Computer program for calculating fastener forces

• US 5,884,232 A
• Filed: 12/20/1996
• Issued: 03/16/1999
• Est. Priority Date: 12/20/1996
• Status: Expired due to Fees

• Current Assignee: Mcdonnell Douglas Corporation (The Boeing Co.)
• Original Assignee: Mcdonnell Douglas Corporation (The Boeing Co.)
• Inventors: Buder, Daniel A.
• Primary Examiner(s): Trammell, James P.
• Assistant Examiner(s): SMITH-STEWART, DEMETRA R
• Application Number:
  US08/770,520
• Time in Patent Office: 816 Days
• Field of Search: 364/508, 364/512, 73/847, 73/862.041, 73/862.042, 73/862.52, 73/862.24, 702/42, 52/283, 52/167.3, 52/167.4, 52/167.6, 52/167.8
• US Class Current: 702/42
• CPC Class Codes: G06F 30/15 Vehicle, aircraft or watercraft design
• CPC Class Codes: G06F 30/23 using finite element methods [FEM] or finite difference methods [FDM]

Abstract

A NASTRAN-programmed computer calculates force and moment data for a structure including joints of interest. The NASTRAN data is read by a computer programmed with the invented program. For each joint, the user selects the members which contribute forces to the joint, and also selects the nearest grid point. A computer programmed with the invented program calculates the resultant force and moment at the proximate grid point. The force and moment are originally defined in a global coordinate system, subsequently transformed into a local coordinate system, and then translated to the centroid of the joint'"'"'s fastener pattern. Axial and shear forces for each fastener are calculated for the nominal case wherein all of the fasteners are operative. Furthermore, each fastener, in turn, is assumed not to transmit axial force and the resulting fail-safe axial forces respectively acting on the remaining operative fasteners are calculated. Fastener forces are screened to determine the critical nominal axial and shear forces, and the critical fasteners which transmit the foregoing critical forces; in addition to the critical fail-safe axial force and consonant critical fail-safe fastener.

Claims

1. A computer system for determining forces acting on fasteners forming a joint in a structural system having a grid point included in one of a plurality of structural members, wherein each of the members contributes to a global force and a global moment acting at the grid point, the computer system comprising:

global means for determining said global force and said global moment, with said global force and said global moment being defined in a global coordinate system having an origin at the grid point;

means for transforming said global force and said global moment into a local force and a local moment defined by a local coordinate system;

means for translating said local force and said local moment from the grid point to a pattern centroid located at the joint;

nominal means for calculating a nominal axial force and a nominal shear force acting on each of the fasteners for a nominal case wherein all of the fasteners are operative;

fail-safe means for calculating fail-safe forces acting axially on each of the fasteners for fail-safe cases wherein each of the fasteners, one at a time, is assumed to transfer an axial force equal to zero, and said fail-safe force comprises a resultant axial force on each of the fasteners remaining operative; and

announcing means for announcing characteristics of suitable fasteners, the characteristics comprising the nominal axial forces and nominal shear forces that the fasteners can withstand without failure.

2. A computer system as defined in claim 1 wherein each of the members respectively causes a partial force and partial moment at the grid point, said global means further includes:

superposition means for superimposing said partial forces and said partial moments at the grid point.

3. A computer system as defined in claim 2 further comprising:

means for obtaining said partial forces and said partial moments at the grid point from output data generated by a computer programmed with a NASTRAN computer program.

4. A computer system as defined in claim 3 further comprising:

means for determining a critical nominal axial force comprised of the highest of said nominal axial forces, and a critical nominal axial fastener transmitting said critical nominal axial force;

means for determining a critical nominal shear force comprised of the highest of said nominal shear forces, and a critical nominal shear fastener transmitting said critical nominal shear force; and

means for determining a critical fail-safe force comprised of the highest of said fail-safe forces, and a critical fail-safe fastener transmitting said critical fail-safe force.

5. A computer system as defined in claim 4 wherein:

said nominal means and said fail-safe means both use said local force and said local moment acting at said pattern centroid to make their respective calculations.

6. A computer system as defined in claim 5 wherein each of the fasteners has a diameter, and a pattern is formed by the fasteners, said computer system further comprising:

means for calculating said pattern centroid based upon said pattern and said diameters.

7. A computer system as defined in claim 6, further comprising:

means for displaying said critical nominal axial force and identifying which one of the fasteners is said critical nominal axial fastener;

means for displaying said critical nominal shear force and identifying which one of the fasteners is said critical nominal shear fastener; and

means for displaying said critical fail-safe force and identifying which one of the fasteners is said critical fail-safe fastener.

8. A computer system as defined in claim 7 further comprising:

the grid point being one of a plurality of grid points; and

the grid point lying nearer to the joint than any other of the plurality of grid points.

9. A computer program for determining forces acting on fasteners forming a joint in a structural system having a grid point included in one of a plurality of structural members, wherein each of the structural members contributes to a global force and a global moment acting at the grid point, the computer program containing program instructions for:

determining said global force and said global moment, with said global force and said global moment bring defined in a global coordinate system having an origin at the grid point;

transforming said global force and said global moment into a local force and a local moment defined by a local coordinate system;

translating said local force and said local moment from the grid point to a pattern centroid located at the joint;

calculating a nominal axial force and a nominal shear force acting on each of the fasteners for a nominal case wherein all of the fasteners are operative;

calculating fail-safe forces acting axially on each of the fasteners for each of a plurality of fail-safe cases in which a different one of the fasteners is assumed to be inoperative and therefore to transfer an axial force equal to zero, wherein, for each of said fail-safe cases, said fail-safe force comprises a resultant axial force on each of the fasteners remaining operative; and

directing the computer systems to announce characteristics of suitable fasteners, the characteristics comprising the nominal axial forces and nominal shear forces that the fasteners can withstand without failure.

