Pressure relief door assembly

Abstract

A pressure relief door (PRD) assembly includes a PRD frame, a PRD coupled to the PRD frame, a latch element configured to remain in a latched condition to maintain the PRD in a closed condition relative to the PRD frame and to assume an unlatched condition to permit the PRD to assume an open condition relative to the PRD frame in accordance with an occurrence of a burst duct event within the PRD frame and a retention element. The retention element is configured to automatically activate responsive to the PRD opening. The retention element includes an end disposable between the PRD and the PRD frame with the retention element automatically activated to provide positive interference to maintain the PRD in the open condition.

Claims

1. A pressure relief door assembly, comprising: a frame; a pressure relief door coupled to the frame; a latch element configured to remain in a latched condition to maintain the pressure relief door in a closed condition relative to the frame and to assume an unlatched condition to permit the pressure relief door to assume an open condition relative to the frame in accordance with an occurrence of a burst duct event within the frame; and a retention element configured to automatically activate responsive to an opening of the pressure relief door, the retention element including an end to which a bias is applied such that the end is biased to translate in a biasing direction which is transversely oriented relative to a direction of translation of the pressure relief door during the opening of the pressure relief door, and the end being disposable due to the bias between the pressure relief door and the frame with the retention element automatically activated to provide positive interference to maintain the pressure relief door in the open condition.

2. The pressure relief door assembly according to claim 1, wherein the retention element comprises: a first frame element affixed to the pressure relief door; a second frame element affixed to the frame; and an elastic element coupled to one of the first and second frame elements to apply the bias such that the end is: elastically biased in the biasing direction against the other of the first and second frame elements in a non-interfering position with the pressure relief door in the closed condition, and disposable in an interference position between the pressure relief door and the frame with the pressure relief door in the open condition.

3. The pressure relief door assembly according to claim 2, wherein the first and second frame elements are misaligned with one another along an edge of the pressure relief door.

4. The pressure relief door assembly according to claim 2, wherein the first and second frame elements comprise L-shaped brackets.

5. The pressure relief door assembly according to claim 2, wherein the elastic element comprises a leaf spring.

6. The pressure relief door assembly according to claim 2, wherein the elastic element comprises bent flanges extending along a portion of the end.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) The subject matter, which is regarded as the disclosure, is particularly pointed out and distinctly claimed in the claims at the conclusion of the specification. The foregoing and other features, and advantages of the disclosure are apparent from the following detailed description taken in conjunction with the accompanying drawings in which:

(2) FIG. 1 is a top down illustration of an aircraft in accordance with embodiments;

(3) FIG. 2 is a view of an engine nacelle of the aircraft of FIG. 1 from the perspective of a viewer looking through the engine nacelle from a rear of the engine nacelle toward the forward direction;

(4) FIG. 3 is an enlarged version of a portion of the engine nacelle of FIG. 2;

(5) FIG. 4 is a view of a pressure relief door (PRD) of the engine nacelle of FIGS. 2 and 3 and of a PRD assembly in accordance with embodiments from the perspective of a viewer looking radially outwardly from inside the engine nacelle;

(6) FIG. 5 is a perspective view of the PRD assembly of FIG. 4 in a non-interference position;

(7) FIG. 6 is a perspective view of the PRD assembly of FIG. 4 in an interference position; and

(8) FIG. 7 is a schematic diagram illustrating a PRD assembly in accordance with alternative embodiments.

(9) The detailed description explains embodiments of the disclosure, together with advantages and features, by way of example with reference to the drawings.

DETAILED DESCRIPTION OF THE DISCLOSURE

(10) As will be described below, a pressure relief door (PRD) assembly is provided for use with an engine nacelle of an aircraft or another suitable vehicle. The PRD assembly allows for a detection of a burst duct by maintaining the PRD in an open position after a burst duct event, until the PRD is reset and closed by a maintenance worker.

(11) With reference to FIG. 1, an aircraft 1 is provided. The aircraft 1 includes a fuselage 2, which has an aerodynamic nose cone and a trailing portion opposite the nose cone, wings 3 extending outwardly from the fuselage 2, a tail portion 4 at the trailing portion of the fuselage 2 and engines 5. The engines 5 are supported under the wings 3 and within engine nacelles 6. Other engine mounting locations for the engines 5 include the rear side of the fuselage 2. Alternatively, the engines 5 can be built into the tail portion 4.

(12) With continued reference to FIG. 1 and with additional reference to FIGS. 2 and 3, the engine nacelles 6 each include an engine assembly 60, an inner fixed structure (IFS) 61 and an outer fixed structure (OFS) 62 that surrounds the IFS 61. For each engine nacelle 6, the IFS 61 forms an aerodynamic fairing around and provides a PRD frame for the engine assembly 60 and multiple compressed air ducts 601 associated with the engine assembly 60, along with several other auxiliary components, tubes, wire harnesses, etc.

(13) The OFS 62 is disposed to surround the IFS 61 and may be provided as a generally annular element with an aerodynamic taper that narrows toward the trailing end of the engine nacelle 6. The IFS 61 includes an engine PRD frame 610, a PRD 611 that is hinge-coupled to the engine PRD frame 610 and a latch element 612. The engine PRD frame 610 can serve as a frame for the PRD 611 that attaches to the IFS 61 (i.e., a housing) or, in some cases, the PRD 611 can include a door and a hinge that attaches directly to the IFS 61. The latch element 612 may include a spring-loading 613 (see FIG. 3) and is configured to normally remain in a latched condition to thereby maintain the PRD 611 in a closed condition. However, the latch element 612 may also assume an unlatched condition to thereby permit the PRD 611 to assume an open condition in accordance with an occurrence of a burst duct event in any one or more of the multiple ducts 601 to relieve excess pressures.

