisite work.
  • the personnel also typically control the operation of the lift from the aerial platform or bucket through a control assembly that is coupled to the bucket and that includes several handles which can be used to manipulate the position and orientation of the bucket by controlling, among others, the multi-section boom.
  • aerial lifts There are many factors to consider for safe operations of aerial lifts including, e.g., the weather condition such as snow, ice and wind, the land condition such as solid or soft ground, sloped or level surface, etc. Among all possible hazards, overturn is one of the most severe accidents that may happen during aerial lift operation. Accordingly, aerial lifts should operate under constraints when working on sloped surfaces due to overturning stability, operational or structural limitations. However, there is currently no means to determine the exact constraints under different working conditions (/. e. , the varied slope), which largely limits the safe applications of aerial lifts.
  • the present disclosure provides a slope operating system that can measure the slope angle of the ground surface on which an aerial lift is working and further limit the horizontal reach via the lower boom raise function if necessary.
  • one aspect of the present disclosure relates to a slope adjustment system for safe operation of an aerial lift, the aerial lift comprising a pedestal sitting on a movable chassis, a turret connected to the top of the pedestal and is able to rotate horizontally, a lower boom having a first end connected to the upper end of the turret and is able to rotate vertically, a knuckle connecting a second end of the lower boom with a first end of an extendable upper boom, and an aerial work platform connected to a second end of the upper boom, the slope adjustment system comprising: a plurality of sensors, comprising at least a slope sensor and a lower boom sensor, wherein the slope sensor is located on the bottom of the turret and measures in real-time a chassis angle that is the angle of the chassis relative to the horizontal surface, the lower boom sensor is located on the lower boom and measures in real-time a lower boom angle that is the angle of the lower boom relative to the chassis surface; a hydraulic enable valve, which is located in the
  • Another aspect of the present disclosure is directed to a method for preventing an aerial lift from overturning during operation, the aerial lift comprising a pedestal sitting on a movable chassis, a turret connected to the top of the pedestal and is able to rotate horizontally, a lower boom having a first end connected to the upper end of the turret and is able to rotate vertically, a knuckle connecting a second end of the lower boom with a first end of an extendable upper boom, and an aerial work platform connected to a second end of the upper boom, the method comprising: a) measuring a chassis angle that is the angle of the chassis relative to the horizontal surface: i.
  • the lower boom is locked at its stowed position, or ii. if the chassis angle measured does not exceed the maximum operating chassis angle, determining a maximum operating lower boom angle based on the chassis angle measured; and b) measuring a lower boom angle that is the angle of the lower boom relative to the chassis surface: i. when the lower boom angle measured is less than the maximum operating lower boom angle, the raise function of the lower boom is enabled, and ii. when the lower boom angle measured reaches the maximum operating lower boom angle, the raise function of the lower boom is disabled.
  • the present disclosure also includes an aerial lift equipped with the slope adjustment system disclosed herein.
  • Fig. 1 illustrates different working status of an aerial lift equipped with a slope adjustment system of the present disclosure.
  • the raise of the lower boom is limited, while on a horizontal surface ⁇ lower panel), it is able to raise to its full capacity.
  • Fig. 2 is a perspective view of an aerial lift equipped with a slope adjustment system, in accordance with certain embodiments of the present disclosure.
  • FIG. 3 is an enlarged view of a portion of the aerial lift of Fig. 2 including the boom rest with a mechanical stow switch, in accordance with certain embodiments of the present disclosure.
  • Fig. 4 is a perspective view of the slope adjustment system described in the present disclosure excluding the boom rest.
  • Fig. 5 is an enlarged view of a portion of the slope adjustment system of Fig. 4 including the control module, the hydraulic enable valve and the slope sensor.
  • Novel systems for safe operation of aerial lifts and methods for preventing aerial lifts from overturning during operation are provided and described.
  • Aerial lifts equipped with such systems or implementing such methods are also provided and described.
  • Various embodiments and modifications are possible and fall within the scope of the present disclosure.
  • a slope adjustment system for safe operation of an aerial lift comprising a pedestal sitting on a movable chassis, a turret connected to the top of the pedestal and is able to rotate horizontally, a lower boom having a first end connected to the upper end of the turret and is able to rotate vertically, a knuckle connecting a second end of the lower boom with a first end of an extendable upper boom, and an aerial work platform connected to a second end of the upper boom