10. The computer program as set forth in claim 9, wherein each of the members respectively causes a partial force and a partial moment at the grid point, the computer program further contains:

program instructions for superimposing said partial forces and said partial moments at the grid point.

11. The computer program as set forth in claim 10, wherein the computer program further contains program instructions for obtaining said partial forces and said partial moments at the grid point from output data generated by a computer programmed with a NASTRAN computer program.

12. The computer program as set forth in claim 11, wherein the computer program further contains program instructions for:

determining a critical nominal axial force comprised of the highest of said nominal axial forces, and a critical nominal axial fastener transmitting said critical nominal axial force;

determining a critical nominal shear force comprised of the highest of said nominal shear forces, and a critical nominal shear fastener transmitting said critical nominal shear force; and

determining a critical fail-safe force comprised of the highest of said fail-safe forces, and a critical fail-safe fastener transmitting said critical fail-safe force.

13. The computer program as set forth in claim 12, wherein the program instructions calculate said nominal axial and shear forces and said fail-safe forces using said local force and said local moment acting at said pattern centroid.

14. The computer program as set forth is claim 13, wherein each of the fasteners has a diameter, and a pattern is formed by the fasteners, the computer program further contains:

program instructions for calculating said pattern centroid based upon said pattern and said diameters.

15. The computer program as set forth in claim 14, wherein the computer program further contains program instructions for:

displaying said critical nominal axial force and identifying which one of the fasteners is said critical nominal axial fastener;

displaying said critical nominal shear force and identifying which one of the fasteners is said critical nominal shear fastener; and

displaying said critical fail-safe force and identifying which one of the fasteners is said critical fail-safe fastener.

16. The computer program as set forth in claim 15, wherein the grid point is a selected one of a plurality of grid points lying nearest to the joint.

25. A computer-readable memory containing the computer program set forth in claim 9.

26. A computer software storage medium containing the computer program set forth in claim 9.

17. A computer system for determining forces acting on fasteners forming a joint in a structural system having a grid point included in one of a plurality of structural members, wherein each of the structural members contributes to a global force and a global moment acting at the grid point, the computer system comprising:

a memory;

a processor; and

a computer program stored in said memory, wherein said processor is responsive to instructions contained in said computer program for;

determining said global force and said global moment, with said global force and said global moment being defined in a global coordinate system having an origin at the grid point;

transforming said global force and said global moment into a local force and a local moment defined by a local coordinate system;

translating said local force and said local moment from the grid point to a pattern centroid located at the joint;

calculating a nominal shear force and a nominal shear force acting on each of the fasteners for a nominal case wherein all of the fasteners are operative;

calculating fail-safe forces acting axially on each of the fasteners for each of a plurality of fail-safe cases in which a different one of the fasteners is assumed to be inoperative and therefore to transfer an axial force equal to zero, wherein, for each of said fail-safe cases, said fail-safe force comprises a resultant axial force on each of the fasteners remaining operative; and

directing the computer system to announce characteristics of suitable fasteners, the characteristics comprising the nominal axial forces and nominal shear forces that the fasteners can withstand without failure.

18. The computer system as set forth in claim 17, wherein each of the members respectively causes a partial force and a partial moment at the grid point, said processor is further responsive to:

the instructions contained in said computer program for superimposing said partial forces and said partial moments at the grid point.

19. The computer system as set forth in claim 18, wherein said processor is further responsive to the instructions contained in said computer program for obtaining said partial forces and said partial moments at the grid point from output data generated by a computer programmed with a NASTRAN computer program.

20. The computer system as set forth in claim 19 wherein said processor is further responsive to the instructions contained in said computer program for:

determining a critical nominal axial force comprised of the highest of said nominal axial forces, and a critical nominal axial fastener transmitting said critical nominal axial force;

determining a critical nominal shear force comprised of the highest of said nominal shear forces, and a critical nominal shear fastener transmitting said critical nominal shear force; and

determining a critical fail-safe force comprised of the highest of said fail-safe forces, and a critical fail-safe fastener transmitting said critical fail-safe force.

21. The computer system as set forth in claim 20, wherein said processor calculates said nominal axial and shear forces and said fail-safe forces using said local force and said local moment acting at said pattern centroid.

22. The computer system as set forth in claim 21, wherein each of the fasteners has a diameter, and a pattern is formed by the fasteners, said processor is further responsive to:

the instructions contained in said computer program for calculating said pattern centroid based upon said pattern and said diameters.

23. The computer system as set forth in claim 22, wherein said processor is further responsive to the instructions contained in said computer program for:

displaying said critical nominal axial force and identifying which one of the fasteners is said critical nominal axial fastener;

displaying said critical nominal shear force and identifying which one of the fasteners is said critical nominal shear fastener; and

displaying said critical fail-safe force and identifying which one of the fasteners is said critical fail-safe fastener.

24. The computer system as set forth in claim 23, wherein the grid point is a selected one of a plurality of grid points lying nearest to the joint.