Temporally staged rapid panel access fastener for highly curved panels

• US 9,567,774 B1
• Filed: 07/19/2016
• Issued: 02/14/2017
• Est. Priority Date: 05/15/2015
• Status: Active Grant

• Current Assignee: Northrop Grumman Systems Corporation (Northrop Grumman Corporation)
• Original Assignee: Northrop Grumman Systems Corporation (Northrop Grumman Corporation)
• Inventors: Neal, Matthew A.
• Primary Examiner(s): Davis, Richard G
• Application Number:
  US15/214,158
• Time in Patent Office: 210 Days
• Field of Search: 244/129.4, 244/129.5
• US Class Current: 1/1
• CPC Class Codes: B64C 1/1446 Inspection hatches for engine cowls B64D29/08
• CPC Class Codes: E05B 51/02 by pneumatic or hydraulic means E05B17/0029 takes precedence
• CPC Class Codes: E05C 1/085 With means for assisting depression of the latch bolt during latching
• CPC Class Codes: E05C 9/10 Actuating mechanisms for bars E05C9/02 - E05C9/06 take precedence
• CPC Class Codes: E05C 9/1841 perpendicular to actuating bar
• CPC Class Codes: E05C 9/24 Means for transmitting movements between vertical and horizontal sliding bars, rods or cables for the fastening of wings, e.g. corner guides means for transmitting movements between vertical and horizontal sliding bars, rods or cables, for moving wings into open or closed position E05F7/08
• CPC Class Codes: E05Y 2900/502 for aircraft
• CPC Class Codes: F16B 19/109 Temporary rivets, e.g. with a spring-loaded pin special clamping devices for workpieces to be riveted together, e.g. operating through the rivet holes B21J15/42; hand tools for temporarily connecting sheets before or during assembly operations B25B31/005
• CPC Class Codes: F16B 21/12 with locking-pins or split-pins thrust into holes
• CPC Class Codes: F16B 2200/91 Use of a pneumatic action

Abstract

A fastener for highly curved access panels on aircraft or other structures, featuring a bottom-grasping design allowing for an unblemished outer panel surface, simple and rapid pneumatic fastener actuation, built-in clamping pre-load, and full retractability of the fastener inside the supporting structure. The fastener includes a Belleville spring with a piston centrally disposed therein, where the piston and spring deflect outward upon application of pneumatic pressure. A pressure chamber within the piston has inlet and outlet orifices designed so that the pressure in the piston chamber gradually increases, requiring several seconds to reach a pressure which causes locking dogs in the piston to deploy radially into a cavity in the access panel. When pressure is removed, the Belleville spring relaxes, the locking dogs grasp a lip of the cavity, and the access panel is latched onto the structure with a clamping pre-load. A pneumatic sequence for unlatching is also provided.

Claims

1. An access panel fastener system, said system comprising:

a pneumatic chamber incorporated in a fixed structure;

a Belleville spring retained around its outer periphery to the fixed structure, where a lower surface of said spring is in fluid communication with the pneumatic chamber and the spring is responsive to a pneumatic pressure in the chamber;

a pneumatic piston slidably disposed through a central hole in the Belleville spring, a lower end of said piston being in fluid communication with the pneumatic chamber and responsive to the pneumatic pressure, where the piston deploys upward until a piston base flange contacts the lower surface of the Belleville spring when the pneumatic pressure in the pneumatic chamber exceeds a first pressure threshold, and where the Belleville spring deflects upward when the pneumatic pressure in the pneumatic chamber exceeds a second pressure threshold;

a piston chamber located in a central bore of the piston with a lower orifice proximate the lower end of the piston and an upper orifice proximate an upper end of the piston, where pressurized air from the pneumatic chamber flows through the lower orifice into the piston chamber and flows out of the piston chamber through the upper orifice;

a plurality of locking dogs slidably disposed in the upper end of the piston, where the locking dogs deploy radially outward when the pneumatic pressure in the piston chamber exceeds a third pressure threshold; and

a retainer cavity mounted on a lower surface of a removable panel such that an opening of the cavity faces downward toward the fixed structure, and where the locking dogs when deployed engage with the retainer cavity to lock the removable panel to the fixed structure,

where the fastener system latches the removable panel to the fixed structure upon application of a latching sequence of pneumatic pressures, and the fastener system unlatches the removable panel from the fixed structure upon application of an unlatching sequence of pneumatic pressures.

2. The fastener system of claim 1 wherein, following the latching sequence of pneumatic pressures, the Belleville spring remains partially flexed and provides a tensile force on the pneumatic piston such that the locking dogs pull the removable panel against the fixed structure with a clamping pre-load.