  • the slope adjustment system comprising: a plurality of sensors, comprising at least a slope sensor and a lower boom sensor, wherein the slope sensor is located on the bottom of the turret and measures in real-time a chassis angle that is the angle of the chassis relative to the horizontal surface, the lower boom sensor is located on the lower boom and measures in real-time a lower boom angle that is the angle of the lower boom relative to the chassis surface; a hydraulic enable valve, which is located in the
  • a “horizontal surface” refers to a flat surface at right angles to a plumb line.
  • a horizontal surface herein can be used interchangeably with a “level surface” in normal operation of an aerial lift that is standard in the industry.
  • a “level surface” refers to a surface that at every point is perpendicular to a plumb line or the direction in which gravity acts, or parallel to the surface of still water.
  • the lower boom angle can be determined by measuring the lower boom’s orientation relative to the horizontal surface.
  • the algorithm employed by the control module is as follows: 1) if the value of the chassis angle received is equal to or greater than a maximum operating chassis angle, the hydraulic enable valve is switched off, the lower boom is locked at its stowed position, and the mechanical stow switch is on; or 2) if the value of the chassis angle received is less than the maximum operating chassis angle, the mechanical stow switch is off and the lower boom is released from its stowed position, the control module determines a maximum operating lower boom angle based on the value of the chassis angle received: a) when the value of the lower boom angle received is less than the maximum operating lower boom angle, the hydraulic enable valve is switched on, and b) when the value of the lower boom angle received reaches the maximum operating lower boom angle, the hydraulic enable valve is switched off.
  • the maximum operating chassis angle varies in different models of aerial lifts.
  • the maximum operating chassis angle can be in the range of 7 to 10 degrees. In some embodiments, the maximum operating chassis angle is 10 degrees.
  • the lower boom can be fully extended (raised) having a maximum operating lower boom angle of 90 degrees when the value of the chassis angle received is equal to or less than a predetermined slope value. That is, an aerial lift working on a sloped surface with an angle that does not exceed a predetermined slope value is allowed to operate to its full envelope range as it operates on a horizontal surface. This predetermined slope value varies depending on aerial lift models. In some embodiments, the predetermined slope value is 5 degrees.
  • the maximum operating chassis angle can exceed 10 degrees if the aerial life is equipped with a suitable set of stabilizers.
  • stabilizers or “outriggers” may refer to auxiliary parts (usually like legs) on a wheeled vehicle that are folded out when it needs stabilization, for example on a crane that lifts heavy loads, or aerial lifts as described in the present disclosure.
  • aerial lifts equipped with stabilizers or outriggers may increase the maximum operating chassis angle by up to 2 degrees.
  • the control module determines the maximum operating lower boom angle based on the value of the chassis angle received and additional parameters selected from the length of the upper boom, the weight of the upper boom, the load of the aerial work platform, and combinations thereof.
  • Exemplary other parameters may include but not limited to the material of the lower boom and/or upper boom, the angle of the upper boom relative to the horizontal surface, the weight of the portion of the aerial lift that is below the pedestal, the weight distribution of the entire aerial lift, etc.
  • the system further comprises a LED panel displaying a real-time status of the aerial lift.
  • the status can be indicated in any suitable manner, e.g., color code, graphic and/or text format, or combinations thereof.
  • Another aspect of the present disclosure is directed to a method for preventing an aerial lift from overturning during operation, the aerial lift comprising a pedestal sitting on a movable chassis, a turret connected to the top of the pedestal and is able to rotate horizontally, a lower boom having a first end connected to the upper end of the turret and is able to rotate vertically, a knuckle connecting a second end of the lower boom with a first end of an extendable upper boom, and an aerial work platform connected to a second end of the upper boom, the method comprising: a) measuring a chassis angle that is the angle of the chassis relative to the horizontal surface: i.
  • the lower boom is locked at its stowed position, or ii. if the chassis angle measured does not exceed the maximum operating chassis angle, determining a maximum operating lower boom angle based on the chassis angle measured; and b) measuring a lower boom angle that is the angle of the lower boom relative to the chassis surface: i. when the lower boom angle measured is less than the maximum operating lower boom angle, the raise function of the lower boom is enabled, and ii. when the lower boom angle measured reaches the maximum operating lower boom angle, the raise function of the lower boom is disabled.
  • the maximum operating chassis angle is in the range of 7 to 10 degrees. In some embodiments, the maximum operating chassis angle is 10 degrees.
