ES1009344U - Improved pump practices for launch from aircraft. (Machine-translation by Google Translate, not legally binding) - Google Patents

Improved pump practices for launch from aircraft. (Machine-translation by Google Translate, not legally binding)

Info

Publication number
ES1009344U
ES1009344U ES19888802771U ES8802771U ES1009344U ES 1009344 U ES1009344 U ES 1009344U ES 19888802771 U ES19888802771 U ES 19888802771U ES 8802771 U ES8802771 U ES 8802771U ES 1009344 U ES1009344 U ES 1009344U
Authority
ES
Spain
Prior art keywords
launch
aircraft
translation
machine
legally binding
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.)
Granted
Application number
ES19888802771U
Other languages
Spanish (es)
Other versions
ES1009344Y (en
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.)
GALANTE TERRER JAVIER
Original Assignee
GALANTE TERRER JAVIER
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 GALANTE TERRER JAVIER filed Critical GALANTE TERRER JAVIER
Priority to ES8802771U priority Critical patent/ES1009344Y/en
Publication of ES1009344U publication Critical patent/ES1009344U/en
Application granted granted Critical
Publication of ES1009344Y publication Critical patent/ES1009344Y/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Landscapes

  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

Pump range improved to launch from aircraft, wherein be formed by two main bodies, the first a cylindrical body closed at both ends by two cups o tapas leaving a duct axial to joins the second body or tube-shaft inertia, two segments cylindrical different diameter and concentric housing a signaling element, introducing the end free of such tube a set of fins for the stabilization of flight, while its opposite end is welded to previous cazoleta closing first body and interior kingdom by tapping the body of drill. (Machine-translation by Google Translate, not legally binding)
ES8802771U 1988-09-20 1988-09-20 PERFECTED PRACTICE PUMP FOR AIRCRAFT LAUNCH. Expired - Fee Related ES1009344Y (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
ES8802771U ES1009344Y (en) 1988-09-20 1988-09-20 PERFECTED PRACTICE PUMP FOR AIRCRAFT LAUNCH.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES8802771U ES1009344Y (en) 1988-09-20 1988-09-20 PERFECTED PRACTICE PUMP FOR AIRCRAFT LAUNCH.

Publications (2)

Publication Number Publication Date
ES1009344U true ES1009344U (en) 1989-08-16
ES1009344Y ES1009344Y (en) 1991-04-16

Family

ID=8258038

Family Applications (1)

Application Number Title Priority Date Filing Date
ES8802771U Expired - Fee Related ES1009344Y (en) 1988-09-20 1988-09-20 PERFECTED PRACTICE PUMP FOR AIRCRAFT LAUNCH.

Country Status (1)

Country Link
ES (1) ES1009344Y (en)

Also Published As

Publication number Publication date
ES1009344Y (en) 1991-04-16

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Legal Events

Date Code Title Description
FD1K Utility model lapsed

Effective date: 20001102