Patent Application
20130105749
This application claims priority to French patent application No. FR 11 03270 filed on Oct. 27, 2011, the disclosure of which is incorporated in its entirety by reference herein.
(1) Field of the Invention
The present invention relates to means for controlling a lifter device, to hoist apparatus, and to an aircraft.
The technical field of the invention is thus the field of devices for hoisting a load that is outside an aircraft.
(2) Description of Related Art
An aircraft, and more particularly a rotorcraft of the helicopter type, may be fitted in optional manner with an installation for transporting external loads.
Such a hoist apparatus may comprise a lifter device capable of lowering or raising a suspension member relative to the fuselage of the aircraft, the suspension member possibly comprising a hoist cable or a hoist chain, for example.
Such a lifter device is commonly referred to as a “winch” by the person skilled in the art. A lifter device conventionally includes a motor that rotates a reel having the suspension member wound thereon.
A hoist apparatus also includes control means for controlling the lifter device. The control means include a grip and at least one control panel.
The control panel may have control members for controlling movement of the suspension member, or indeed for controlling a hook device arranged at the free end of the suspension member. In addition, the control panel may include an indicator for indicating the length of the suspension member that has been deployed from the lifter device, a control button for controlling a beam carrying the lifter device or deflector means of the hoist apparatus, a system for controlling the aircraft, means for shearing the suspension member, and possibly also means for communicating with the aircraft cockpit.
The term “control member” is used to cover any means present on control means for controlling a hoist device.
Under such circumstances, the control means are often fastened to the structure of the aircraft.
An operator, conventionally referred to as a winch operator, holds the control means in one hand and the suspension member in the other hand.
The operator holds the suspension member in order to guide it.
Furthermore, by holding the suspension member, the operator can evaluate the tension exerted on the suspension member in order to determine whether any load suspended from the suspension member is or is not resting on the ground. It is difficult for the operator to assess distances, since such distances are distorted by the aircraft being vertically above the ground.
The state of the art includes document EP 0 120 995 which describes a hoist apparatus having a lifter device co-operating with a suspension member, and a control device connected by a cable to the lifter device.
The control device comprises a unit having a body and handle means. The body then has a longitudinal slot associated with closure means, the slot being open to receive the suspension member and then being closed once the suspension member has been inserted in the slot.
Document U.S. Pat. No. 3,755,725 describes a hoist device having a lifter device connected to a grip, the grip also being connected to a hook.
The following documents are also known: US 2006/226106; FR 1 254 845; and US 2003/057408.
An object of the present invention is thus to provide control means for controlling a hoist device of an aircraft and enabling safety of an operator to be optimized without disturbing control over a winching operation.
According to the invention, control means for controlling a lifter device are provided with a grip for holding in the hand, the grip comprising a body extending longitudinally in a first direction in elevation from a first end to a second end, the control means including at least one control member for controlling the lifter device.
The control means may in particular have control members including members for controlling movement of the suspension member or indeed for controlling a hook device arranged at the free end of the suspension member, an indicator for indicating the length of the suspension member, means for controlling a beam carrying the lifter device or deflector means of the apparatus, means for shearing the suspension member, a system for controlling the aircraft, or indeed means for communicating with the aircraft cockpit.
The control means are also remarkable in particular in that the body includes a groove extending longitudinally in a second direction in elevation, the groove having a back wall and an open section that is open to the outside of the grip so that a suspension member carried by the lifter device can be reversibly inserted in said groove through said open section while allowing the suspension member to slide relative to the grip, the suspension member being held in said groove by the hand of an operator.
Under such circumstances, a suspension member, in particular such as a hoist cable or chain, may be inserted in an open groove of the grip. The control means then comprise a grip containing a blind recess capable of receiving a suspension member, and not a body provided with a slot that is associated with closure means of the type described in document EP 0 120 995.
The invention thus provides control means capable of guiding the suspension member and of controlling a hoist device.
In order to perform a winching operation, an operator takes hold of the control means. The operator then places the control means on the suspension member, the suspension member being capable of sliding in the grip.
The operator may then hold the grip in a first hand, the first hand preventing the suspension member from escaping from the groove in the grip. Thus, while using this first hand, the operator can both manipulate the control members of the control means, and can also guide the suspension member in a plane while using the first hand via the control means.
It should be observed that the first hand is also relatively well protected by the control means. If the suspension member presents metal splinters as a result of wear, any risk of contact between such splinters and the first hand is minimized insofar as the operator does not apply direct force against the suspension member.
Using this first hand on its own, the operator can thus control the lifter device and guide the suspension member manually. An operator is then not disturbed by using such control means insofar as the operator continues to hold the suspension member with one hand.
The operator can thus hold onto the aircraft with the other hand in order to keep in a safe position. The other hand may serve solely to keep the operator in place on the aircraft, and is therefore not used for controlling the lifter device.
It should be observed that since the operator is holding onto the aircraft with the other hand, the operator can also guide the suspension member with the first hand with maximized force and agility.
Finally, the operator can easily and quickly separate the control means from the suspension member, since the open section is closed only by a portion of the operator's first hand. Opening the hand in part enables the suspension member to be extracted from the groove, or enables the suspension member to be caused to penetrate into the groove.
In another aspect, it can be understood that the control means may include wired or wireless connection means connected to the various controlled elements, and in particular to the lifter device.
The control means may also possesses one or more of the following additional characteristics.
For example, the back wall of the groove may face the palm of an operator's hand, with the fingers of said hand covering the groove at least in part, and more particularly the open section of said groove.
In another aspect, the control means optionally include a control panel secured to the second end of the grip, the control panel carrying at least one control member.
