Rapid panel access fastener for highly curved panels

Patent metadata

Field	Value
Publication number	US-9458648-B1
Application number	US-201514713225-A
Country	US
Kind code	B1
Filing date	May 15, 2015
Priority date	May 15, 2015
Publication date	Oct 4, 2016
Grant date	Oct 4, 2016

Abstract

A fastener for highly curved access panels on aircraft or other structures is disclosed. The fastener features a bottom-grasping design which allows for an unblemished outer panel surface, simple and rapid pneumatic fastener actuation for both latching and unlatching, high reliability, built-in clamping pre-load of the access panel onto the structure, 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 pneumatic valve opens upon application of a higher pressure, allowing 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.

First claim

What is claimed is:

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 chamber exceeds a first pressure threshold, and where the Belleville spring deflects upward when the pneumatic pressure in the chamber exceeds a second pressure threshold;
a pneumatic valve fitted in a central bore of the piston proximate the lower end of the piston, where the pneumatic valve opens when the pneumatic pressure in the chamber exceeds a third pressure threshold;
a plurality of locking dogs slidably disposed in an upper end of the piston, where the locking dogs deploy radially outward when exposed to the pneumatic pressure after the pneumatic valve opens; 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 pressure in the chamber to exceed the first threshold in order to deploy the piston upward, increasing the pressure to exceed the second threshold in order to deflect the Belleville spring upward, increasing the pressure to exceed the third threshold in order to open the pneumatic valve and deploy the locking dogs radially outward, decreasing the pressure below a fourth threshold in order to relax the Belleville spring and cause the locking dogs to grasp a lip of the retainer cavity, further decreasing the pressure below a fifth threshold in order to cause the pneumatic valve to close, and further decreasing the pressure to zero to complete the latching.

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, the third threshold is in a range of 110-130 psi, the fourth threshold is in a range of 60-80 psi, and the fifth threshold is in a range of 20-40 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, the pneumatic valve to close, and the piston to retract, and further decreasing the pressure to zero to complete the unlatching.

6. The fastener system of claim 1 wherein the pneumatic valve is a magnetically-seated valve which requires a higher pneumatic pressure to cause the valve to open off of its magnetic seat than to maintain the valve in an open position.

7. The fastener system of claim 1 further comprising a retraction magnet fitted in the upper end of the piston and magnetic pills attached to the locking dogs, where the retraction magnet provides a magnetic force to maintain the locking dogs in a radially inward position when the locking dogs are not exposed to the pneumatic pressure.

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 pistons 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 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 chamber exceeds a first pressure threshold, and where the Belleville spring deflects upward when the pneumatic pressure in the chamber exceeds a second pressure threshold;
a magnetically-seated pneumatic valve fitted in a central bore of the piston proximate the lower end of the piston, where the pneumatic valve opens when the pneumatic pressure in the chamber exceeds a third pressure threshold;
a plurality of locking dogs slidably disposed in an upper end of the piston, where the locking dogs deploy radially outward when exposed to the pneumatic pressure after the pneumatic valve opens; 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 applicati

Assignees

• Northrop Grumman Systems Corp

Inventors

• Neal Matthew A
• Smith Charles R

Classifications

• B64C1/1446

  Inspection hatches (for engine cowls B64D29/08) · CPC title

• E05B51/02 Primary

  by pneumatic or hydraulic means {(E05B17/0029 takes precedence)} · CPC title

• F16B5/0088

  with locking means moving substantially perpendicular to the main plane, e.g. pins, screws · CPC title

• F16B5/0084

  characterised by particular locking means · CPC title

• E05C9/24

  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 title