GB563929A - Improvements in or relating to jack screws particularly for aircraft cowls - Google Patents
Improvements in or relating to jack screws particularly for aircraft cowlsInfo
- Publication number
- GB563929A GB563929A GB3396/42A GB339642A GB563929A GB 563929 A GB563929 A GB 563929A GB 3396/42 A GB3396/42 A GB 3396/42A GB 339642 A GB339642 A GB 339642A GB 563929 A GB563929 A GB 563929A
- Authority
- GB
- United Kingdom
- Prior art keywords
- screw
- sleeve
- cup
- nut
- worm
- 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
- 229910000906 Bronze Inorganic materials 0.000 abstract 1
- 239000010974 bronze Substances 0.000 abstract 1
- KUNSUQLRTQLHQQ-UHFFFAOYSA-N copper tin Chemical compound [Cu].[Sn] KUNSUQLRTQLHQQ-UHFFFAOYSA-N 0.000 abstract 1
- 239000000428 dust Substances 0.000 abstract 1
- 239000000463 material Substances 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/08—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of power plant cooling systems
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transmission Devices (AREA)
- Gear Transmission (AREA)
Abstract
563,929. Screw-and-nut gearing. STEVENS, A. H. (Lear Avia, Inc.). March 14, 1942, No. 3396. [Class 80 (iii)] [Also in Groups X, XXV, XXXII and XXXIII] Consists in screw-and-nut gearing particularly applicable to the operation of ventilating flaps on the cowl of aircraft engines. Flaps 23, Fig. 2, are spaced around a cowl 20. Each flap is resiliently connected to one end of a jack screw 25, the other end of which is resiliently connected to a stationary gear-box 26. These boxes are mounted on a ring 27 and are actuated by flexible shafts 28 from an electric motor 31 preferably embodying features described in Specification 549,552. The jack, screw, Fig. 3, comprises a screw 32 flexibly coupled to gearbox 26 through a cup 33, and a coacting sleeve 34 flexibly coupled to a cup 35 secured to the flap 23. By arranging the sleeve adjacent the flap, the screw 32 is protected from dust &c. carried by the air stream. The motor drives a worm 41, Fig. 5, gearing with a worm-wheel 43 secured to a shaft 44 coupled to the flexible shafts 28. Sleeve 34, Fig. 8, has a ring 51 with flange 53 forced thereon, and a retainer ring 54 is press fitted into cup 35, the rings being bonded to rubber 50. The flange 53 is sufficiently large to prevent the sleeve dropping through the aperture 56 in the base of the cup. The screw 32 is secured to the cup 33 in a similar manner and the cup is connected by screws 74 to a flanged member 73 integral with the shaft 72, Fig. 12, of a gear unit. In this unit a worm-wheel 75 on shaft 72 is driven by a worm coupled to the flexible shafts 28. In modified forms of connection of sleeve and screw to the cups 35, 33 respectively, the flanged rings 51, 67, Fig. 8, are replaced by thick barrelshaped rings. The screw 32 works in a long nut 61, Fig. 8, of tough material, e.g. tobin bronze, the nut being secured by swaging over the end of the sleeve at 62. A nut 64 on the end of the screw prevents the latter from being pulled out from the sleeve.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3396/42A GB563929A (en) | 1942-03-14 | 1942-03-14 | Improvements in or relating to jack screws particularly for aircraft cowls |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3396/42A GB563929A (en) | 1942-03-14 | 1942-03-14 | Improvements in or relating to jack screws particularly for aircraft cowls |
Publications (1)
Publication Number | Publication Date |
---|---|
GB563929A true GB563929A (en) | 1944-09-06 |
Family
ID=9757545
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3396/42A Expired GB563929A (en) | 1942-03-14 | 1942-03-14 | Improvements in or relating to jack screws particularly for aircraft cowls |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB563929A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110466782A (en) * | 2019-07-26 | 2019-11-19 | 中国航发沈阳发动机研究所 | A kind of aero-engine elastic connecting component |
-
1942
- 1942-03-14 GB GB3396/42A patent/GB563929A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110466782A (en) * | 2019-07-26 | 2019-11-19 | 中国航发沈阳发动机研究所 | A kind of aero-engine elastic connecting component |
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