US2397450A - Fabricated structure - Google Patents

Fabricated structure Download PDF

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Publication number
US2397450A
US2397450A US523846A US52384644A US2397450A US 2397450 A US2397450 A US 2397450A US 523846 A US523846 A US 523846A US 52384644 A US52384644 A US 52384644A US 2397450 A US2397450 A US 2397450A
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Prior art keywords
stringers
blanket
flanges
secured
skin
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Expired - Lifetime
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US523846A
Inventor
Watter Michael
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ThyssenKrupp Budd Co
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Edward G Budd Manufacturing Co
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Publication date
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Priority to US523846A priority Critical patent/US2397450A/en
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Publication of US2397450A publication Critical patent/US2397450A/en
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings

Definitions

  • This invention relates to fabricated structures, particularly metallic structures, such as airioils,
  • the blanket is initially provided with relatively heavy stringers and is attached to the framework while there is ample space between the stringers to receive the tool elements needed to make the connection.
  • the clips are first attached to the skin blanket and later attached to the framework.
  • the blanket is secured to the framework, it may be desirable to further stiffen or strengthen it and, according to the present invention, this is accomplished by attaching auxiliary stringers between the original stringers which were present when the blanket was connected to the frame.
  • the original stringers are preferably run through the spaced frame elements, usually the ribs, and the auxiliary stringers are arranged as intercostals located wholly between the frame elements or ribs.
  • the blanket may be reinforced over the total area or over local areas by auxiliary stringers of any desired character and size, usually of a smaller size than the through-running stringers and conveniently of derby shape partly or wholly overlying the side flanges of the through-running stringers.
  • Fig. 1 is a plan view of a skin blanket, certain related inter-spar ribs being shown in broken lines;
  • Fig. 3 is a partial transverse section taken on the line il of Fig. 1;
  • Fig. 4 is a perspective view of one of the intercostal stringers
  • Fig. 5 is a perspective view of a cap for the stringer shown in Fig. 4;
  • Fig. 6 is a perspective view of another one of the intercostal stringers.
  • Fig. 'l is a perspective view of a cap for the stringer shown in Fig. 6.
  • a skin blanket A is secured to a framework which includes spaced ribs B and spars C
  • the skin blanket includes a skin sheet it made up of as many adjoining pieces as necessary and a plurality of through-running stringers H which are connected to the skin before the blanket is secured to the frame.
  • the stringers II are shown to be made of a flanged Y-bulb shape with return out-curved flanges,
  • the bulb portion is designated by the numeral ila, the web by lib, the main base flanges by He, and the return flanges by lid.
  • the rib B as shown, comprises a web plate I5, a web plate extension l6 formedwith recesses ii to receive the stringers, cap strips 18, and strut stringers i8. Cupped clips 20 connect the skin It, stringers ii and rib elements It together, the
  • clips preferably being split to enable them to be easily inserted in the recessed sides of the stringers and being secured together by the strut stringers i9.
  • the clips 20 have an end plate body portion aligned with the rib web plate l5 and side flanges which lie against andare secured to the web lib and flange 0 of the stringers II.
  • the other edges of the clips are flat and lie against and are secured to the rib plate extension i6 and the strut stringer N.
  • the skin blanket is spliced through the rib by certain joint means generally indicated by the numeral II but it is not necessary to describe the details of this Joint for an understanding of the present invention.
  • intercostal stringers are inserted between the principal stringers Ii.
  • the intereostals 25 are formed as derby sections having rounded channels 25a and attaching flanges 25?).
  • One side flange of the intercostal stringers is secured above a side flange lie of the principal stringers Ii and where twin stringers are used the common central flange 25b Adjacent the ribs the return flanges lld oi the principal stringers are' cut away at lie, as best shown in Fig. 1, and here caps are secured over the ends oi the stringers.
  • the caps are made to fit the stringers 25 and here comprise curved portions 80a with closed ends and flanges 302.). They may be joggled, as at the, where they drop .oi! oi' the ends of the flanges oi the principal stringers.
  • the caps 30 at one end of the stringers may be secured to the stringers before the stringers are attached to the skin sheets, and the caps at the other end also it the space for the full length or the stringers is not obstructed; but usually this space is obstructed and it is desired to secure the caps at the other end after the stringer elements have been brought into proper position secured to the stringers and their caps before they are attached to the assembly.
  • are inserted after the stringer with its unflanged cap has been inserted.
  • of cap and stringer, being laterally outstanding, can be secured together, as by welding, after the parts have been inserted and secured to the assembly.
  • the invention provides an improved structure and an improved method oi.
  • a fabricated structure composed oi spaced ribs, through-running stringers, intermediate stringers which end at the ribs, and a cover sheet, the first said stringers having base flanges secured to the skin, said flanges having return edges extending away from the skin, the edges being cut away at the ribs, and the intermediate stringers being concave and having base flanges mounted onthe base flanges of the first stringers, the intermediate stringers also having closed cupped ends fitting over the ends of the side edges 0! the first stringers.
  • a fabricated structure comprising in combination, a plurality of spaced ribs, a skin blanket, and clips securing the blanket to the ribs, said blanket comprising parallel stringers including large through-running flanged Y-bulb members and small flanged-derby capped intercostals, the caps at one end of the derby stringers having lateral flange connections with these derby stringers.

