GB560996A - Improvements in or connected with wings for aircraft - Google Patents

Improvements in or connected with wings for aircraft

Info

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
Application number
GB1544142A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
SHORT BROTHERS ROCHESTER & BEDFORD Ltd
Original Assignee
SHORT BROTHERS ROCHESTER & BEDFORD Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by SHORT BROTHERS ROCHESTER & BEDFORD Ltd filed Critical SHORT BROTHERS ROCHESTER & BEDFORD Ltd
Priority to GB1544142A priority Critical patent/GB560996A/en
Publication of GB560996A publication Critical patent/GB560996A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C9/00Adjustable control surfaces or members, e.g. rudders
    • B64C9/14Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/16Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • B64C9/20Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by multiple flaps
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C9/00Adjustable control surfaces or members, e.g. rudders
    • B64C9/14Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/16Adjustable 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.
GB1544142A 1942-11-03 1942-11-03 Improvements in or connected with wings for aircraft Expired GB560996A (en)

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)

* Cited by examiner, † Cited by third party
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

Cited By (3)

* Cited by examiner, † Cited by third party
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

Similar Documents

Publication Publication Date Title
GB1059638A (en) Rotor blade folding mechanism
GB560996A (en) Improvements in or connected with wings for aircraft
US2719300A (en) Fire control for stud driver
ATE24605T1 (en) HANDLING DEVICE FOR DOORS.
GB1175959A (en) Door locks.
US1858345A (en) Automatic window fastener
GB592591A (en) Improvements in locking devices
GB573165A (en) Improvements in or relating to door locks
US2406772A (en) Folding photographic camera
US2344348A (en) Handcuff
GB558755A (en) Improvements in and relating to catapult spools for aircraft
US2188642A (en) Automatic latch with push-button release
US2520799A (en) Camera having film cutoff knife and removable magazine
US3736810A (en) Slat retract gate
GB371442A (en) Improvements in or connected with means for controlling aeroplanes
SU201082A1 (en) Aircraft landing gear shutters control device
GB548916A (en) Improvements in and relating to mechanism for releasably locking a pivoted member in one or more positions, particularly applicable to retractable undercarriages for aircraft
GB986661A (en) Door lock
US2587867A (en) Latch mechanism
GB544543A (en) Improvements in or relating to the operating mechanisms of retractable members on aircraft
GB555556A (en) Improvements in door and like fastenings
GB1397946A (en) Door including a door fastening device
GB698356A (en) Improvements in or relating to aircraft landing lamps
US2441033A (en) Door latch
GB516270A (en) Improvements in or relating to locking pins whereby two parts may be secured in predetermined relationship