US2111557A

US2111557A - Airplane wing structure

Info

Publication number: US2111557A
Application number: US72496A
Authority: US
Inventors: Nicholas A Draim
Original assignee: Individual
Current assignee: Individual
Priority date: 1936-04-03
Filing date: 1936-04-03
Publication date: 1938-03-22
Anticipated expiration: 1955-03-22

Description

March 22, 1938. N A, D AM 2,111,557

AIRPLANE WING STRUCTURE Filed April 3, 1936 INVENTOR N/CHOLAS A. DRA/M ATTORNEY Patented Mar. 22, 1938 UNITED STATES PATENT OFFICE 1 Claim.

(Granted under the act of March 3, 1883, as amended April 30, 1928; 370 0. G. 757) This invention relates to an airplane wing structure and it has a particular relation to means for securing the fabric to the frame or rib elements thereof.

The principal object of the invention is the provision of means for attaching the fabric to the ribs of an airplane wing so as to present a Sub stantially flush surface to the airflow.

Another object of the invention is the provision of means whereby the fabric may quickly and easily be secured to and removed from the frame structure of the wing without in any way sacrificing the supporting characteristics of the wing, and which will effectively resist any tendency to rip or tear at this point due to the friction of the airflow.

With these and other objects in view, as well as other advantages that may be incident to the use of the improvements, the invention consists in the parts and combinations thereof hereinafter set forth and claimed, and with the understanding that the several necessary elements constituting the same may be varied in proportion and arrangement without departing from the nature and scope of the invention, as defined in the appended claim.

In order to make the invention more clearly understood, there are shown in the accompanying drawing, means for carrying the invention into practical use, without limiting the improvements in their useful application to the particular construction, which, for the purpose of explanation, have been made the subject of illustration.

In the accompanying drawing:

Fig. 1 is an enlarged transverse sectional view through an airplane wing rib and illustrating the improved means for securing thefabric thereto; and

Fig. 2 is a similar view of another form of rib construction.

Referring to the drawing, and particularly to Fig. 1 thereof, an airplane wing structure embodying the invention is shown as comprising a hollow rib member ID of modified U-shape in cross section and formed at its outer edge with outwardly extending flanges I l. Secured to these flanges by welding, riveting, or in any preferred manner, is a member l2 having a central depression l3 which closes and seats within the space along the outer side of the rib l0.

Extending over the outer surface of the rib l0 and member I2 is the main supporting fabric M of the wing which is flexed inwardly into the depression l3, as indicated at l5, and secured therein by a channel member or retaining strip l6. Thismember securely clamps the fabric in posit-ion and is secured within the depression l3 by fastening means in the form of tubular rivets H. The retaining strip l5 and fastening means l6 are disposed wholly within the outer fabric sup porting surface of the rib and are enclosed by a strip of tape l8 which bridges these members and is secured to the fabric I8 along its edges by a suitable adhesive so as to present a substantially flush unbroken surface to the airflow of the wing.

In Fig. 2 a slightly modified rib constructionds illustrated wherein a depression I9 is formed directly in the outer edge of a tubular rib 20, and in which the fabric is secured in a manner similar to that previously described. It will be noted, however, that in both of these constructions the parts which secure the fabric to the rib are disposed entirely within the plane of the airflow and present little or no resistance thereto.

A construction such as that described enables the fabric to be quickly and easily attached to or removed from the supporting structure with the simplest of tools and from the outside surface of the wing. Moreover, the fabric is held in position in a continuous line rather than at intervals, which materially reduces the tendency for the fabric to rip or tear at its line of attachment,

which tendency has heretofore been principally due to the relative looseness of the fabric between the attaching rivets.

Other modifications and changes in the proportions and arrangement of the parts may be made by those skilled in the art without departing from the nature and scope of the invention as defined in the appended claim.

The invention described herein may factured and used by or for the Government of the United States of America for governmental purposes without the payment of any royalties thereon or therefor.

I claim: Airplane wing structure comprising a rib having an inner portion of substantially U-shape in cross-section formed with outwardly extending spaced flanges on the legs thereof and an outer portion having a longitudinally extending depression disposed within the space between the legs of the U-shaped portion and having oppositely extending fabric supporting flanges overlying and secured to the flanges of said U- haped portion; fabric supported by said rib and flexed into the depression of the outer portion thereof; a channel 'member disposed within' the depression of said outer portion for maintaining said fabric from displacement from said rib; headed rivets for securing said channel member in said depression, said channel member and the heads of said rivets being disposed wholly within the outer fabric supporting surfaces of the flanges of the outer portion of said rib; and a strip of tape secured to the outer surface of said fabric and extending over said channel member and rivets and forming a substantially flush outer surface for said wing.

NICHOLAS A. DRAIM.

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