In a first variant, the open section is rectilinear. It is then easy to insert the suspension member in the groove.
In a second variant, the open section is curved. It is then more difficult to make the suspension member penetrate into the groove, since the operator needs to perform a particular movement in order to enable the suspension member to be arranged within the grip. However, it should be observed that it is easier to keep the suspension member in this groove.
In a first embodiment, the first direction is parallel to the second direction.
In a second embodiment, the first direction presents an acute angle relative to the second direction. It is then found to be easier to exert a force on the suspension member.
Furthermore, the control means may include a removable trough defining the groove.
Such a trough may optionally be made of a polymer material having a low coefficient of friction and good mechanical strength, such as a material known under the name polyoxymethylene (or polyformaldehyde) or by the initials POM or the trademark Teflon®.
The trough is then a wear part that may be changed without requiring the entire control means to be discarded.
In another aspect, the control means include connection means for connecting the grip to an operator's arm, such as at least one loop or strap. During particular operations, the operator can thus let go of the control means.
In addition to providing control means, the invention also provides a hoist device provided with a lifter device co-operating with a suspension member, the hoist device having control means for controlling the lifter device, the control means comprising a grip for holding in the hand, the grip comprising a body extending longitudinally in a first direction in elevation from a first end to a second end, the control means including at least one control member for controlling said lifter device.
The control means are then of the above-described type.
Finally, the invention also provides an aircraft including such a hoist device.
The invention and its advantages appear in greater detail from the following description of embodiments given by way of illustration and with reference to the accompanying figures, in which:
Elements that are present in more than one of the figures are given the same references in each of them.
Under such circumstances, the hoist device 5 comprises a suspension member 15 such as a hoisting cable or chain. The suspension member 15 then extends under gravity from a lifter device 10 to hook means 16. For example, the hoist device 5 may include a hoist cable 15 carrying a release hook 16, the hoist cable 15 being wound on a winch 10.
In addition, the lifter device may be fastened to the fuselage 2 by a support beam 11 that may optionally be movable.
Furthermore, the hoist device 5 includes control means 20 having at least one control member suitable for controlling the various active elements of the device, specifically the hook means 16, the lifter device 10, and the beam 11, for example.
The control means 20 include a grip 25. The grip possesses a body 30 that may be held in the hand of an operator, and that may well be shaped to match a human hand.
The body 30 then extends in elevation in a first direction Dl from a first end 31 towards a second end 32. Control members 40 for controlling the hoist device may then be fastened to the body 30, or to a control panel 50 secured to the second end 32.
The control members may be connected by wired connections to the relevant elements as in the example shown diagrammatically, however it is also possible to envisage using wireless connections.
Furthermore, the body 30 may include a groove 33 extending longitudinally in elevation in a second direction D2. The groove 33 may optionally be formed in the control panel 50.
The groove 33 also extends in a transverse plane from a back wall 34 towards a section 35 that is transversely open to the outside EXT. Under such circumstances, it is possible to cause an item to penetrate into the groove 33, and in particular the suspension member 15.
The suspension member may be inserted in the groove independently of the position of the hook member, and regardless of the items carried by the hook member.
The operator's palm 100 then comes into abutment against a portion of the body 30 acting as the back wall 34, and advantageously shaped to match the shape of the palm. Conversely, the operator's fingers 101 close over the groove 33, the fingers 101 covering the groove at least in part when the operator grips the grip 25.
It can be understood that the suspension member can slide in the groove 33 under gravity as shown by arrows F0, the suspension member being held in the groove in particular by the operator's fingers. It can also be seen that the second direction is in the gravity direction when the grip 25 is arranged on the suspension member.
Furthermore, it can be seen that the grip may include a replaceable trough 60 defining the groove 33. The trough may thus have U-shaped sections.
With reference to
The operator can thus use a first hand firstly for controlling the hoist device by using the control means 20, and secondly for guiding and moving the suspension member 15 along double-headed arrows F1. Consequently, the operator can then also use the other hand to hold tight to handle means 3 of the aircraft.
In this first embodiment, the first direction D1 is parallel to the second direction D2, and may coincide with the second direction D2.
Furthermore, the open section may be rectilinear in order to make it easier to place the suspension member in the groove 33.
In another variant shown in
In the second embodiment of
In addition, it can be seen that the portion of the grip in contact with the operator's palm 100 may be shaped to match the shape of the palm, this portion also defining the back wall 34 of the groove 33.
This portion may also include a thumb support 90 for supporting the thumb of the first hand that is holding the grip. The thumb may come directly into contact with the suspension member 15.
Furthermore, the inlet section of the groove may be rectilinear or curved.
In addition, with reference to
Independently of the embodiment, it should be observed that the control means may include a plurality of control members 40, e.g. arranged on the control panel 50.
In particular, the control members may include:
an indicator 43 for indicating the length of the suspension member that is deployed out from the lifter device;
a control button 42 for controlling the beam 11 carrying the lifter device 10, or deflector means of the apparatus;
a joypad button 44 for controlling the aircraft, e.g. by co-operating with an autopilot device of the aircraft;
communications means 45 for communicating with the aircraft cockpit;
means for shearing the suspension member; and
a control button 41 for controlling the lifter device, e.g. a button of the trigger type.
Furthermore, with reference to
Naturally, the present invention may be subjected to numerous variations as to its implementation. Although several embodiments are described above, it will readily be understood that it is not conceivable to identify exhaustively all possible embodiments. It is naturally possible to envisage replacing any of the means described by equivalent means without going beyond the ambit of the present invention.
| Number | Date | Country | Kind |
|---|---|---|---|
| 11 03270 | Oct 2011 | FR | national |