  • the maximum operating lower boom angle is 90 degrees when the chassis angle measured is equal to or less than a predetermined slope value. In some embodiments, the predetermined slope value is 5 degrees.
  • the maximum operating chassis angle can exceed 10 degrees if the aerial life is equipped with a suitable set of stabilizers.
  • the maximum operating lower boom angle is determined based on the chassis angle measured and additional parameters selected from the length of the upper boom, the weight of the upper boom, the load of the aerial work platform, and combinations thereof.
  • the chassis angle and the lower boom angle are measured by a set of sensors.
  • the sensors used herein are not limited to any specific type or model. Each senor may work alone or in combination with others.
  • the lower boom angle is measured and monitored in real-time, to ensure the aerial life is operating in safe zone.
  • the present disclosure also includes an aerial lift equipped with the slope adjustment system disclosed herein. [0033]
  • the following discussion provides examples to further illustrate the present disclosure. These examples are illustrative only and are not intended to limit the scope of the disclosure in any way.
  • a typical aerial lift 100 comprises a movable chassis 1 (usually a motor vehicle such as a truck), a pedestal 2 sitting on the movable chassis 1, a turret 3 connected to the top of the pedestal 2 and is able to rotate horizontally, a lower boom 4 (often including a compensation link 401) having a first end 402 connected to the upper end 301 of the turret 3 and is able to rotate vertically, a knuckle 5 connecting a second end 403 of the lower boom 4 with a first end 601 of an extendable upper boom 6, and an aerial work platform 7 connected to a second end 602 of the upper boom 6.
  • a movable chassis 1 usually a motor vehicle such as a truck
  • a pedestal 2 sitting on the movable chassis 1
  • a turret 3 connected to the top of the pedestal 2 and is able to rotate horizontally
  • a lower boom 4 (often including a compensation link 401) having a first end 402 connected to the upper end 301 of the turre
  • the aerial lift 100 When the aerial lift 100 is operating on a horizontal surface or a sloped surface with an angle that is equal to or less than a certain value (that depends on specific aerial lift model, normally 5 degrees), the aerial lift is allowed to operate to its full envelope range, i.e., the lower boom 4 can raise to its full extension without potential risk of overturing due to the change of gravity center of the aerial lift as a whole.
  • the slope angle exceeds, e.g., 5 degrees above the horizontal surface, the structural, functional, and overturning stability limits may be exceeded when the aerial work platform is at a maximum horizontal position, that is, the risk of overturing increases significantly.
  • a solution to this overturing risk is to limit the the lower boom maximum raised position when operating on a sloped surface, as shown in Fig. 1.
  • the present disclosure provides a slope adjustment system to implement this safety measure.
  • the system employs a set of angular sensors to assist determining the limitation on the lower boom raise function.
  • a slope sensor 8 can be installed in the turret 3 and measure in real-time the angle between the chassis 1 and the horizontal surface (i.e., chassis angle).
  • the chassis angle is equivalent to the slope angle of the sloped surface relative to the horizontal surface.
  • the real-time value of the chassis angle is sent to a control module 11 located in the turret 3, which compares the chassis angle value to a predetermined maximum operating chassis angle.
  • the control module 11 then disables the lower boom 4 raise (elevate) function by switching off a hydraulic enable valve 10 that is also located in the turret 3 and operably connected to a hydraulic control valve 13 located inside the pedestal 2 and the lower boom 4 is locked at its stowed position, under certain circurmstances, the upper boom 6 though may be free to operate. If the chassis angle received does not exceed the maximum operating chassis angle, a mechanical stow switch 801 on the top of a boom rest 8 is turned off (Fig. 3) and the slope sensor 8 stops measuring/updating the chassis angle, and both the lower boom 4 and the upper boom 6 are allowed to operate.
  • the control module 11 determines a maximum operating lower boom angle based on the value of the chassis angle last received. This creates a “safe zone” for the lower boom 4 to operate.
  • a lower boom sensor 9 located on the lower boom 4 can measure in real-time a lower boom angle that is the angle of the lower boom relative to the chassis surface (or equivalently the surface on which the aerial lift is operating). The control module 11 receives this real-time lower boom angle and compares it to the prior-determined maximum operating lower boom angle, within which the lower boom 4 can freely operate.
  • the control module 11 switches off the hydraulic enable valve 10, thereby disables the raise function of the lower boom 4 and prevents it from further elevation.
  • an LED panel 12 is also included in the slope adjustment system. The operating personnel can check the panel to monitor the status of the aerial lift and ensure the operation is within the safe zone.
  • Fig. 5 provides an enlarged view focusing on the slope senor 8, the control module 11 and the hydraulic enable valve 10.