3. The fastener system of claim 1 wherein the latching sequence of pneumatic pressures includes increasing the pneumatic pressure in the pneumatic chamber to exceed the first threshold in order to deploy the piston upward, increasing the pneumatic pressure in the pneumatic chamber to exceed the second threshold in order to deflect the Belleville spring upward, maintaining the pneumatic pressure in the pneumatic chamber above the second threshold while a pressure in the piston chamber rises to exceed the third threshold in order to deploy the locking dogs radially outward, decreasing the pressure in the pneumatic chamber below the second threshold in order to relax the Belleville spring and cause the locking dogs to grasp a lip of the retainer cavity, and further decreasing the pressure to zero to complete the latching sequence.

4. The fastener system of claim 3 wherein the first threshold is in a range of 5-15 pounds per square inch (psi) of pneumatic pressure, the second threshold is in a range of 90-110 psi, and the third threshold is in a range of 25-35 psi.

5. The fastener system of claim 1 wherein the unlatching sequence of pneumatic pressures includes increasing the pressure in the chamber to exceed the second threshold in order to deflect the Belleville spring upward and allow the locking dogs to retract into the piston, decreasing the pressure to allow the Belleville spring to relax, and further decreasing the pressure to zero to complete the unlatching sequence.

6. The fastener system of claim 1 wherein the lower orifice has a diameter of 0.01 inches+/−

20% and the upper orifice has a diameter of 0.019 inches+/−

20%.

7. The fastener system of claim 1 further comprising magnetic pills attached to the locking dogs, where the magnetic pills provide a magnetic force to maintain the locking dogs in a radially inward position when the locking dogs are not exposed to a pneumatic pressure exceeding the third threshold.

8. The fastener system of claim 1 wherein the locking dogs have a shape which fits over a lower lip of the retainer cavity when in a latched condition such that the locking dogs cannot retract into the piston.

9. The fastener system of claim 1 wherein the fixed structure is part of an aircraft, the removable panel is an access panel with a smooth outer surface, and a plurality of the fastener systems are used to secure the access panel to the aircraft, where the plurality of fastener systems are interconnected along a pneumatic supply line such that all of the fastener systems latch or unlatch simultaneously upon application of one of the sequences of pneumatic pressures.

10. The fastener system of claim 9 wherein the pneumatic piston in each of the fastener systems is completely retracted into the fixed structure before the access panel is placed into position on the fixed structure, thereby enabling the access panel to have a highly curved shape.

11. An aircraft access panel fastener system, said system comprising:

a removable access panel located on an exterior surface of an aircraft;

a pneumatic supply line which provides a pneumatic pressure, said pneumatic supply line being incorporated in a fixed structure of the aircraft; and

a plurality of pneumatically-actuated fasteners for latching the access panel to the fixed structure, each of the fasteners comprising;

a pneumatic chamber incorporated in the fixed structure, where the pneumatic chamber is in fluid communication with the pneumatic supply line;

a Belleville spring retained around its outer periphery to the fixed structure, where a lower surface of said spring is in fluid communication with the pneumatic chamber and the spring is responsive to the pneumatic pressure in the pneumatic chamber;

a pneumatic piston slidably disposed through a central hole in the Belleville spring, a lower end of said piston being in fluid communication with the pneumatic chamber and responsive to the pneumatic pressure, where the piston deploys upward until a piston base flange contacts the lower surface of the Belleville spring when the pneumatic pressure in the pneumatic chamber exceeds a first pressure threshold, and where the Belleville spring deflects upward when the pneumatic pressure in the pneumatic chamber exceeds a second pressure threshold;

a piston chamber located in a central bore of the piston with a lower orifice proximate the lower end of the piston and an upper orifice proximate an upper end of the piston, where pressurized air from the pneumatic chamber flows through the lower orifice into the piston chamber and flows out of the piston chamber through the upper orifice;

a plurality of locking dogs slidably disposed in the upper end of the piston, where the locking dogs deploy radially outward when the pneumatic pressure in the piston chamber exceeds a third pressure threshold; and

a retainer cavity mounted on a lower surface of the access panel such that an opening of the cavity faces downward toward the fixed structure, where the locking dogs when deployed engage with the retainer cavity to lock the access panel to the fixed structure, and where the locking dogs have a shape which fits over a lower lip of the retainer cavity when in a latched condition such that the locking dogs cannot retract into the piston,

where the plurality of fasteners latches the access panel to the fixed structure upon application of a latching sequence of pneumatic pressures, and the plurality of fasteners unlatches the access panel from the fixed structure upon application of an unlatching sequence of pneumatic pressures.

