Aviation crash sensor

• US 6,299,102 B2
• Filed: 03/12/1998
• Issued: 10/09/2001
• Est. Priority Date: 05/12/1995
• Status: Expired due to Fees

• Current Assignee: Conax Florida Corporation (Cobham PLC)
• Original Assignee: H. Koch & Sons Co. (Cobham PLC)
• Inventors: Happ, Michael J.
• Primary Examiner(s): Jordan, Charles T.
• Assistant Examiner(s): DINH, TIEN QUANG
• Application Number:
  US09/041,338
• Publication Number:
  US 20010019089A1
• Time in Patent Office: 1,307 Days
• Field of Search: 244/122.AG, 244/118.5, 244/121, 244/122.R, 280/806
• US Class Current: 244/122.0AG
• CPC Class Codes: B60R 2021/01325 Vertical acceleration
• CPC Class Codes: B60R 21/013 including means for detecting collisions, impending collisions or roll-over
• CPC Class Codes: B60R 21/0133 by integrating the amplitude of the input signal
• CPC Class Codes: B60R 22/4619 Transmission of tensioning power by cable, e.g. using a clutch on reel side
• CPC Class Codes: B64C 27/006 Safety devices
• CPC Class Codes: B64D 25/00 Emergency apparatus or devices, not otherwise provided for parachutes B64D17/00, B64D19/00; jettisoning of fuel tanks or fuel per se B64D37/00; specially adapted for protection against criminal attack, e.g. anti-hijacking systems B64D45/0015 ; safety belts or body harnesses in general A62B35/00; safety belts or body harnesses for land vehicles B60R22/00; jettisonable parts of fuselage facilitating emergency escape B64C
• CPC Class Codes: B64D 25/02 Supports or holding means for living bodies

Abstract

An aircraft crash sensor activates an aircrew safety device upon sensing an aircraft impact in any direction to minimize the aircrew flail envelope and reduce the possibility of injury caused by the crash. The crash sensor is useful in a plurality of different aircraft all having different characteristics and mounting orientations for the crash sensor. It includes accelerometers which sense accelerations along three orthogonal axes. The memory contains algorithms for each of a plurality of different aircraft. The memory also contains a program which converts the acceleration data measured along the sensor'"'"'s axes to acceleration data on the aircraft'"'"'s orthogonal X, Y and Z axes. These converted acceleration signals are input to a microcontroller which evaluates them, by analyzing them with an algorithm contained in non-volatile programmable memory, to determine when a crash has occurred. If a crash is determined, an output signal is provided to operate an aircrew restraint system which secures aircrewmen in their seats, or to air bags or other safety systems. Measured data is stored in memory for future retrieval.

Claims

1. A method of identifying a crash occurrence for any of a plurality of different vehicles to activate a vehicle safety device, comprising the steps of

a. providing an electronic crash sensor for measuring accelerations along three orthogonal axes,

b. programming the crash sensor with an algorithm which analyzes the accelerations along each axis to produce velocity change data and comparing these data to threshold criteria to determine an occurrence of a crash for any of the plurality of vehicles,

c. programming the crash sensor to convert the data along the crash sensor'"'"'s axes to data along the vehicle'"'"'s axes when mounted in any of the plurality of vehicles,

d. mounting the crash sensor in one of the plurality of vehicles in a manner which identifies said one vehicle to provide the threshold criteria and axis conversions of said one of the plurality of vehicles for use by the crash sensor,

e. repeatedly measuring vehicle accelerations along the crash sensor'"'"'s axes to provide measured axis accelerations, converting the measured axis accelerations to converted vehicle axis accelerations, and analyzing the converted vehicle axis accelerations to determine the presence or absence of an acceleration crash pulse, and for as long as the presence of an acceleration crash pulse is determined, engaging a recorder and starting an elapsed time measurement to provide a cumulated time value, repeating said measuring and converting steps to provide successive converted vehicle axis acceleration values and integrating said successive converted vehicle axis acceleration values to provide converted velocity changes and cumulating said converted velocity changes to provide a cumulated velocity change value and analyzing the cumulated velocity change value to determine the presence or absence of a velocity change crash threshold and if the presence of a velocity change crash threshold is determined, comparing said cumulated time value required to reach said velocity change crash threshold with pre-programmed cumulated time values and if said cumulated time value is within said pre-programmed cumulated time values concluding that a crash has occurred, and

f. providing an activation signal to the safety device when a conclusion is reached that a crash has occurred.

2. The method of claim 1, including the step of

g. providing each vehicle with a unique connector which mates with a crash sensor connector to identify each vehicle to the crash sensor.