(14) As shown in FIGS. 2-4, the PRD 611 is disposed in an upper hemisphere of the engine PRD frame 610. As such, if a burst duct event occurs at some point during the operation of the engine 5 or at some other point, the force of gravity will act upon the PRD 611 and cause the PRD 611 to tend to fall toward the latched condition, which would make detection of the burst duct event difficult during a normal inspection of the engine 5 and the engine nacelle 6. In fact, even if the PRD 611 remains open a little bit, it may be difficult for an operator to see because the PRD 611 is located on top of the IFS 61 (and inside of a dark duct), so a more obviously open PRD 611 would be helpful. To this end, each engine nacelle 6 further includes a PRD assembly 10 (see FIG. 4). The PRD assembly 10 includes a PRD retention element 20. The PRD retention element 20 is configured to automatically activate in an event the PRD 611 opens and is further configured to provide positive interference in a manner directed to maintain the PRD 611 in the open condition.

(15) In accordance with embodiments, a single- or multiple-part hinge 614 may be provided proximate to a leading edge 6110 of the PRD 611 to thereby couple the PRD 611 to the engine PRD frame 610 such that the PRD 611 can pivot in an open condition about a hinge axis close to the leading edge 6110. Also, the latch element 612 may be disposed at a trailing edge 6111 of the PRD 611 and the PRD retention element 20 may be disposed at a lateral edge 6112 of the PRD 611. However, it is to be understood that this is not required and that other configurations are possible. These other configurations may include, but are not limited to, the latch element 612 and the PRD retention element 20 being disposed at other edges of the PRD 611 or the latch element 612 and the PRD retention element 20 being incorporated into a same device (e.g., a latch and retention element). With the above in mind, however, and for the purposes of clarity and brevity, the following description will only relate embodiments in which the latch element 612 and the PRD retention element 20 are disposed at the trailing and lateral edges 6111 and 6112, respectively.

(16) With continued reference to FIG. 4 and with additional reference to FIGS. 5 and 6, the PRD retention element 20 includes a first frame element 30, a second frame element 40 and an elastic element 50. The first frame element 30 is affixed to the PRD 611 and may be provided as an L-shaped bracket 31 with a first leg 310 that is fastened to a surface of the PRD 611 and a second leg 311 that protrudes away from a plane of the surface of the PRD 611. The second frame element 40 is affixed to the engine PRD frame 610 and may be provided as an L-shaped bracket 41 with a first leg 410 that is fastened to a surface of the engine PRD frame 610 and a second leg 411 that protrudes away from a plane of the surface of the engine PRD frame 610.

(17) In accordance with embodiments, the respective surfaces of the PRD 611 and the engine PRD frame 610 may be substantially parallel such that the respective first legs 310, 410 of the first and second frame elements 30 and 40 are disposable at a similar plane with the PRD 611 in the closed condition. The respective second legs 311, 411 of the first and second frame elements 30 and 40 may be, but need not be, disposed in parallel with one another. In some embodiments, the second leg 411 of the second frame element 40 may be at least partially superimposed over a portion of the PRD 611.

(18) In accordance with further embodiments, the first frame 30 and the second frame 40 may be axially misaligned with respect to one another and, with such a misaligned configuration, the elastic element 50 may be provided as a leaf spring 501 that is substantially as wide as the height of the respective second legs 311, 411 of the first and second frame elements 30 and 40. The elastic element 50 has a first end 51 and a second end 52. The elastic element 50 is coupled to one of the first and second frame elements 30 and 40 at the first end 51 such that the second end 52 extends distally toward the other of the first and second frame elements 30 and 40 (for purposes of clarity and brevity, the following description will relate to the case in which the first end 51 is coupled to the second leg 311 of the first frame element 30 and that the second end 52 extends distally toward the second frame element 40). The second end 52 includes bent flanges 521 on either lateral side thereof and further includes generally continuous first and second curves 522, 523 that provide the elastic element with a predefined elasticity.

(19) The second end 52 is thus elastically biased against the second leg 411 of the second frame element 40 in a non-PRD-interfering position with the PRD 611 in the closed condition (see FIG. 5). Here, it is noted that since at least the second leg 411 of the second frame element 40 is superimposed over the portion of the PRD 611, the second end 52 is maintained in a superimposed position over the PRD 611 and in a non-superimposed position with respect to the engine PRD frame 610 and thus does not impede movement of the PRD 611 from the closed condition to the open position during a burst duct event.

(20) By contrast, the second end 52 is disposable in a PRD-interference position between the PRD 611 and the engine PRD frame 610 with the PRD 611 in the open condition. That is, once the PRD 611 moves into the open condition, the second end 52 passes away from the second leg 411 and is no longer prevented from elastically extending into the PRD interference position between the PRD 611 and the engine PRD frame 610 (see FIG. 6). In this position, the bent flanges 521 impinge against the interior surface of the PRD 611 and the outer surface of the engine PRD frame 610.

(21) In accordance with alternative embodiments and, with reference to FIG. 7, the first and second frame elements 30 and 40 may be axially aligned with respect to one another. In this case, the elastic element 50 may be provided as a compression spring 502 that extends along a substantially straight line in the closed and open conditions.

(22) While the disclosure is provided in detail in connection with only a limited number of embodiments, it should be readily understood that the disclosure is not limited to such disclosed embodiments. Rather, the disclosure can be modified to incorporate any number of variations, alterations, substitutions or equivalent arrangements not heretofore described, but which are commensurate with the spirit and scope of the disclosure. Additionally, while various embodiments of the disclosure have been described, it is to be understood that the exemplary embodiment(s) may include only some of the described exemplary aspects. Accordingly, the disclosure is not to be seen as limited by the foregoing description, but is only limited by the scope of the appended claims.