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  • Engineering & Computer Science (AREA)
  • Structural Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Geology (AREA)
  • Mechanical Engineering (AREA)
  • Forklifts And Lifting Vehicles (AREA)
PCT/US2022/034011 2021-06-17 2022-06-17 Aerial lift slope adjustment system Ceased WO2022266454A2 (en)

Priority Applications (9)

Application Number Priority Date Filing Date Title
AU2022293564A AU2022293564A1 (en) 2021-06-17 2022-06-17 Aerial lift slope adjustment system
EP22825908.1A EP4355683A4 (en) 2021-06-17 2022-06-17 Aerial lift slope adjustment system
MX2023015198A MX2023015198A (es) 2021-06-17 2022-06-17 Sistema de ajuste de inclinacion de plataforma aerea.
BR112023026451A BR112023026451A2 (pt) 2021-06-17 2022-06-17 Sistema de ajuste de inclinação de elevador aéreo
CN202280051664.3A CN118103320A (zh) 2021-06-17 2022-06-17 空中升降机倾斜度调节系统
JP2023577664A JP2024524110A (ja) 2021-06-17 2022-06-17 空中リフト傾斜調整システム
KR1020247001502A KR20240029025A (ko) 2021-06-17 2022-06-17 공중 리프트 경사 조정 시스템
CA3222999A CA3222999A1 (en) 2021-06-17 2022-06-17 Aerial lift slope adjustment system
US18/537,538 US20240132335A1 (en) 2021-06-17 2023-12-12 Aerial lift slope adjustment system

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US202163211813P 2021-06-17 2021-06-17
US63/211,813 2021-06-17

Related Child Applications (1)

Application Number Title Priority Date Filing Date
US18/537,538 Continuation US20240132335A1 (en) 2021-06-17 2023-12-12 Aerial lift slope adjustment system

Publications (2)

Publication Number Publication Date
WO2022266454A2 true WO2022266454A2 (en) 2022-12-22
WO2022266454A3 WO2022266454A3 (en) 2023-02-02

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ID=84527630

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2022/034011 Ceased WO2022266454A2 (en) 2021-06-17 2022-06-17 Aerial lift slope adjustment system

Country Status (10)

Country Link
US (1) US20240132335A1 (https=)
EP (1) EP4355683A4 (https=)
JP (1) JP2024524110A (https=)
KR (1) KR20240029025A (https=)
CN (1) CN118103320A (https=)
AU (1) AU2022293564A1 (https=)
BR (1) BR112023026451A2 (https=)
CA (1) CA3222999A1 (https=)
MX (1) MX2023015198A (https=)
WO (1) WO2022266454A2 (https=)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2025129279A1 (pt) * 2023-12-20 2025-06-26 Madal Palfinger S/A Pedestal de sustentação para conjunto de elevação de cesto aéreo aplicado em chassi de veículo

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112938853B (zh) * 2021-03-10 2022-05-27 湖南星邦智能装备股份有限公司 高空作业平台实施稳定作业的优化控制方法

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Publication number Priority date Publication date Assignee Title
CA2197583A1 (en) 1996-03-14 1997-09-15 Jean Lavallee Capacity indicator and load measuring system for arial lifts
JP4854318B2 (ja) 2005-04-06 2012-01-18 株式会社アイチコーポレーション 高所作業車

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US6434437B1 (en) * 1999-12-02 2002-08-13 Caterpillar Inc. Boom extension and boom angle control for a machine
JP2001335292A (ja) * 2000-05-30 2001-12-04 Komatsu Ltd 高所作業車
US7489098B2 (en) * 2005-10-05 2009-02-10 Oshkosh Corporation System for monitoring load and angle for mobile lift device
JP7173899B2 (ja) * 2019-02-28 2022-11-16 株式会社アイチコーポレーション 作業車の安全装置

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA2197583A1 (en) 1996-03-14 1997-09-15 Jean Lavallee Capacity indicator and load measuring system for arial lifts
JP4854318B2 (ja) 2005-04-06 2012-01-18 株式会社アイチコーポレーション 高所作業車

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of EP4355683A4

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2025129279A1 (pt) * 2023-12-20 2025-06-26 Madal Palfinger S/A Pedestal de sustentação para conjunto de elevação de cesto aéreo aplicado em chassi de veículo

Also Published As

Publication number Publication date
MX2023015198A (es) 2024-03-25
CA3222999A1 (en) 2022-12-22
US20240132335A1 (en) 2024-04-25
EP4355683A2 (en) 2024-04-24
JP2024524110A (ja) 2024-07-05
AU2022293564A1 (en) 2024-01-04
WO2022266454A3 (en) 2023-02-02
KR20240029025A (ko) 2024-03-05
EP4355683A4 (en) 2025-10-08
CN118103320A (zh) 2024-05-28
BR112023026451A2 (pt) 2024-03-05

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