12. The fastener system of claim 11 wherein the pneumatic pistons in each of the fasteners is completely retracted into the fixed structure before the access panel is placed into position on the fixed structure, thereby enabling the access panel to have a highly curved shape.

13. The fastener system of claim 11 wherein, following the latching sequence of pneumatic pressures, the Belleville spring in each of the fasteners remains partially flexed and provides a tensile force on the pneumatic piston such that the locking dogs pull the access panel against the fixed structure with a clamping pre-load.

14. The fastener system of claim 11 wherein the latching sequence of pneumatic pressures includes increasing the pressure in the supply line to exceed the first threshold in order to deploy the pistons upward, increasing the pressure in the supply line to exceed the second threshold in order to deflect the Belleville springs upward, maintaining the pneumatic pressure in the supply line above the second threshold while a pressure in the piston chambers rises to exceed the third threshold in order to deploy the locking dogs radially outward, decreasing the pressure in the supply line below the second threshold in order to relax the Belleville springs and cause the locking dogs to grasp a lip of the retainer cavities, and further decreasing the pressure in the supply line to zero to complete the latching sequence.

15. The fastener system of claim 11 wherein the unlatching sequence of pneumatic pressures includes increasing the pressure in the supply line to exceed the second threshold in order to deflect the Belleville springs upward and allow the locking dogs to retract into the pistons, decreasing the pressure in the supply line to allow the Belleville springs to relax, and further decreasing the pressure in the supply line to zero to complete the unlatching sequence.

16. A method for latching a removable access panel to a fixed structure, said method comprising:

providing a plurality of fasteners, where each of said fasteners includes a pneumatic chamber incorporated in the fixed structure, a Belleville spring retained around its outer periphery to the fixed structure where a lower surface of said spring is in fluid communication with the pneumatic chamber, a pneumatic piston slidably disposed through a central hole in the Belleville spring where a lower end of said piston is in fluid communication with the pneumatic chamber, a piston chamber located in a central bore of the piston with a lower orifice proximate the lower end of the piston and an upper orifice proximate an upper end of the piston, where pressurized air from the pneumatic chamber flows through the lower orifice into the piston chamber and flows out of the piston chamber through the upper orifice, a plurality of locking dogs slidably disposed in the upper end of the piston, and a retainer cavity mounted on a lower surface of the access panel such that an opening of the cavity faces downward toward the fixed structure;

placing the access panel in position on the fixed structure;

increasing a pneumatic pressure in a pneumatic supply line from zero to a first pressure, said supply line being in fluid communication with the pneumatic chamber of each of the plurality of fasteners, where the first pressure causes the pneumatic piston in each of the fasteners to deploy upward into the retainer cavity until a piston base flange contacts the lower surface of the Belleville spring;

increasing the pneumatic pressure in the supply line to a second pressure causing the Belleville spring in each of the fasteners to deflect upward;

maintaining the pneumatic pressure in the supply line above the second threshold while a pressure in the piston chambers rises to exceed a third threshold in order to deploy the locking dogs radially outward;

decreasing the pressure in the supply line below the second threshold in order to relax the Belleville springs and cause the locking dogs to grasp a lip of the retainer cavities; and

further decreasing the pneumatic pressure in the supply line to zero.

17. The method of claim 16 wherein, following the decrease of the pneumatic pressure in the supply line to zero, the Belleville spring in each of the fasteners remains partially flexed and provides a tensile force on the pneumatic piston such that the locking dogs pull the access panel against the fixed structure with a clamping pre-load.

18. The method of claim 16 wherein the first pressure is in a range of 5-15 pounds per square inch (psi) of pneumatic pressure, the second pressure is in a range of 90-110 psi, and the third pressure is in a range of 25-35 psi.

19. The method of claim 16 further comprising a sequence for unlatching the removable access panel from the fixed structure, where the unlatching sequence includes:

increasing the pneumatic pressure in the supply line to the second pressure, causing the Belleville spring in each of the fasteners to deflect upward and releasing the locking dogs from the lower lip of the retainer cavity, thus allowing the locking dogs to retract into the piston;

decreasing the pneumatic pressure in the supply line to allow the Belleville springs to relax and the pistons to partially retract; and

decreasing the pneumatic pressure in the supply line to zero to allow the pistons to fully retract into the fixed structure.

20. The method of claim 16 wherein the pneumatic piston in each of the fasteners is completely retracted into the fixed structure before the access panel is placed into position on the fixed structure, thereby enabling the access panel to have a highly curved shape.