Description

FABRICATED STRUCTURE Filed Feb. 25, 1944 2 Sheets-Sheet 1 1 m1: Ii T ffffffi F i I:::, :1E:;::::::;; 1 -IIILLiiiTlZIZZ I Z B @5 K4 2 Q g f INVENTOR I Michael miter;
gv m 7. /M- ATTORNEY March 26, 1946.
' Filed Feb. 25, 1944 M. WATTER FABRICATED STRUC TURE 2 Sheets-Sheet 2 I N V EN TOR Michael Matter; 1
.4 TTORNE Y Patented Mar. 26, 1946 p 2.397.450 ranmcxran s-rauoruan' Michael WattenPhiladelphia, Pa., assignor to Edward G. Budd Manufacturing Company,
Philadelphia, Pa., a corporation of Pennsylvania Application February 25, 1944, Serial No. 523,846
3 Claims.
This invention relates to fabricated structures, particularly metallic structures, such as airioils,
which include an interior framework and a covering sheet, and has for an object the provision of improvements in this art.
In order to secure the desired strength and light weight in an airfoil cover, it is customary to reinforce the thin metal cover sheet with 'stifleners,
(01. Rik-3 tools of considerable size, hence as much free a space as possible is desirable at the region of connection.
According to the present invention, the blanket is initially provided with relatively heavy stringers and is attached to the framework while there is ample space between the stringers to receive the tool elements needed to make the connection. With such a construction, it is easy to connect the clips either to the skin blanket or the framework. Preferably, the clips are first attached to the skin blanket and later attached to the framework. After the blanket is secured to the framework, it may be desirable to further stiffen or strengthen it and, according to the present invention, this is accomplished by attaching auxiliary stringers between the original stringers which were present when the blanket was connected to the frame. The original stringers are preferably run through the spaced frame elements, usually the ribs, and the auxiliary stringers are arranged as intercostals located wholly between the frame elements or ribs. In this manner, the blanket may be reinforced over the total area or over local areas by auxiliary stringers of any desired character and size, usually of a smaller size than the through-running stringers and conveniently of derby shape partly or wholly overlying the side flanges of the through-running stringers.
The objects and advantages of the invention will be apparent from the following description of an exemplary embodiment, reference being made to the accompanying drawings, wherein:
Fig. 1 is a plan view of a skin blanket, certain related inter-spar ribs being shown in broken lines;
Fig. 2 is a partial longitudinal section taken on the line 2-2 of Fig. 1;
Fig. 3 is a partial transverse section taken on the line il of Fig. 1;
Fig. 4 is a perspective view of one of the intercostal stringers;
Fig. 5 is a perspective view of a cap for the stringer shown in Fig. 4;
Fig. 6 is a perspective view of another one of the intercostal stringers; and
Fig. 'l is a perspective view of a cap for the stringer shown in Fig. 6.
Referring to the drawings, a skin blanket A is secured to a framework which includes spaced ribs B and spars C, The skin blanket includes a skin sheet it made up of as many adjoining pieces as necessary and a plurality of through-running stringers H which are connected to the skin before the blanket is secured to the frame. Herein the stringers II are shown to be made of a flanged Y-bulb shape with return out-curved flanges, The bulb portion is designated by the numeral ila, the web by lib, the main base flanges by He, and the return flanges by lid.
The rib B, as shown, comprises a web plate I5, a web plate extension l6 formedwith recesses ii to receive the stringers, cap strips 18, and strut stringers i8. Cupped clips 20 connect the skin It, stringers ii and rib elements It together, the
. clips preferably being split to enable them to be easily inserted in the recessed sides of the stringers and being secured together by the strut stringers i9. As shown in Figures 2 and 3, the clips 20 have an end plate body portion aligned with the rib web plate l5 and side flanges which lie against andare secured to the web lib and flange 0 of the stringers II. The other edges of the clips are flat and lie against and are secured to the rib plate extension i6 and the strut stringer N. In some instances, at certain rib stations the skin blanket is spliced through the rib by certain joint means generally indicated by the numeral II but it is not necessary to describe the details of this Joint for an understanding of the present invention.
After the above-described assembly has been completed, with the exception possibly of the spars C, certain intercostal stringers are inserted between the principal stringers Ii. Conveniently, the intereostals 25 are formed as derby sections having rounded channels 25a and attaching flanges 25?). One side flange of the intercostal stringers is secured above a side flange lie of the principal stringers Ii and where twin stringers are used the common central flange 25b Adjacent the ribs the return flanges lld oi the principal stringers are' cut away at lie, as best shown in Fig. 1, and here caps are secured over the ends oi the stringers. The caps are made to fit the stringers 25 and here comprise curved portions 80a with closed ends and flanges 302.). They may be joggled, as at the, where they drop .oi! oi' the ends of the flanges oi the principal stringers.
The caps 30 at one end of the stringers may be secured to the stringers before the stringers are attached to the skin sheets, and the caps at the other end also it the space for the full length or the stringers is not obstructed; but usually this space is obstructed and it is desired to secure the caps at the other end after the stringer elements have been brought into proper position secured to the stringers and their caps before they are attached to the assembly. And, as stated, the caps with the flanges 3| are inserted after the stringer with its unflanged cap has been inserted. The flanges 3| of cap and stringer, being laterally outstanding, can be secured together, as by welding, after the parts have been inserted and secured to the assembly.
While various connecting means may be used for joining the structural elements, it is assumed for purposes of illustration that the means may be resistance welding, and in various places conventional weld indicia are shown in the drawings. Conveniently all or most of the welding on the skin blanket and ribs is done before the spars are attached, unless ample access openings are present as is sometimes the case.
It is thus seen that the invention provides an improved structure and an improved method oi.
assembly which furnishes maximum strength and lightness and maximum access for assembling operations.
While one embodiment oi the invention has been illustrated and described, it is to be understood that there. may be various embodiments within the limits or the prior art and the scope or the subioined claims.
What is claimed is:
l. A fabricated structure comprising in combination, a plurality of spaced ribs, a skin blanket, and clips securing the blanket to the ribs, said blanket including heavy rib-attached stringers and light flanged-derby stringers, some of the derbystringers being of double derby section with flanges on each side and in the middle, the side flanges being-secured upon flanges oi the heavy stringers and the middle flange being secured on a filler plate, said derby-section stringers terminating short of the ribs and having closed end caps.
2. A fabricated structure composed oi spaced ribs, through-running stringers, intermediate stringers which end at the ribs, and a cover sheet, the first said stringers having base flanges secured to the skin, said flanges having return edges extending away from the skin, the edges being cut away at the ribs, and the intermediate stringers being concave and having base flanges mounted onthe base flanges of the first stringers, the intermediate stringers also having closed cupped ends fitting over the ends of the side edges 0! the first stringers.
3. A fabricated structure comprising in combination, a plurality of spaced ribs, a skin blanket, and clips securing the blanket to the ribs, said blanket comprising parallel stringers including large through-running flanged Y-bulb members and small flanged-derby capped intercostals, the caps at one end of the derby stringers having lateral flange connections with these derby stringers.
MICHAEL WA'ITER.
US523846A 1944-02-25 1944-02-25 Fabricated structure Expired - Lifetime US2397450A (en)

