On-Board Modular Hoist
20170183205 ยท 2017-06-29
Inventors
Cpc classification
B66D3/20
PERFORMING OPERATIONS; TRANSPORTING
H02P7/06
ELECTRICITY
B66D3/22
PERFORMING OPERATIONS; TRANSPORTING
H02P27/04
ELECTRICITY
B60K6/20
PERFORMING OPERATIONS; TRANSPORTING
International classification
B66D3/22
PERFORMING OPERATIONS; TRANSPORTING
B60K6/20
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A modular winch onboard an aircraft includes at least one cable wound onto a drum. The winch includes a basic mechanical assembly intended to be attached to the aircraft. The basic mechanical assembly is capable of receiving, in a removable manner, at least one module for varying at least one of the performance characteristics of the winch.
Claims
1. A modular winch designed to be onboard an aircraft, said winch including at least one cable wound onto a drum, and comprising a basic mechanical assembly intended to be attached to the aircraft, said basic mechanical assembly being designed to receive, in a removable manner, at least one module for varying at least one of the performance characteristics of said winch, namely the length of the cable, the diameter of the cable, the power of the winch and consequently the winding and unwinding speed of said cable, the power supply of the winch: wherein the basic mechanical assembly attached to the aircraft comprises a mechanical connection connecting a drive module, which is capable of varying the characteristics relating to the power of the winch, to a cable module; and wherein the at least one module comprises a cable module, which is capable of varying characteristics relating to the cable, comprising at least one cable, at least one drum around which the cable is adapted to be wound/unwound, and a rotation portion of said drum designed to be connected to the mechanical connection.
2. The onboard modular winch according to claim 1: wherein the drive module comprises a motor whose drive shaft is designed to be connected to the mechanical connection, and; wherein said mechanical connection is designed to transmit the rotational movement of the drive shaft to the rotation portion of the drum for the winding/unwinding of said cable.
3. The onboard modular winch according to claim 1, wherein the module capable of varying the characteristics relating to the power supply consists of an electronic module, designed to produce an AC or DC current for the drive module from the electrical power generated by the aircraft.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0017] Further characteristics and advantages of the invention will become apparent from the description provided below, which is for reference only and is in no way restrictive, with reference to the accompanying figures, in which:
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DETAILED DESCRIPTION OF THE INVENTION
[0028] With reference to
[0029] The basic mechanical assembly (2) ensures the mechanical (attachment to the aircraft) and electrical (power and control) interfacing between the aircraft and the cable module (3).
[0030] With reference to
[0031] The basic mechanical assembly (2) further comprises mechanical connection means (5) for mechanically connecting the drive module (4) to the cable module (3). The mechanical connection means (5) are arranged on the lower part of the basic mechanical assembly (2) and comprise a hollow shaft (5a) mounted in such a way as to freely rotate. The hollow shaft (5a) has internal splines (6) and is designed to receive a splined shaft that engages on both sides, for transmitting rotation from one to the other.
[0032] The cable module (3) comprises a drum (7) around which said cable (7a) is stored. The cable module (3) helps vary the characteristics relating to the cable (7a). With reference to
[0033] The housing (8) of the cable module (3) comprises internally and partially above, a drum (7) mounted such as to be able to rotate around its axis of rotation. Said drum (7) is latched, via the transmission means (9), to the rotation means (10) such as to allow the winding of a cable (7a) around said drum (7). These rotation means (10) are in the form of a splined shaft (10a) protruding outwards from the housing (8) of the cable module (3). Said splined shaft (10a) is intended to be inserted into the hollow shaft (5a) of the mechanical connection means (5) of the basic mechanical assembly (2), and to engage the internal splines (6) of said hollow shaft (5a).
[0034] The cable (7a) is then attached at one end to the drum (7) and comprises at its free end, a hook and/or a handle (not shown) according to the winching missions to be performed.
[0035] The drive cable (4) helps vary the characteristics relating to power. With reference to
[0036] The rotation of the motor (12) drives the rotation of the splined shaft (15), which leads to the rotation of the hollow shaft (5a), which drives the rotation of the rotation means (10) of the drum (7), and therefore the rotation of the drum (7) allowing the winding or the unwinding of the cable (7a).
[0037] The electronic module helps vary the characteristics relating to the power supply, and can produce an AC or DC current for the drive module from the electrical power generated by the aircraft.
[0038] With reference to
[0039] These different modules are therefore provided with means of implementing, in an easy manner, a mechanical and/or electrical connection between them, in order to facilitate the choice of the user depending upon the mission to be performed.
[0040] As is clear from the foregoing, the invention proposes a modular winch that can be interchanged quickly and easily depending, for example, upon the power of the motor, the length of cable required, etc., especially based upon the winching mission to be performed.
[0041] That said, and as mentioned in the introduction, the basic mechanical assembly (2) can integrate the functions of the drive module (4) and the electronic module.