3. The method of claim 2, including the steps of

h. integrating measured vehicle accelerations to produce orthogonal velocity changes,

i. normalizing said velocity changes, and

j. combining said velocity changes and comparing them with velocity criteria to identify occurrence of a crash threshold.

4. An electronic crash sensor for use in a plurality of vehicles comprising

solid state accelerometers for measuring accelerations along 3 orthogonal axes and producing acceleration signals,

a microprocessor-based controller for receiving and analyzing the acceleration signals to determine occurrence of a crash threshold, and for providing safety device control signals when a crash threshold occurs,

means for mounting the crash sensor in a vehicle,

means for identifying said vehicle to the crash sensor,

a nonvolatile programmable memory having a vehicle identification program which identifies the orientation of the crash sensor'"'"'s orthogonal axes relative to the vehicle'"'"'s axes for each of the plurality of vehicles and converts the crash sensor'"'"'s measured axis accelerations into vehicle axis accelerations,

a control program in said memory containing a crash detection algorithm for analyzing accelerations to determine occurrence of a crash for each of the plurality of vehicles, and

an external communication port enabling control program modification and data retrieval, whereby

the controller repeatedly samples the acceleration signals and utilizes the programs to identify occurrence of a vehicle crash and provide said safety device control signals.

5. The electronic crash sensor of claim 4, including a program for storing vehicle acceleration data in said memory.

6. The electronic crash sensor of claim 4, wherein the means for identifying said vehicle to the crash sensor comprises a connector on the crash sensor and a mating connector on each vehicle which has a physical interface specific to that vehicle.

7. The electronic crash sensor of claim 4, including a digital data bus on the crash sensor enabling communication with, and control of, subsystems on the vehicle.

8. A method of evaluating vehicle acceleration data measured along three measurement axes to identify a predetermined event, which is defined by vehicle acceleration and/or velocity criteria on three vehicle axes which are different from the measurement axes, and to command vehicle safety systems actions, comprising the steps of

a. converting measurement axis acceleration data into vehicle axis acceleration data,

b. applying the converted data to an algorithm which includes one or more of

predetermined acceleration thresholds,

rate of velocity changes, and

magnitude of velocity changes,

 

for each vehicle axis to perform an analysis which determines the occurrence of said predetermined event,

c. commanding vehicle safety systems actions in response to determination of occurrence of said predetermined event, and

d. recording event data for later retrieval.

9. A process for activating an air crew safety device comprising:

mounting a tri-axis accelerometer on an aircraft, said tri-axis accelerometer providing electronic acceleration data along three orthogonal axes, an X axis, a Y axis and a Z axis;

loading an algorithm in a microcontroller processing unit and inputting data limits specific to the aircraft on which the tri-axis accelerometer is mounted to enable said algorithm to determine if a crash threshold has occurred;

repeatedly sampling acceleration values received from said tri-axis accelerometer along said X, Y and Z axes to provide current acceleration values along each axis;

normalizing said current acceleration values by dividing by a normalized coefficient to provide current normalized acceleration values along each axis, squaring said current normalized acceleration values and summing the squared current normalized acceleration value for the X axis and the Y axis and the Z axis to provide a tri-axis summed current normalized acceleration value;

comparing said tri-axis summed current, normalized acceleration value to a pre-programmed acceleration value and if it exceeds said pre-programmed acceleration value, engaging an integrator;

if said integrator is engaged, integrating said current acceleration values to calculate current change in velocity values along each of said axes;

if said integrator is engaged, adding the current change in velocity to any previous changes in velocity values calculated while said integrator is engaged to provide a cumulative changes in velocity along each of said axes and determining the cumulative time that the integrator has been engaged;

normalize said cumulative changes in velocity along each of said axes by dividing by a normalizing velocity coefficient to calculate normalized cumulative changes in velocity along each axis;

raising said normalized cumulative changes in velocity along each axis to a pre-programmable power to provide raised, normalized velocity changes along each axis;

summing the raised, normalized velocity change calculated along the X axis to that calculated along the Y axis and to that calculated along the Z axis to reach a cumulative, triaxial normalized velocity result; and

evaluating the cumulative, triaxial normalized velocity result and the time that the integrator has been engaged to reach said result and compare to a pre-programmed value and if said result is within said pre-program med value, activate air crew safety devices.

10. The process of claim 9 further including the step of mounting the tri-axis accelerometer in an orientation wherein the X, Y and Z axes of said tri-axis accelerometer are not all parallel to respective X, Y and Z axes of said aircraft and before said normalizing the current acceleration values step, converting acceleration data from the axes of said tri-axis accelerometer to vehicle X, Y and Z axes acceleration values and using the calculated vehicle X, Y and Z axes acceleration values in all steps following said normalizing step.