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2582144A (en) * 1946-02-20 1952-01-08 Johns Manville Wall assembly
US2638170A (en) * 1947-06-28 1953-05-12 Richard H Prewitt Aircraft propeller or rotor
US20100258676A1 (en) * 2007-10-18 2010-10-14 Airbus Operations (S.A.S.) Aircraft including stiffener edge junctions and method for producing one such aircraft

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2582144A (en) * 1946-02-20 1952-01-08 Johns Manville Wall assembly
US2638170A (en) * 1947-06-28 1953-05-12 Richard H Prewitt Aircraft propeller or rotor
US20100258676A1 (en) * 2007-10-18 2010-10-14 Airbus Operations (S.A.S.) Aircraft including stiffener edge junctions and method for producing one such aircraft
CN101896399A (en) * 2007-10-18 2010-11-24 空中客车营运有限公司 Aircraft including stiffener edge junctions and method for producing one such aircraft
JP2011500415A (en) * 2007-10-18 2011-01-06 エアバス オペレーションズ (エスアーエス) Aircraft having a stiffener end connection and a method of manufacturing such an aircraft
US8480031B2 (en) * 2007-10-18 2013-07-09 Airbus Operations Sas Aircraft including stiffener edge junctions and method for producing one such aircraft
CN101896399B (en) * 2007-10-18 2013-09-25 空中客车营运有限公司 Aircraft including stiffener edge junctions and method for producing one such aircraft

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