Helicopter seat safety system

• US 5,746,395 A
• Filed: 10/20/1995
• Issued: 05/05/1998
• Est. Priority Date: 10/20/1995
• Status: Expired due to Term

• Current Assignee: LMS Incorporated (Davey Tree Expert Company)
• Original Assignee: LMS Incorporated (Davey Tree Expert Company)
• Inventors: Peck, Walter Richard, Oates, Ronald Wayne
• Primary Examiner(s): GRANT, WILLIAM ALEXANDER
• Application Number:
  US08/546,073
• Time in Patent Office: 928 Days
• Field of Search: 244/122 R, 244/122 AG, 244/122 AH, 244/122 B, 244/121, 297/216.15, 297/216.16, 297/216.17
• US Class Current: 244/121
• CPC Class Codes: B64D 25/04 Seat modifications

Abstract

A helicopter safety system provides an increased likelihood of survivability without injury during "survivable" helicopter crashes. The system provides spinal compression for precompressing an operator'"'"'s spine in response to a crash signal from a crash sensor. Also included is a strap tensioning device which tensions an inertia reel strap and thus restraining the operator'"'"'s upper body more effectively in the helicopter seat. Preferably, the strap tensioning device is initiated simultaneously with the spinal compression. Also included are energy absorbers connected to the seat pan, for example, between the seat pan and the seat frame, and airbags connected to the harness. The harness also includes a cross coupling element to provide for a lateral support configuration.

Claims

1. A helicopter seat safety system comprising:

a harness, including an inertia reel strap; and

a strap tensioning means engaged with the inertia reel strap, a cockpit floor and a seat frame of the helicopter seat;

wherein the strap tensioning means tensions the inertia reel strap as a result of the occurrence of a specific operational condition, such that an upper body of a seat occupant is pulled toward a back of the helicopter seat;

a seat pan for supporting the buttocks of a seat occupant, and a spinal compression means coupled to the seat pan, wherein the spinal compression means pushes the seat pan in an upward direction relative to the cockpit floor as a result of the occurrence of the specific operational condition; and

the seat frame being coupled to the seat pan and driven by the spinal compression means such that pushing of the seat frame in the upward direction relative to the cockpit floor causes the strap tensioning means to tension the inertia reel strap.

2. A helicopter seat safety system as recited in claim 1, wherein the strap tensioning means comprises:

a slideable block;

an upper roller connected to one end of the slideable block;

a lower roller connected to a second end of the slideable block;

a floor-mounted bracket;

a seat frame-mounted bracket; and

a motion doubling strap,

wherein the upper roller is engaged with the inertia reel strap, the motion doubling strap is connected to the lower roller at a first end and to the seat frame-mounted bracket at a second end, and the motion doubling strap is engaged with the floor-mounted bracket intermediate the first end and the second end.

3. A helicopter seat safety system comprising:

a seat pan for supporting a buttocks of a seat occupant;

a seat frame coupled to and supporting the seat pan;

a spinal compression means connected to the seat frame, wherein the spinal compression means pushes the seat frame and the seat pan in an upward direction as a result of the occurrence of a specific operational condition,

a crash sensor for sensing, as the specific operational condition, a crash condition, wherein the crash sensor causes the spinal compression means to be initiated as a result of sensing of the crash condition,

wherein the spinal compression means includes a ballistic powder charge which is initiated as a result of the crash sensor sensing the crash condition.

4. A helicopter seat safety system as recited in claim 3, further comprising a controller connected to the crash sensor and the ballistic powder charge of the spinal compression means, the controller controlling the initiation of the ballistic powder charge of the spinal compression means in response to the crash sensor.

5. A helicopter seat safety system as recited in claim 4, wherein the ballistic powder charge has at least two different types of powder.

6. A helicopter seat safety system as recited in claim 5, wherein a first powder type of the ballistic powder comprises fast burning pistol powder and a second powder type of the ballistic powder comprises slower burning rifle powder.

7. A helicopter seat safety system as recited in claim 6, wherein the controller controls initiation of the ballistic powder to simultaneously commence firing of the first powder type and the second powder type.

8. A helicopter seat safety system comprising:

a seat pan for supporting a buttocks of a seat occupant;

a seat frame coupled to and supporting the seat pan; and

a spinal compression means connected to the seat frame, wherein the spinal compression means pushes the seat frame and the seat pan in an upward direction as a result of the occurrence of a specific operational condition;

an energy absorber coupled to the seat pan, the energy absorber deforming to absorb energy when a downward force on the seat pan exceeds a predetermined threshold;

a harness, including an inertia reel strap;

a strap tensioning means engaged with the inertia reel strap such that the strap tensioning means tensions the inertia reel strap as a result of the occurrence of the specific operational condition;

a first belt having a first end and a second end, the first end of the first belt being connected to a right-rearward section of the seat pan, the second end of the first belt comprising a first buckle connector;

a second belt having a first end and a second end, the first end of the second belt being connected to a left-rearward section of the seat pan, the second end of the second belt comprising a second buckle connector;

a multi-point buckle having a first receptacle on a left side for receiving the first buckle connector and a second receptacle on a right side for receiving the second buckle connector;

a cross coupling element for maintaining a crossing orientation of the first belt and the second belt in a region of intersection between the first belt and the second belt; and

an airbag connected to at least one of the first belt and the second belt, the airbag being inflated as a result of the occurrence of the specific operational condition.

9. A method of protecting an occupant of a helicopter seat during a crash condition, comprising the steps of:

sensing the crash condition via a crash sensor;

tensioning an inertia reel strap to restrain the occupant'"'"'s upper body in response to the sensed crash condition; and

pushing a seat pan upwards in response to the sensed crash condition;

wherein the pushing and tensioning steps occur in a predetermined sequence and;

wherein the pushing step commences simultaneously with the tensioning step.

10. A method of protecting an occupant of a helicopter seat during a crash condition, comprising the steps of:

sensing the crash condition via a crash sensor;

tensioning an inertia reel strap to restrain the occupant'"'"'s upper body in response to the sensed crash condition; and

pushing a seat pan upwards in response to the sensed crash condition and;

pushing a seat frame which is in fixed engagement with the seat pan, and releasing the seat pan from the fixed engagement with the seat frame.

11. A method as recited in claim 10, wherein the releasing step commences after completion of the pushing step.

12. A method as recited in claim 10,

the pushing further comprising increasing spacing between the seat pan and the cockpit floor thereby increasing the distance of stroke of the energy absorbers.

13. A method as recited in claim 10,

the seat pan pushing step further comprising decreasing a velocity of the seat pan and the buttocks of the occupant during an early portion of the crash condition and reducing energy content of the velocity of the occupant subsequently removed by the energy absorbers.

14. A method of protecting an occupant of a helicopter seat during a crash condition, comprising the steps of:

sensing the crash condition via a crash sensor;

tensioning an inertia reel strap to restrain the occupant'"'"'s upper body in response to the sensed crash condition;

pushing a seat pan and a seat frame, which is in fixed engagement with the seat pan, upwards in response to the sensed crash condition;

the pushing decreasing downward velocity of the seat pan and of the occupant during an early portion of a crash event indicated by the crash condition

subsequently releasing the seat pan from the fixed engagement with the seat frames only earth gravity being active on the seat pan and the occupant for a period of time to precompress the spine of the seat occupant to a desired level.