GB560996A - Improvements in or connected with wings for aircraft - Google Patents
Improvements in or connected with wings for aircraftInfo
- Publication number
- GB560996A GB560996A GB1544142A GB1544142A GB560996A GB 560996 A GB560996 A GB 560996A GB 1544142 A GB1544142 A GB 1544142A GB 1544142 A GB1544142 A GB 1544142A GB 560996 A GB560996 A GB 560996A
- Authority
- GB
- United Kingdom
- Prior art keywords
- flap
- nut
- flaps
- link
- movement
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
- B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
- B64C9/20—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by multiple flaps
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
- B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transmission Devices (AREA)
Abstract
560,996. Controlling aircraft. SHORT BROS. (ROCHESTER, & BEDFORD), Ltd.; and GOUGE, A. Nov. 3, 1942, Nos. 15441 and 18608. [Class 4] An aircraft wing is provided with primary and secondary ex tension flaps. in tandem which are adapted to be extended in sequence outwardly and down wardly so as to open slots at their leading edges at separate and successive stages, first one slot and then the other being opened by continued operation of the extending means. In one form, a primary flap B normally nested beneath the trailing edge of a wing A has a secondary flap C normally nested beneath the primary flap, both flaps being movable rearwardly and downwardly upon curved rails, not shown, mounted on the wing A and flap B respectively: The flap B is extended by a nut D traversed along a screwed shaft D until the position shown in Fig. 2 is reached, which is the position for take-off, after which, further movement of the nut releases a latching lever B<5> from engagement with one end of a lever B<1> pivoted in the flap B, the other end of which is connected by a link B<2> to a pin B<3> working in a slot A<1>. Continued movement of the nut D<1> immediately causes the pin B<3> to engage the end of the slot A<1> and the lever B<1> is turned to project the secondary flap C through a link B<4>, lever C<1> and link C<2>. The position with both flaps projected is used for landing. Reverse movement of the screwed shaft restores the parts to their initial position. Fig. 8 'shows another form in which the nut D<1> is connected primarily to the secondary flap C by a jointed link C<5>, C<2>. When the position shown is reached, the end of the link C<5>, which is forked, encounters an abutment on the flap B, and two rollers C<6>, Fig. 11, engage recesses in two half pinions B<8> mounted in the flap B and engaging short racks A<2> on the wing. Further movement of the nut D<1> then projects the flap B and the half pinions are rotated by the racks A<2> until they engage the opposite sides of the rollers C<6>, to which position they are biassed by a coiled spring, and further movement of the nut D<1> projects the flap B completely. Return movement of the nut returns the flap B to the position shown in which the rollers C<6> are released from the pinions B<8> by the action of the racks, whereupon the flap C can be retracted. Fig. 16 shows another form in which the nut D<1>, slidable in a groove B<6> in the flap B, is connected by a link C<2> to the flap C, both flaps being biassed to their retracted positions by springs E, E<1>, of which the spring E<1> is the stronger. Movement of the nut D<1> to project the flaps first moves the flaps B, C together until the flap B encounters a stop, after which the flap C is projected. In a modification, the spring E<1> is omitted and the flap C is projected until the nut D<1> encounters an abutment on the flap B which is then extended. In a further modification, the nut D<1> is similarly connected to the flap C and both springs are omitted. In this form the flap B is locked to the wing by a pivoted latch which is released by the nut D<1> just before the latter reaches the abutment on the flap. In the form shown in Fig. 4, a nut D<1> on the shaft D is connected by a link C<2> to the flap C and a second nut on the shaft is rotatable within a housing D<3> having trunnions working in guides B<7> in the flap B. Rotation of the shaft D extends the flap C until an extension on the nut D<1> releases a lock B<5> just before the nut engages an abutment D<2> on the flap B. The nut in the housing D<3> rotates freely during this stage of the extension. Further rotation of the shaft causes movement of the flap B and the end pressure of the housing D<3> against the enclosed nut arrests its rotation so that it advances in step with the nut D<1> and prevents the flap from overrunning the nut D<1>. The flaps may be further subdivided and arranged to open slots successively as the operating mechanism is actuated. Specifications 443,516, 470,923 and 510,774 are referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1544142A GB560996A (en) | 1942-11-03 | 1942-11-03 | Improvements in or connected with wings for aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1544142A GB560996A (en) | 1942-11-03 | 1942-11-03 | Improvements in or connected with wings for aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB560996A true GB560996A (en) | 1944-05-01 |
Family
ID=10059194
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1544142A Expired GB560996A (en) | 1942-11-03 | 1942-11-03 | Improvements in or connected with wings for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB560996A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4434959A (en) | 1981-09-28 | 1984-03-06 | The Boeing Company | Airfoil flap assembly with flap track member |
USRE32907E (en) * | 1981-09-28 | 1989-04-18 | The Boeing Company | Airfoil flap assembly with flap track member |
US11459091B2 (en) * | 2018-12-20 | 2022-10-04 | Bombardier Inc. | System and method for controlling aircraft flight control surfaces |
-
1942
- 1942-11-03 GB GB1544142A patent/GB560996A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4434959A (en) | 1981-09-28 | 1984-03-06 | The Boeing Company | Airfoil flap assembly with flap track member |
USRE32907E (en) * | 1981-09-28 | 1989-04-18 | The Boeing Company | Airfoil flap assembly with flap track member |
US11459091B2 (en) * | 2018-12-20 | 2022-10-04 | Bombardier Inc. | System and method for controlling aircraft flight control surfaces |
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