System for training helicopter pilots

• US 5,678,999 A
• Filed: 08/07/1995
• Issued: 10/21/1997
• Est. Priority Date: 08/08/1994
• Status: Expired due to Term

• Current Assignee: Augusto Ulderico Cicare
• Original Assignee: Augusto Ulderico Cicare
• Inventors: Cicare, Augusto Ulderico
• Primary Examiner(s): Hirsch, Paul J.
• Application Number:
  US08/511,966
• Time in Patent Office: 806 Days
• Field of Search: 434/32, 434/33, 434/55
• US Class Current: 434/33
• CPC Class Codes: G09B 9/46 the aircraft being a helicopter

Abstract

The invention relates to a system for training helicopter pilots, more particularly to a system to be used as a highly efficient means for complementing present methods for training pilots. The object of the invention is avoiding the stress to which the trainee is subjected during the first flights and providing understanding of the helicopter behavior easily and without risk. The invention proposes a system basically comprised by a structure and a conventional helicopter permitting simulating stationary or translational actual flight without separating from the ground. The structure comprises a shiftable base having a support for free rotation of a frame from which the helicopter is suspended, so that it may raise and lower within set limits and also that it may be tilted to the sides in a restricted way. This giving the possibility of practicing various maneuvers, also considerably reducing the training cost.

Claims

1. A system for training helicopter pilots, particularly, a system for complementing present methods for training pilots in helicopters, comprising, in combination:

a device for simulating the behavior of a helicopter under actual flight, without raising from the ground; and

a conventional helicopter having a mast or rotor shaft and being provided with anchoring means anchored to said device;

the device being comprised of a lower part forming a permanent supporting base for the structure and provided with self-oriented means for displacing the structure on a horizontal plane;

an upper part having a frame, including a vertical shaft on the lower part mounted for free rotation on a vertical support of said base;

said frame including a hollow lower cross member, said vertical shaft being integral with said cross member and being connected thereto at the middle point of said lower cross member;

an upper cross member parallel to the lower cross member;

a pair of extendible, vertical side members engaged respectively to opposite ends of the lower cross member;

means for angularly positioning said helicopter, said means being mounted on the upper cross member, said means including a crosshead carrying a tubular member for engaging the anchoring means of said helicopter, the mast of said helicopter passing coaxially and freely through said tubular member;

said crosshead having a first pair of joint journals engaged to the upper cross member and a second pair of journals located orthogonally with respect to the first pair engaged to said tubular member, the axis of said pair of journals being coplanar with respect to the transverse and longitudinal shafts of the helicopter, and the intersection point coinciding with the axis of the rotation axis of the frame;

the side members of the frame including cylinders, rigidly connected to the lower hollow cross member, and including rods engaged, on one side, connected to the upper cross member and, on the other side, connected to pistons of said cylinders, the pistons forming therein corresponding upper chambers communicating with the atmosphere, and lower chambers communicating with a reservoir containing a fluid under a determined pressure, limited by at least said lower hollow cross member of the frame;

said lower chambers of the cylinders being permanently pressurized by said fluid in order to generate in said rods a force proportional to said pressure, counteracting the helicopter weight for positioning the latter along the vertical shaft, coinciding with the rotating axis of the frame.

2. A system as claimed in claim 1, wherein said lower part of the device, has a polygonal shape and includes a perimetral profile connected by converging radial profiles with a connecting support for the frame rotating shaft, constituted by a tubular hub having flanges for fixing radial profiles of the base.

3. A system as claimed in claim 1, including a tubular hub with end seats for corresponding bearings giving rotating support to said frame shaft, secured to said lower cross member, and provided with a tubular sleeve, said frame shaft having a lower end thread for receiving a nut retaining the shaft in said hub.

4. A system as claimed in claim 1, wherein said frame rotating shaft comprises, over the supporting hub thereof, a sprocket meshing with a pinion of a centrifugal brake, mounted on said base, capable of limiting the rotating speed of the frame.

5. A system as claimed in claim 1, wherein said frame lower cross member has opposite ends thereof and is of hollow, cylindrical shape and on said opposite ends is crossed by the cylinders of the frame side members, said cylinders being closed by end blocks of the lower hollow cross member, against which heads are secured, located outside said cross member, each head having a cylindrical cavity, coaxial to the cylinder axis, connected by means of a first conduit, through the block fixing the head, to the interior of the lower hollow cross member, each head having a second permanent communication conduit with the lower chamber of said cylinders, said head cavity being closed by a resilient material membrane, corresponding to a lower extension of the piston to form, combined with the pressurized fluid contained in said hollow cross member, a means for dampening the end of stroke of the pistons.

6. A system as claimed in claim 1, wherein said frame upper cross member includes a pair of hollow, parallel, profiled, separated members, between which said helicopter mast projects, and which are engaged at their ends by corresponding bridge plates, the latter having corresponding sleeves with interior tapered surfaces for supporting end tapered portions of said rods of the frame side members, said rods projecting through the bridge plates for being secured thereagainst by nuts threaded to said rods.

7. A system as claimed in claim 1, wherein said base is polygonal and said polygonal base comprises said auto-oriented means constituted by wheels mounted on supports joined for free rotation on the perimetral profile of the base.

8. A system as claimed in claim 1, wherein said base includes shifting means for sliding over a water basin.

9. A system as claimed in claim 1, wherein said reservoir for pressurized fluid is a container of pressurized air formed by said lower cross member and an air reservoir in direct communication therewith, to compensate pressure variations in the cylinders of the extendible members.

10. A system as claimed in claim 1, wherein said reservoir for pressurized fluid is a container confining a hydraulic fluid constituted by said lower hollow cross member, having a conduit for fluid inlet, closed by a valve regulating the pressure upon filling to working pressure by a hydraulic pump.

11. A system as claimed in claim 1, wherein said reservoir for pressurized fluid is formed by said frame lower hollow cross member, divided longitudinally by a partition forming a pair of reservoirs of different volumes for said fluid, the lower volume reservoir being in direct communication with the cylinders of extendible members, and the higher volume reservoir through one conduit, wherein a by-pass valve is included which may be selectively operated by the user.

12. A system as claimed in claim 1, wherein said crosshead carrying the tubular member engaging the helicopter anchoring means comprises a ring joined at opposite sides thereof by said first pair of journals to corresponding plates, fixed to facing surfaces of the members forming the upper cross member, the second pair of journals being mounted on the sides of said ring, displaces 90°

with respect to the first pair of journals, remaining on the second pair of journals joined to diametrically opposed points of said tubular member.

13. A system as claimed in claim 1, wherein said tubular member engages the helicopter anchoring means and has a lower flange connected to the housing of the gear box of the main rotor of the helicopter.

14. A system as claimed in claim 1, wherein said device simulates the behavior of a helicopter under stationary and translational flight, under low speed.

15. A system as claimed in claim 1, wherein said frame is of rectangular shape.